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VFS Forum Proceedings Papers Index

Forum Proceedings — 8842 papers found.

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Forum Presented At Title Authors Date Presented Date Added
Forum 02 Second Annual Forum of the American Helicopter Society, Inc. Second Annual Forum Proceedings, 175 pages. March 14, 1946 2018-23-07
Forum 03 A Comparison of Rotor Theory with Experimental Data Obtained From NACA Flight Tests of a Helicopter in Various Flight Conditions Alfred Gessow March 27, 1947 2012-02-10
Forum 03 Vibration Isolation in Helicopters Bartram Kelley, Bell Aircraft Corporation March 27, 1947 2012-02-10
Forum 03 Effect of Blade Stalling on the Efficiency of a Helicopter Rotor as Measured in Flight F.B. Gustafson and Alfred Gessow, Langley Memorial Aeronautical Laboratory March 27, 1947 2012-02-10
Forum 03 Limitations in Helicopter Design J. A. J. Bennett March 27, 1947 2012-02-10
Forum 03 The Helicopter - Navy Operational Uses, Past, Present and Future Captain C. C. Marcy, USN March 27, 1947 2012-02-10
Forum 03 Whirl Testing of Helicopter Rotors by the Air Materiel Command P. A. Simmons March 27, 1947 2012-02-10
Forum 03 Rotor Governor Testing by the A. M. C. W. E. Zins March 27, 1947 2012-02-10
Forum 03 Design and Development of Helicopter Main Transmissions Miller A. Wachs, Sikorsky Aircraft March 27, 1947 2012-02-10
Forum 03 Test Instrumentation Problems of the Helicopter Haig Kurkjian March 27, 1947 2012-02-10
Forum 03 Regulatory Problems Facing the Helicopter Industry L. Welch Pogue, National Aeronautic Association March 27, 1947 2012-02-10
Forum 03 Maintenance Procedures in Commercial Helicopter Operations Lou Leavitt, Helicopter Air Transport, Inc. March 27, 1947 2012-02-10
Forum 03 Agricultural Uses of The Helicopter Frank H. Kelley Jr., Bell Aircraft Corporation March 27, 1947 2012-02-10
Forum 03 Commercial School Operations H. G. Earle March 27, 1947 2012-02-10
Forum 03 Some Problems of Helicopter Operation and Their Influence on Design Reginald Brie, A.F.l.Ae.S. March 27, 1947 2012-02-10
Forum 03 Recent Post Office Experiences with Helicopter Operations A. E. Newton, U.S. Post Office March 27, 1947 2012-02-10
Forum 03 The Economics of the Helicopter for the Individual Horace T. Pentecost, Hoppi-Copters, Inc. March 27, 1947 2012-02-10
Forum 04 Co-Axial Design for Helicopter Mass Production Watson, Rowland J., Hopp-Copters, Inc. April 22, 1948 2012-19-07
Forum 04 Contribution to the Problem of Helicopter Stability Hohenemser, Kurt, McDonnell Aircraft Corporation April 22, 1948 2012-19-07
Forum 04 Gyroscopic Forces on Hinged Rotors Myers, Garry C. Jr. April 22, 1948 2012-19-07
Forum 04 Notes on the Flying Qualities of Helicopters Reeder, John P. and Gustafson, F. B. April 22, 1948 2012-19-07
Forum 04 Some Aspects of Convertible Aircraft Design Lichten, R. L., Bell Aircraft Corporation April 22, 1948 2012-19-07
Forum 04 Lubrication Considerations in Helicopter Transmissions Wolf, Robert A. and Lappin, Arthur N. April 22, 1948 2012-19-07
Forum 04 The Design of Rotor Blade Dampers Douglas, L. L., Kellett Aircraft Corporation April 22, 1948 2012-19-07
Forum 04 Attacking the Maintenace Problem through Mechanical Design Doman, Glidden S., Doman-Frasier Helicopters, Inc. April 22, 1948 2012-19-07
Forum 04 The Coast Guard Cutter-Helicopter Team Commander Erickson, F. A., U.S.C.G. April 22, 1948 2012-19-07
Forum 04 Commercial Helicopter Operations Flint, Knute April 22, 1948 2012-19-07
Forum 04 Economic Factors Relating to Helicopter Air Mail Operations Rothman, Jack E., United Air Lines, Inc. April 22, 1948 2012-19-07
Forum 04 Application of the Helicopter in Connection with Surface Transport James, Russell B. April 22, 1948 2012-19-07
Forum 04 A Review of the Motion Picture "Los Angeles Airways Operations" Short, V. R., Sikorsky Aircraft April 22, 1948 2012-19-07
Forum 04 Helicopters Stabilizing Device Dorand, R., Societe Nationale De Constructions Aeronautiques Du Center April 22, 1948 2012-19-07
Forum 04 The Gyrodyne Dr. Bennett, J. A. J., Fairey Aviation Co. Ltd. April 22, 1948 2012-19-07
Forum 04 Helicopter Development at Bristol Aircraft Hafner, Raoul, Bristol Aeroplane Co. April 22, 1948 2012-19-07
Forum 04 The Helicopter in the Post Office Department Aiken, Paul, Post Office Department April 22, 1948 2012-19-07
Forum 04 The Military Aspects of Rotary Wing Development Colonel Culbertson, A. T. April 22, 1948 2012-19-07
Forum 04 Army Air Rescue Operations Captain Lyons, James April 22, 1948 2012-19-07
Forum 05 Honors Dinner Speech Col. E C. Dyer, United States Marine Corps May 12, 1949 2016-09-08
Forum 05 Performance Characteristics of a Combined Rotary Wing and Fixed Wing System Kurt R. Hohenemser, McDonnell Aircraft Corporation May 12, 1949 2016-09-08
Forum 05 Jet Propelled Rotor for Helicopters Joseph S. Yasecko, Air Materiel Command, Wright-Patterson Air Force Base May 12, 1949 2016-09-08
Forum 05 Flight Testing of Helicopters by the U.S. Navy John W. Mazur, Flight Test Division, U.S. Naval Air Test Center May 12, 1949 2016-09-08
Forum 05 Design and construction of the Cornell Fiberglass Helicopter Main Rotor Blades Harold Hirsch, Cornell Aeronautical Laboratory, Buffalo, New York May 12, 1949 2016-09-08
Forum 05 Helicopter Flight Test Technique Variable Blade Stiffness Program Hans Weichsel Jr., Cornell Aeronautical Laboratory, Inc., Buffalo, N.Y. May 12, 1949 2016-09-08
Forum 05 An Analysis of the Pressure Jet Helicopter L.L. Douglas, Kellet Aircraft Corporation May 12, 1949 2016-09-08
Forum 05 Development of Metal Blades a Simplified Dynamic Stress Analysis of Hinged Rotor Blades Robert Mayne and Wm. C. Johnson Jr., Goodyear Aircraft Corporation, Akron, Ohio May 12, 1949 2016-09-08
Forum 05 Miscellaneous Flight Characteristics of the Model 47 Helicopter T.J. Harriman, Asst. Chief Helicopter Engineer, Bell Aircraft Corporation May 12, 1949 2016-09-08
Forum 05 Properties of Case Hardened Steel Surface Effect of Grinding and Method of Detection and Prevention of Defective Areas Lawrence E. Follis, Sikorsky Aircraft May 12, 1949 2016-09-08
Forum 05 Punch Card Computing Techniques and their Application to Rotary Wing Aircraft Problems Frank L. Stulen, Parsons Corporation, Traverse City, Michigan May 12, 1949 2016-09-08
Forum 05 Note on the Fatigue Properties of Steel and Light Alloy for Helicopter Rotor Blades B.K.O. Lundberg, Director, The Aeronautical Research Institute of Sweden, FFA; and G. Larson, Research Engineer at the FFA May 12, 1949 2016-09-08
Forum 07 Helicopter Rotor Performance Possibilities Mr. Joseph Stuart, III, Bell Aircraft Corp. April 26, 1951 2012-27-02
Forum 07 The Effects of Compressibility on the Characteristics of Helicopter Rotors Mr. Paul J. Carpenter, N.A.C.A. April 26, 1951 2012-27-02
Forum 07 Service Life of Helicopter Rotors Mr. Robert Rosenbaum, C.A.A. April 26, 1951 2012-27-02
Forum 07 Design of a Rotor Kite Mr. Igor Benson, Kaman Aircraft Corp. April 26, 1951 2012-27-02
Forum 07 The Adaptation of Jets to Helicopters Mr. Paul H. L. Morain, Societe Nationale de Constructions Aeronautiques du Sud-Ouest, France April 26, 1951 2012-27-02
Forum 07 Demonstration Testing of Helicopters for the U.S. Navy Mr. John W. Mazur, Naval Air Test Center. April 26, 1951 2012-27-02
Forum 07 A Discussion of CAA Policies, Flight Test Procedures and Civil Air Regulations for Helicopters Mr. G. DeVore, C.A.A. April 26, 1951 2012-27-02
Forum 07 Testing Machines for Helicopter Transmissions Mr. D. W. Botstiber, Piasecki Helicopter Corp. April 26, 1951 2012-27-02
Forum 07 Symposium on Commercial Operations Mr. H. Boris - Repr. French Helicopter Operations; Clarence M. Belinn, President, Los Angeles Airways; Carl Agar, Okanogan Air Services April 26, 1951 2012-27-02
Forum 07 Symposium on Military Operations Capt. F. D. Foley, U.S.N. April 26, 1951 2012-27-02
Forum 07 Some Lessons of the Liverpool-Cardiff Helicopter Service Mr. L. S. Wigdortchick, British European Airways April 26, 1951 2012-27-02
Forum 07 Some Economic and Logistic Aspects of Helicopter Operations by the Armed Forces Lt. Col. K. B. McCutcheon, U.S.M.C. April 26, 1951 2012-27-02
Forum 07 Economic Prospects for Large Transport Helicopters Mr. Richard K. Waldo, C.A.A. April 26, 1951 2012-27-02
Forum 08 Problems in Korean Helicopter Maintenance and Their Relations to the Service Representative Harold Nachlin, United Aircraft Corp May 15, 1952 2012-08-03
Forum 08 U. S. Army Helicopter Maintenance Experience in Korea Lt. Col. George L. Lovett, Ordnance Corps May 15, 1952 2012-08-03
Forum 08 Design for Maintenance Lt. Phillip W. Kerr, USN, and Capt. Eugene J. Pope, USMC May 15, 1952 2012-08-03
Forum 08 Korean Rescue Operations Major John J. Dean, USAF Air Rescue Service May 15, 1952 2012-08-03
Forum 08 Helicopter Operations in Alaska Lt. Col. Gene L. Douglas, USAF, Air Rescue Service May 15, 1952 2012-08-03
Forum 08 Helicopter Operation for Patrol of Power Lines in Remote Areas T. J. Burgess, Hydro-Electric Power Commission May 15, 1952 2012-08-03
Forum 08 The Effect of Blade Mass Constant and Flapping Hinge Offset on Maximum Blade Angles of Attack at High Advance Ratios John R. Meyer Jr., and Gaetano Falabella. Jr., Massachusetts Institute of Technology May 15, 1952 2012-08-03
Forum 08 Some Remarks on Dynamic Stability of the Helicopter and Characteristics of Gyratory Stabilizing Systems Dr. G. J. Sissingh, Kellett Aircraft Corp May 15, 1952 2012-08-03
Forum 08 An Analysis of the Helicopter Transfer Function to Predict Achievable Handling Characteristics of the Stabilized Helicopter Edward Sterling Carter Jr., Sikorsky Aircraft Division May 15, 1952 2012-08-03
Forum 08 Comparison of Helicopter Rotor Propulsion Systems Joseph Stuart III, Bell Aircraft Corp May 15, 1952 2012-08-03
Forum 08 Some Aerodynamic and Dynamic Problems of the Compound Rotary-Fixed Wing Aircraft Kurt Hohenemser, McDonnell Aircraft Corp May 15, 1952 2012-08-03
Forum 08 Development of High Lift Airfoils by Boundary Layer Control Kenneth Razak, University of Wichita May 15, 1952 2012-08-03
Forum 08 Air Force Testing and Evaluation of Helicopters Capt. Wayne W. Eggert, Wright-Patterson AFB May 15, 1952 2012-08-03
Forum 08 Role of Transport Helicopter in Metropolitan Areas Jack Rothman, New York Airways May 15, 1952 2012-08-03
Forum 09 Basic Problems In Helicopter Development F. L. Dohlhoff May 14, 1953 2016-18-11
Forum 09 Basic Problems In Helicopter Development F. L. Dohlhoff May 14, 1953 2015-25-01
Forum 09 Application Of Statistical Techniques To The Interpretation Of Fatigue Data Donald L. Henry May 14, 1953 2015-25-01
Forum 09 Application Of Statistical Techniques To The Interpretation Of Fatigue Data Donald L. Henry May 14, 1953 2019-30-01
Forum 09 The Application Of Models To Helicopter Vibration And Flutter Research George W. Brooks May 14, 1953 2015-25-01
Forum 09 Applications Of Stress Models To Rotor Blade Design Analysis Thomas H. Purcell May 14, 1953 2015-25-01
Forum 09 An Approach To The Determination Of Higher Harmonic Rotor Blade Stresses H. Daughaday; J. Kline May 14, 1953 2015-25-01
Forum 09 Tip-Mounted. Turbojet Engines For Helicopter Rotor Propulsion John B. Nichols May 14, 1953 2015-25-01
Forum 09 Development Of The Double Cage Full Phasing Borg - Warner Sprag Clutch H. P. Troendly; R. R. Anderson May 14, 1953 2015-25-01
Forum 09 Talk To Bf Delivered Before The American Helicopter Society May 1953 Stephen duPont May 14, 1953 2015-25-01
Forum 09 Simulated Service Testing Of Rotor Blades Earl T. Ireton Jr. May 14, 1953 2015-25-01
Forum 09 Convertiplane Development Tests William E. Cobey May 14, 1953 2015-25-01
Forum 09 Some Problems Of Helicopter Rotor Blade Ice Removal L. C. Houser May 14, 1953 2015-25-01
Forum 09 The Design Of An Electrical Cyclic Thermal De-Icing System For Helicopter Rotor Blades Ward J. Carter May 14, 1953 2015-25-01
Forum 09 Anti-Ice Testing Of The Prewitt Metal Rotor Blade Robert M. DeWitt May 14, 1953 2015-25-01
Forum 09 A New Approach To Helicopter Stability F. A. Erickson May 14, 1953 2015-25-01
Forum 09 Flight Operations I. B. Washburn May 14, 1953 2015-25-01
Forum 09 Flight Operations George P. Gaffney May 14, 1953 2015-25-01
Forum 09 Flight Operations Edward J. Larkin May 14, 1953 2015-25-01
Forum 09 Flight Characteristics Of The Coaxial Helicopter James V. Ryan May 14, 1953 2015-25-01
Forum 10 Accelerometer Control Bartram Kelley May 24, 1954 2012-08-03
Forum 10 The Technical Aspects of the Transfer of Fuel to a Tip Mounted Ramjet Engine Combustion Chamber H. K. Holm May 24, 1954 2012-08-03
Forum 10 Automatic Control of Helicopters Delvin E. Kendall Jr. May 24, 1954 2012-08-03
Forum 10 Theory of Rotor Blade Uncoupled Flap Bending Aero-Elastic Vibrations Peter F. Leone May 24, 1954 2012-08-03
Forum 10 Summary of Discussion For Gas Turbine Panel F. L. Doblhoff May 24, 1954 2012-08-03
Forum 10 Advantages of Centrifugal Compressors in Helicopter Gas-Turbine Engines S. D. Hage May 24, 1954 2012-08-03
Forum 10 Control Aspects of the Free Turbine Helicopter Engine R. F. Owens May 24, 1954 2012-08-03
Forum 10 A Practical Approach to the Metal Blade Spar Problem F. L. Stulen and A. J. Belfour May 24, 1954 2012-08-03
Forum 10 Design and Flight Test of a Two-Speed Helicopter Transmission Lt. Paul L. Munter May 24, 1954 2012-08-03
Forum 10 Design and Development of the Hydro-Mechanical Clutch A. Koup and Miller Wachs May 24, 1954 2012-08-03
Forum 10 A Column-Spring Blade Retention Giving Speed-Governing Characteristics William H. Raser, Jr May 24, 1954 2012-08-03
Forum 10 Optimum Design of Transport Helicopters for Maximum Net Profit F. David Schnebly and Richard M. Carlson May 24, 1954 2012-08-03
Forum 10 Operational and Economic Experience of Helicopter Air Service, Inc. C. W. Moore May 24, 1954 2012-08-03
Forum 10 Some Observations on Military Transport Helicopter Economics and Availability Major Michael J. Strok, Office, Chief of Transportation, Department of the Army May 24, 1954 2018-04-10
Forum 10 Some Interesting Experiences In Developing Helicopter Transmission Lubrication Systems N.C. Taylor, Piasecki Helicopter Corporation May 24, 1954 2018-04-10
Forum 11 Whirling-Arm Study of Wing Helicopters Wesley L. Cresap and George Galerstein, Bell Aircraft Corporation April 27, 1955 2012-20-07
Forum 11 Remarks on the Unloaded Rotor Type of Convertiplane Kurt H. Hohenemser, McDonnell Aircraft Corporation April 27, 1955 2012-20-07
Forum 11 The Bristol Type 173 - Design, Development and Experiences Raoul Hafner April 27, 1955 2012-20-07
Forum 11 Development of the Cessna CH-1 Helicopter Charles M. Seibel April 27, 1955 2012-20-07
Forum 11 Application of Helicopter Flight Simulators for Training and Research Purposes P. de Guillenchmidt, Giravions Dorand Company April 27, 1955 2012-20-07
Forum 11 Preliminary Investigation of the Karman - Yuan Helicopter Rotor System Dr. S. W. Yuan, Polytechnic Institute of Brooklyn April 27, 1955 2012-20-07
Forum 11 Effect of Blade Stalling and Drag Divergence on Power Required by a Helicopter Rotor at High Forward Speed Kenneth B. Amer, Hughes Tool Company April 27, 1955 2012-20-07
Forum 11 Effect of Blade Stalling and Drag Divergence on Power Required by a Helicopter Rotor at High Forward Speed Kenneth B. Amer, Hughes Tool Company April 27, 1955 2015-18-09
Forum 11 The Helicopter Activities of British European Airways Reginald Brie, A.F.R.Ae.S., A.F.I.Ae.S. April 27, 1955 2012-20-07
Forum 11 Design Requirements for Transport Type Helicopters J. E. Gallagher, New York Airways, Inc. April 27, 1955 2012-20-07
Forum 11 The Operation of Okanagan Helicopters Ltd. Carlyle C. Agar, Okanagan Helicopters, Ltd. April 27, 1955 2012-20-07
Forum 11 The Regulatory Aspects of Helicopter Operations K. S. Cooper, Civil Aeronautics Administration April 27, 1955 2012-20-07
Forum 11 The Helicopter Take-Off Problem R. B. Lightfoot April 27, 1955 2012-20-07
Forum 11 Equipment for Blind Approaches G. S. Hislop, Fairey Aviation Co. April 27, 1955 2012-20-07
Forum 11 Future Heliports Martin A. Warskow, The Port of New York Authority April 27, 1955 2012-20-07
Forum 11 Helicopter Navigation Cmdr. W. W. Bush, ANDB, Civil Aeronautics Administration April 27, 1955 2012-20-07
Forum 11 Instrumentation for Helicopter Navigation Dr. D. G. C. Luck, Radio Corp. of America April 27, 1955 2012-20-07
Forum 11 Addendum to 10th Annual Forum -- Theory of Rotor Blade Uncoupled Lag Bending Aero-Elastic Vibrations Peter F. Leone, Kellett Aircraft Corporation April 27, 1955 2012-20-07
Forum 12 Design Highlights of Lycoming's XT-53 Gas Turbine Dr. Anselm Franz May 2, 1956 2012-08-03
Forum 12 Fatigue Strength of Structures Having Bolted Connections Leonard A. Goran May 2, 1956 2012-08-03
Forum 12 The T58: A New Heritage for Helicopter Powerplants Harold T. Hokanson May 2, 1956 2012-08-03
Forum 12 A Study in Rotor Mechanics Bartram Kelley May 2, 1956 2012-08-03
Forum 12 The Rotor Acceleration Technique for Helicopter Tip Jet Engine Performance Raymond M. Lockwood May 2, 1956 2012-08-03
Forum 12 Comments on Helicopter Design and Test Requirements Robert R. Lynn May 2, 1956 2012-08-03
Forum 12 Experimental Investigation of Compressibility Effects on a Helicopter Rotor Having NACA 632-015 Airfoil Section James P. Shivers and Paul J. Carpenter May 2, 1956 2012-08-03
Forum 12 Helicopter Instrument Flight Operations Raymond F. Bohling May 2, 1956 2012-08-03
Forum 12 A Discussion of the Problems in the Selection and Development of Military Helicopter Pilots William H. Coffee May 2, 1956 2012-08-03
Forum 12 Helicopter and Fixed Wing Separation Standards Howard Higgins May 2, 1956 2012-08-03
Forum 12 Notes on Steep Instrument Approaches in a Helicopter John P. Reeder and James B. Whitten May 2, 1956 2012-08-03
Forum 12 Factors Affecting Utilization of Utility and Light Transport Aircraft (Fixed and Rotary Wing) Lt. Col. George Gaffney May 2, 1956 2012-08-03
Forum 12 Operating Efficiency of Verti-craft in Amphibious Operations Major William MacLean May 2, 1956 2012-08-03
Forum 12 Why No More Helicopter Subsidy James S. Ricklefs May 2, 1956 2012-08-03
Forum 12 Navigational Problems with Helicopters Robert L. Suggs May 2, 1956 2012-08-03
Forum 12 Addendum to the Twelfth Annual National Forum Addendum to the Twelfth Annual National Forum of the American Helicopter Society, May 2-5, 1956 at Sheraton-Park Hotel, Washington, D.C. May 2, 1956 2020-13-01
Forum 13 Metal Rotor Blade Development George H. Linnabery May 8, 1957 2012-10-03
Forum 13 Closing the Loop on Automatic Stabilization Equipment Walter Gerstenberger and Edward S. Carter Jr. May 8, 1957 2012-10-03
Forum 13 T53 Flight Test and Test Stand Results Leroy A. Howard May 8, 1957 2012-10-03
Forum 13 The Limitations of a Wing for Low Speed Flight John B. Nichols May 8, 1957 2012-10-03
Forum 13 Compromises Associated With VTOL and STOL Propellers Robert A. Rogers May 8, 1957 2012-10-03
Forum 13 Compromises Associated With VTOL and STOL Propellers Robert A. Rogers May 8, 1957 2015-22-12
Forum 13 Designing for Crash Survival in VTOL Aircraft A. Howard Hasbrook May 8, 1957 2012-10-03
Forum 13 Stability and Control of Propeller-Driven Transport VTOL Airplanes Robert H. Kirby May 8, 1957 2012-10-03
Forum 13 Determination of Flapwise Load Distribution on a Rotor Blade from Measured Strain and Rotor Data Herbert Somerson May 8, 1957 2012-10-03
Forum 13 Physical Interpretation of Helicopter Chordwise Vibration William B. Gevarter May 8, 1957 2012-10-03
Forum 13 On a Type of Low-Advance-Ratio Blade Flapping Instability of Three-or-More-Bladed Rotors Without Drag Hinges Kurt H. Hohenemser May 8, 1957 2012-10-03
Forum 13 Theoretical and Experimental Study of the Coupled Flap Bending and Torsion Aero-Elastic Vibrations of a Helicopter Rotor Blade Peter F. Leone May 8, 1957 2012-10-03
Forum 13 A Parametric Analysis Method for Rotor Blade Structural Design Alex Berman May 8, 1957 2012-10-03
Forum 13 Helicopter Transport Operations in the North Lt. Col. Oscar N. Tibbetts May 8, 1957 2012-10-03
Forum 13 The French Army Helicopter Operation in Algeria Thomas R. Pierpoint and Louis J. Geier May 8, 1957 2012-10-03
Forum 14 Presentation on Army Aviation April 16, 1958 2018-31-07
Forum 14 The Hot Cycle Jet Helicopter April 16, 1958 2018-31-07
Forum 14 Stability and Control of Unducted Stand on Helicopters Lt. M. William Townsend Jr., USN, and Edward Seckel April 16, 1958 2012-10-03
Forum 14 Test Experience on the Vertol 76 Tilt Wing VTOL Research Aircraft Paul J. Dancik, Frederick R. Mazzitelli, and Walter D. Peck April 16, 1958 2012-10-03
Forum 14 Ryan Vertiplane Development Fred Landgraf April 16, 1958 2012-10-03
Forum 14 Flight Testing of the XV-3 Convertiplane John R. Mertens, and Charles E. Davis April 16, 1958 2012-10-03
Forum 14 Flight Testing of the XV-3 Convertiplane John R. Mertens, and Charles E. Davis April 16, 1958 2016-29-04
Forum 14 Recent Advances in the Flying Qualities of Tandem Helicopters Bruce Blake, James M. Clifford, Raymond Kaczynski, and Philip F. Sheridan April 16, 1958 2012-10-03
Forum 14 Induced Flow Near a Rotor and Its Application to Helicopter Problems Harry H. Heyson April 16, 1958 2012-10-03
Forum 14 A Study of Turbine-Powered Helicopter Drive System Instability John C. Keeling, and David L. Kidd April 16, 1958 2012-10-03
Forum 14 A Mechanical Speed Control for Helicopter Power Plants Norman C. Olson April 16, 1958 2012-10-03
Forum 14 Tip Mounted Turbojet Helicopters Robert A. Wagner April 16, 1958 2012-10-03
Forum 14 Pressure Jet Helicopters Friedrich L. Von Doblhoff April 16, 1958 2012-10-03
Forum 15 Statistical Aspects of the Rotor Fatigue Problem G. F. Goetsch May 7, 1959 2012-10-03
Forum 15 General Electric T58 in Service Operation Coulman Westcot Jr. May 7, 1959 2012-10-03
Forum 15 Operational Analysis of Maintenance Costs Joseph A. Moro May 7, 1959 2012-10-03
Forum 15 Safe Mechanisms for Helicopters Raoul Hafner May 7, 1959 2012-10-03
Forum 15 Potential Service and Maintenance Improvements with Hydraulics W. Patterson and W. L. Flinn May 7, 1959 2012-10-03
Forum 15 Some Operational and Economic Aspects of the Fairey Rotodyne G. Hislop May 7, 1959 2012-10-03
Forum 15 Analysis of Helicopter Stability Augmentation Obtainable with the Oehmichen Pitch-Flap Coupling Concept G. Bruning May 7, 1959 2012-10-03
Forum 15 Means for Achieving Desirable Handling Characteristics in a Small Helicopter Kenneth Amer May 7, 1959 2012-10-03
Forum 15 The Application of Modern Gas Turbines to VTOL Aircraft W. Bloomfield May 7, 1959 2012-10-03
Forum 15 Some Notes on the Design of Prop-Rotors for Convertiplanes C. R. Haig Jr. May 7, 1959 2012-10-03
Forum 15 Development of the Quad Control System for VTOL Aircraft D. H. Kaplan May 7, 1959 2012-10-03
Forum 16 Increasing Helicopter Speeds E. L. Brown and Jan M. Drees May 11, 1960 2012-10-03
Forum 16 The Application of Tip Turbojets to the Solution of Design and Operating Problems of Large Helicopters John B. Nichols May 11, 1960 2012-10-03
Forum 16 Aerodynamic Efficiency Potentials of Rotary Wing Aircraft Evan A. Fradenburgh May 11, 1960 2012-10-03
Forum 16 Helicopter Range Extension Using Floating Wing Fuel Tanks Charles B. Fay May 11, 1960 2012-10-03
Forum 16 Economic and Operating Factors for the Rotodyne in Scheduled Passenger Operations David E. Postle May 11, 1960 2012-10-03
Forum 16 Operations - Federal Aviation Agency Programs in the Helicopter and V/STOL Fields Lt. Col. Frederick C. Goodwin, USA May 11, 1960 2012-10-03
Forum 16 Regulatory and Procedural Requirements for Helicopter Operations Major Hubert D. Gaddis, USA May 11, 1960 2012-10-03
Forum 16 Heliport Psychology Hal C. Conners May 11, 1960 2012-10-03
Forum 16 Impact Survival in Rotary Wing Military Aircraft Capt. William R. Knowles, MSC May 11, 1960 2012-10-03
Forum 16 An Operator's Viewpoint of Helicopter Safety J. C. Weadock May 11, 1960 2012-10-03
Forum 16 Armed Helicopters - A Forecast Lt. Col. John W. Oswalt, USA May 11, 1960 2012-10-03
Forum 16 Role of the Helicopter in the United States Air Force Lt. Col. O. B. O'Neill, USAF May 11, 1960 2012-10-03
Forum 16 Ground Effect Machine (GEM): Operational Problems Major Lester C. Robertson, USA and Major J. L. Wosser, USMC May 11, 1960 2012-10-03
Forum 17 Helicopter Noise, Its Evaluation and Treatment Harry Sternfeld Jr., and J. Everette Forehand May 3, 1961 2012-10-03
Forum 17 Basic Theories of Fatigue Failure and Their Design Implications Charles D. Nash Jr. May 3, 1961 2012-10-03
Forum 17 An Application of a Polyamide Epoxy Adhesive to Airframe Structural Components Raymond B. Krieger Jr. May 3, 1961 2012-10-03
Forum 17 Fundamentals of Rolling-Element Bearing Lubrication L. B. Sibley, F. K. Orcutt, and C. M. Allen May 3, 1961 2012-10-03
Forum 17 Evaluation of Some Rotor Hub Concepts Orin Brenning May 3, 1961 2012-10-03
Forum 17 New Techniques for Helicopter Reliability Control James A. Gean May 3, 1961 2012-10-03
Forum 17 Reliability and Maintainability Programs for Modern Helicopters and VTOL Aircraft George Powell and L. J. Geier May 3, 1961 2012-10-03
Forum 17 Helicopter Component Life and Reliability William Stieglitz May 3, 1961 2012-10-03
Forum 17 Overhaul on Condition - Eliminate Time Between Overhaul A. A. Coronato May 3, 1961 2012-10-03
Forum 17 Salt Water Ingestion by Gas Turbine Engines Ted F. Stirgwolt May 3, 1961 2012-10-03
Forum 17 What Has the Free Turbine Done for the Helicopter David Richardson May 3, 1961 2012-10-03
Forum 17 Service and Test Experience - Turbine Powered Helicopter Theodore L. Hoffmann and Charles C. Moore May 3, 1961 2012-10-03
Forum 17 The Practical Problems of Gas Turbine Operations in Helicopters Capt. David A. Spurlock, USMC May 3, 1961 2012-10-03
Forum 17 Design Consideration in Army Helicopter Colonel David B. Parker May 3, 1961 2012-10-03
Forum 17 An Analytical Study of Rotor Performance at High Forward Speeds Franklin D. Harris May 3, 1961 2012-10-03
Forum 17 Important Considerations Concerning Autorotation Handling Characteristics Charles M. Seibel May 3, 1961 2012-10-03
Forum 17 A Review of Current Helicopter Loads Research As Applied to the Problem of Rotor-Blade Fatigue Substantiation John F. Ward and LeRoy H. Ludi May 3, 1961 2012-10-03
Forum 18 The Hot Cycle Propulsion System Research Program K. B. Amer May 2, 1962 2012-10-03
Forum 18 Chemical Ice Protection for Helicopter Rotors and a Comparison with the Electrothermal System J. F. Van Wyckhouse May 2, 1962 2012-10-03
Forum 18 A Simplified Theory of Hingeless Rotors with Application to Tandem Helicopters Dr. M. I. Young May 2, 1962 2012-10-03
Forum 18 Longitudinal Dynamic Stability of a Helicopter with Torsionally Flexible Blades and Servo-Flap Control Hugh H. McIntyre May 2, 1962 2012-10-03
Forum 18 A Comparison of Detailed and Simplified Methods of Analysis on Rotor Stability in Forward Flight with Model Test Results H. J. deGarcia, and C. H. Perisho May 2, 1962 2012-10-03
Forum 18 Longitudinal Handling Qualities for Hovering E. Seckel, J. J. Traybar, and G. E. Miller May 2, 1962 2012-10-03
Forum 18 Delay of Rotor Blade Stall by Dynamic Tuning G. J. Sissingh May 2, 1962 2012-10-03
Forum 18 The Evaluation of Stability and Control Characteristics of Aircraft at Low Speeds Using Dynamically Similar Models in Semi-Free Flight H. C. Curtiss Jr., W. F. Putnam, and E. Martinez May 2, 1962 2012-10-03
Forum 18 Use of the Variable Stability and Control X-14A to Determine Attitude Control Power and Damping Requirements for a Visual Hovering Task in a VTOL Airplane L. Stewart Rolls, and Fred J. Drinkwater, III May 2, 1962 2012-10-03
Forum 18 An Investigation of VTOL Operational Problems Due to Downwash Effects Richard R. Pruyn and Leonard Goland May 2, 1962 2012-10-03
Forum 19 Second Harmonic Control Rodney K. Wernicke, and Jan M. Drees, Bell Helicopter Co. May 1, 1963 2012-10-03
Forum 19 Application of an Absorber to Reduce Helicopter Vibration Levels Charles W. Ellis, and Robert Jones, Kaman Aircraft Corp. May 1, 1963 2012-10-03
Forum 19 Loads Prediction for Structural Rigid Rotor Systems J. E. Rhodes, and John A. Gaidelis, Lockheed-California Co. May 1, 1963 2012-10-03
Forum 19 A Method for Determining the Fully Coupled Aeroelastic Response of Helicopter Rotor Blades Edward R. Wood, and Kurt D. Hilzinger, Sikorsky Aircraft Div. May 1, 1963 2012-10-03
Forum 19 A Linearized Theory for the Estimation of Helicopter Rotor Characteristics at Advance Ratios Above 1.0 Peter J. Arcidiacono, David S. Jenney and Arthur F. Smith, Research Laboratories, United Aircraft Corp. May 1, 1963 2012-10-03
Forum 19 High Speed Helicopter Rotor Design Jan M. Drees, Bell Helicopter Co. May 1, 1963 2012-10-03
Forum 19 VTOL Automatic Flight Control L. Kaufman, and E. R. Schultz, Kaman Aircraft Corp. May 1, 1963 2012-10-03
Forum 19 An Integrated Hydraulic Control System Combining Boost, Control Fuel, Stability Augmentation, and Gust Alleviation R. P. Carroll, C. J. Wirth, and F. L. Smith, Kaman Aircraft Corp. May 1, 1963 2012-10-03
Forum 19 Design Philosophy of the OH-5A Helicopter Sidney S. Sherby, Hiller Aircraft Co. May 1, 1963 2012-10-03
Forum 19 Research Flight Tests of the High Performance Iroquois Wesley L. Cresap and Robert R. Lynn, Bell Helicopter Co. May 1, 1963 2012-10-03
Forum 19 Design and Development of the Army XV-5A Lift Fan Powered V/STOL Aircraft H. B. Starkey, Ryan Aeronautical Co., and H. C. True, General Electric Co. May 1, 1963 2012-10-03
Forum 19 The Hummingbird Program E. B. Gibson, Lockheed-Georgia Co. May 1, 1963 2012-10-03
Forum 19 Results of the XH-51A Rigid Rotor Research Helicopter Program W. H. Statler, R. R. Heppe, and E. S. Cruz, Lockheed - California Co. May 1, 1963 2012-10-03
Forum 19 Future Development of the ASW Helicopter Lt. Commander Robert E. Schock, USN, USNATC, Patuxent River, Md. May 1, 1963 2012-10-03
Forum 19 Designing for Compatibility Harold S. Oakes, Sikorsky Aircraft Div. May 1, 1963 2012-10-03
Forum 19 Inertial Navigation Robert J. Holm, Litton Systems, Inc. May 1, 1963 2012-10-03
Forum 19 The Evolution of Doppler Navigation for Steep Gradient Aircraft John J. Bowden, Ryan Aeronautical Co. / Ryan Electronics May 1, 1963 2012-10-03
Forum 19 Helicopter Noise and Passive Defense C. R. Cox, Bell Helicopter Co. May 1, 1963 2012-10-03
Forum 19 Engineering Requirements for the Commercial Helicopter Robert L. Suggs, Petroleum Helicopters, Inc. May 1, 1963 2012-10-03
Forum 19 Partners in Progress - The Military and Commercial Helicopter M. Maxfield, Vertol Div., Boeing Co. May 1, 1963 2012-10-03
Forum 19 A Discussion of U. S. Army Aircraft Armament Program Major Donald J. Haid, Chief, U. S. Army Aviation Human Research Unit May 1, 1963 2012-10-03
Forum 19 Computed Induced Velocity, Induced Drag, and Angle of Attack Distributions for a Two-Bladed Rotor Raymond Piziali and Frank DuWaldt, Cornell Aeronautical Laboratory May 1, 1963 2012-10-03
Forum 19 Flight Test Experiences in Obtaining the First Commercial Certification of a Helicopter for True Vertical Takeoff and Landing Capability John Diamond and H. H. Moser, Vertol Div., Boeing Co. May 1, 1963 2012-10-03
Forum 19 Development and Test of the Bell OH-4A Light Observation Helicopter R. L. Lichten, Bell Helicopter Co. May 1, 1963 2012-10-03
Forum 19 Design, Development and Flight Test of P-1127 W. E. Gasich and G. Grogan, Norair Div., Northrop Corp. May 1, 1963 2012-10-03
Forum 19 Height Velocity Diagram Flight Test Project On The Bell 47G3B Helicopter T.W. Sanford, Jr., W.J. Hanley, and Gilbert De Vore May 1, 1963 2018-04-10
Forum 19 Height Velocity Diagram Flight Test Project On The Bell 47G3B Helicopter T.W. Sanford, Jr., W.J. Hanley, and Gilbert De Vore May 1, 1963 2018-04-10
Forum 20 Maneuverability Criteria for Weapons Helicopters David S. Jenney, Robert Decker, and Richard G. Stutz, Sikorsky Aircraft Div. May 13, 1964 2016-21-10
Forum 20 Maneuverability Criteria for Weapons Helicopters David S. Jenney, Robert Decker, and Richard G. Stutz, Sikorsky Aircraft Div. May 13, 1964 2012-10-03
Forum 20 Review of Helicopter Handling-Qualities Criteria and Summary of Recent Flight Handling-Qualities Studies Robert J. Tapscott, NASA May 13, 1964 2012-10-03
Forum 20 Advanced Rotary-Wing Handling Qualities Major Paul R. Curry and Mr. James T. Matthews Jr., USATRECOM May 13, 1964 2012-10-03
Forum 20 11th Air Assault Division Night Helicopter Operations Lt. Col. John B. Stockton, 11th Air Assault Aviation Group, Fort Benning, Ga. May 13, 1964 2012-10-03
Forum 20 Selected Army Aviation Problem Areas Major Joseph A. Gappa Jr., USABAAR, Fort Rucker, Ala. May 13, 1964 2012-10-03
Forum 20 European Helicopter Developments Robert R. Piper, TRECOM, Ft. Eustis, Va. May 13, 1964 2012-10-03
Forum 20 New Concepts in Helicopter and VTOL Transmission Systems J. Nelson Daniel, TRECOM, Ft. Eustis, Va. May 13, 1964 2012-10-03
Forum 20 Considerations Relating to Stopping a Rotor in Forward Flight P. W. Theriault, I. H. Culver, and L. Celniker, Lockheed-California Co. May 13, 1964 2012-10-03
Forum 20 A Summary of Hingeless-Rotor Research at NASA-Langley John F. Ward and Robert J. Huston, NASA May 13, 1964 2012-10-03
Forum 20 Helicopter Vibration Control by Cargo Isolation R. Gabel, D. A. Reed, Vertol Div. - Boeing Co., and R. F. Wilkus, WPAFB May 13, 1964 2012-10-03
Forum 20 A Pressurized Spar Inspection System Thomas P. Dixon, Sikorsky Aircraft Div. May 13, 1964 2012-10-03
Forum 20 Development of Rotor Blades with Extreme Chordwise and Spanwise Flexibility Richard R. Pruyn and Thomas G. Swales, Kellett Aircraft Corp. May 13, 1964 2012-10-03
Forum 20 Structural Behaviour of the Super Frelon in High Speed Flight F. L. Legrand, Sud Aviation May 13, 1964 2012-10-03
Forum 20 A New Technique for Steep Angle Approach Guidance Francis X. Kelly Jr., Airborne Instruments Laboratory May 13, 1964 2012-10-03
Forum 20 V/STOL Control-Display Subsystem Requirements Study R. W. Schwartz, WPAFB, and J. T. Shearer, Lear Siegler, Inc. May 13, 1964 2012-10-03
Forum 20 Design and Development of the Stability Augmentation System for the Lockheed/Army XV-4A Erwin A. Naumann, and Herman Schmier, Bendix Corp., Eclipse Pioneer Div. May 13, 1964 2012-10-03
Forum 20 Helipath, The Next Generation in Self-Contained Navigation J. C. Forrest, General Precision, Inc., GPL Div. May 13, 1964 2016-29-04
Forum 20 Helipath, The Next Generation in Self-Contained Navigation J. C. Forrest, General Precision, Inc., GPL Div. May 13, 1964 2012-10-03
Forum 20 Recent Developments in Simplifying and Improving the Tilt Wing Design Charles B. Fay, Vertol Div., Boeing Co. May 13, 1964 2012-10-03
Forum 20 Dassault Aircraft "Balzac V" Y. Thiriet, Generale Aeronautique Marcel Dassault May 13, 1964 2012-10-03
Forum 21 The XH-51A Rigid Rotor Compound Helicopter Program William K. Foulke, and J. Eric Rhodes, Lockheed-California Co. May 12, 1965 2012-10-03
Forum 21 Low-Speed Aerodynamic Flight Boundaries and Control Aspects of Tilt-Wing Aircraft Bernard L. Fry, Vertol Div., Boeing Co. May 12, 1965 2012-10-03
Forum 21 High Speed Helicopter Research With Jet Thrust Augmentation W. E. Blackburn, Kaman Aircraft Corp. May 12, 1965 2012-10-03
Forum 21 Model and Full Scale Compound Helicopter Research Evan A. Fradenburgh, and Richard M. Segel, Sikorsky Aircraft Div. May 12, 1965 2012-10-03
Forum 21 Rotor Performance in the Light of Recent Advances in Aerodynamics Methodology Franklyn J. Davenport, Vertol Div., Boeing Co. May 12, 1965 2012-10-03
Forum 21 An Analytical Study of the Dynamics of VTOL Aircraft in Unsteady Flight H. C. Curtiss Jr., Princeton University May 12, 1965 2012-10-03
Forum 21 Effects of Blade Stall on Helicopter Rotor Blade Bending Loads Kenneth B. Amer, and Sally LaForge, Hughes Tool Co., Aircraft Div. May 12, 1965 2012-10-03
Forum 21 Research on Factors Influencing Handling Qualities for Precision Hovering and Gun Platform Tasks James W. Clark, and David P. Miller, United Aircraft Research Laboratories May 12, 1965 2012-10-03
Forum 21 The Role of Cost/Effectiveness in V/STOL Combat Systems Development J. J. Schneider, L. L. Leisher, and S. A. Marciniec, Vertol Div., Boeing Co. May 12, 1965 2012-10-03
Forum 21 Models in Cost-Effectiveness Analysis: An Example Oliver Bryk, Research Analysis Corp. May 12, 1965 2012-10-03
Forum 21 Cost Effectiveness Optimization During System Definition and Development John A. Lockerd, Bell Helicopter Co. May 12, 1965 2012-10-03
Forum 21 Some Consideration in the Design of a Large Single Rotor Helicopter Power Transmission System Lester R. Burroughs and James L. Lastine, Sikorsky Aircraft Div. May 12, 1965 2012-10-03
Forum 21 A Study of the Turbine Integrated Geared Rotor for the Heavy-Lift Helicopter Robert B. Bossler Jr., Kaman Aircraft Corp. May 12, 1965 2012-10-03
Forum 21 High-Speed Helicopters and Compounds in Maneuvers and Gusts J.M. Drees and M.J. McGuigan, Bell Helicopter Co. May 12, 1965 2012-10-03
Forum 21 IFR Certification of the Sikorsky S-61L/N Helicopter Robert S. Decker, Sikorsky Aircraft Div. May 12, 1965 2012-10-03
Forum 21 Helicopter Instrument Operations in Terminal Areas Alder P. Betti, Flight Standards Service May 12, 1965 2012-10-03
Forum 21 Research Pictorial Flight Displays for Full IFR Rotary Wing Flight D. J. Dougherty, Bell Helicopter Co. May 12, 1965 2012-10-03
Forum 21 The "Guide Lite" System David H. Kaplan, Burroughs Corp. May 12, 1965 2012-10-03
Forum 21 Project Red Dog Chester R. Mead, Major Signal Corps, 11th Air Assault Div. May 12, 1965 2012-10-03
Forum 21 British Experience of the Tropical Testing of Helicopters G.F. Langdon, Aeroplane and Armament Experimental Establishment May 12, 1965 2012-10-03
Forum 21 Pilot Report on XV-5A Fan Mode Handling Qualities W.L. Everett, Ryan Aeronautical Co. May 12, 1965 2012-10-03
Forum 21 Special Features of the CH-53A Aircraft Systems and Test Requirement Charles M. Echeverria, Sikorsky Aircraft Div. May 12, 1965 2012-10-03
Forum 21 Abusive Testing of Turboshaft Engines Gerhard Sonder, General Electric Co. May 12, 1965 2012-10-03
Forum 21 Results of Army YCH-54A Heavy Lift Helicopter Field Experience Associated With the 11 Air Assault Division (Test) Joe D. Ecrette, Major, United States Army May 12, 1965 2012-10-03
Forum 21 The 200+ Knot Flight Research UH-1B W. L. Cresap, John Duhon, R. R. Lynn, and J. Van Wyckhouse, Bell Helicopter Co. May 12, 1965 2012-10-03
Forum 22 The USAF CH-3C Helicopter V/STOL In-Flight Refueling Program and Its Operational Uses and Implications Harry P. Dunn, Captain, USAF May 11, 1966 2012-10-03
Forum 22 Experimental Boundary Layer Study on Hovering Rotors W. H. Tanner, Bell Helicopter Co; P. F. Yaggy, Ames Research Center May 11, 1966 2012-10-03
Forum 22 Airfoil Sections for Helicopter Rotors - A Reconsideration Franklyn J. Davenport, and John V. Front, Boeing Co., Vertol Div. May 11, 1966 2012-10-03
Forum 22 S-61F Flight Research Program Phillip D'Ostilio, Sikorsky Aircraft Div. May 11, 1966 2012-10-03
Forum 22 Helicopter Rotor Blade Radar Antenna Hugh W. Upton, Bell Helicopter Co. May 11, 1966 2012-10-03
Forum 22 To Fly a Helicopter to the Terminal in Bad Weather Lcdr R. E. Goodspeed, U. S. Navy May 11, 1966 2012-10-03
Forum 22 Systems Integration in Helicopters Thomas H. Sanders, Boeing Co., Vertol Div. May 11, 1966 2012-10-03
Forum 22 The IHAS Flight Control System James P. Murphy, Teledyne Systems Co; Horace Welk, U. S. Naval Air Development Center; Louis Cotton, Sikorsky Aircraft Div. May 11, 1966 2012-10-03
Forum 22 Flying Qualities of the XV-5A V/STOL Aircraft Major William L. Welter, U. S. Army Aviation Test Activity May 11, 1966 2012-10-03
Forum 22 Control Requirements and Operating Characteristics of Lift Engine Transports in Low Speed Flight Robert C. Baker, Sikorsky Aircraft Div. May 11, 1966 2012-10-03
Forum 22 Flight Control Influence on VTOL Handling Qualities W. L. Holladay, North American Aviation, Inc. May 11, 1966 2012-10-03
Forum 22 An Analytical Study of Helicopter Handling Qualities in Hover Richard P. Walton, and Robert L. Stapleford, Systems Technology, Inc. May 11, 1966 2012-10-03
Forum 22 Single Rotor Helicopter Transient Following a Power Failure at High Speeds Knute C. Hansen, Sikorsky Aircraft Div. May 11, 1966 2012-10-03
Forum 22 Fail Safe Structural Features of the Hughes OH-6A Helicopter H. G. Smith, Hughes Tool Co. May 11, 1966 2012-10-03
Forum 22 Concepts and Techniques for Helicopter Airframe Fatigue Tests Walter A. Lane, Sikorsky Aircraft Div. May 11, 1966 2012-10-03
Forum 22 The Dynamic Antiresonant Vibration Isolator William G. Flannelly, Kaman Aircraft Corp. May 11, 1966 2012-10-03
Forum 22 Problem Trends in External Cargo Transport by Heavy-Lift Helicopters Meade H. Mitchell Jr., and Jules A. Vichness, U.S. Army Aviation Material Laboratories May 11, 1966 2012-10-03
Forum 22 Future Requirements for Military Vertical Replenishment and Utility Helicopters Lcdr S. A. Coakley, and Lcdr C. D. VanGundy, USN May 11, 1966 2012-10-03
Forum 22 Commercial External Load Operation With the Vertol 107 Helicopter John B. Conley, New York Airways, Inc. May 11, 1966 2012-10-03
Forum 22 The Influence of External Loading on the Design of a Helicopter Robert J. Tynan, and Gordon A. Buchmiller, Sikorsky Aircraft Div. May 11, 1966 2012-10-03
Forum 22 Qualitative Commentary on Tandem Helicopter External Cargo Sling Operation A. J. Hutto, The Boeing Co., Vertol Div. May 11, 1966 2012-10-03
Forum 22 Technical Development of the SA 330 Rene Mouille, Sud-Aviation May 11, 1966 2012-10-03
Forum 22 Experimental Study on the Unsteady Aerodynamics of a Tandem Rotor Operating in the Vortex Ring State Kyuichiro Washizu, and Akira Azuma, University of Tokyo; Jiro Koo and Toichi Oka, National Aerospace Laboratory May 11, 1966 2012-10-03
Forum 22 VJ-101C -- Supersonic VTOL Program George L. Bright, Entwicklungsring S?d GmbH May 11, 1966 2017-23-02
Forum 22 VJ-101C -- Supersonic VTOL Program George L. Bright, Entwicklungsring S?d GmbH May 11, 1966 2012-10-03
Forum 22 A Low Altitude Control Concept For U.S. Army Rotary Wing Aircraft Otto H. Schoenberger, US Army Electronics Command, Avionics Laboratory; W.T. Robertson, Sperry Phoenix Company May 11, 1966 2018-10-10
Forum 23 Determination of Helicopter Rotor Blade Compressibility Effects-Prediction Vs. Flight Test Norman, David C. and Somsel, John R., U.S. Air Force May 10, 1967 2012-23-07
Forum 23 Aerodynamic Considerations of Stopping a Rotor in Flight Prouty, R. W. and Donham, R. E., Lockheed-California Company May 10, 1967 2012-23-07
Forum 23 Avionics for the Light Observation Helicopter Wilkins, F. W., Sylvania Electronics Systems May 10, 1967 2012-23-07
Forum 23 Evaluation of Two Instrument-Landing Displays in Simulated IFR Approaches with a Helicopter Gracey, William, NASA May 10, 1967 2012-23-07
Forum 23 Electrostatic Discharging Systems for Helicopters - A Review of the State of the Art De La Cierva, Juan, Dynasciences Corporation May 10, 1967 2012-23-07
Forum 23 The Effects of Flight Dynamics on Rotor Blade Antenna Performance Gruber, Robert and Woltornist, Victor, Lockheed Electronics Company May 10, 1967 2012-23-07
Forum 23 Emergency Lift and Autorotational Boost Systems for Single Engine Helicopters Kelley, Archie P., The Garrett Corporation May 10, 1967 2012-23-07
Forum 23 Bending Strength of Spur Gear Teeth McIntyre, W. L. and Malot, R. C., Allison (General Motors); Givens, E. R., USAAVLABS May 10, 1967 2012-23-07
Forum 23 Increased Helicopter Capability Through Advanced Powerplant Technology Kailos, Nicolas C., U.S. Army May 10, 1967 2012-23-07
Forum 23 Structural Development the of XV-9A Hot Cycle Research Aircraft Smith Jr., H. G., Hughes Tool Company May 10, 1967 2012-23-07
Forum 23 A Comparison of Fatigue Life and Reliability from Constant and Variable Amplitude Loading Test Davis, Caleb S. and Young, Louis, Lockheed May 10, 1967 2012-23-07
Forum 23 Helicopter Cargo Restraint Vichness, Jules A. and House, Thomas L., U.S. Army May 10, 1967 2012-23-07
Forum 23 The Army CH-54A in RVN, HLH on the Move Rickmeyer, Jaros C., Flying Cranes May 10, 1967 2012-23-07
Forum 23 Optimum Use of Contingency Power Rating for Increasing Permissible Operating Gross Weight in Twin-Turbine Helicopters Nesbitt, E. J. and Montanaro, J.O., Sikorsky Aircraft May 10, 1967 2012-23-07
Forum 23 Suppression of Transmitted Harmonic Rotor Loads by Blade Pitch Control Daughaday, H., Cornell; McIntyre, H. H., Kaman May 10, 1967 2012-23-07
Forum 23 An Analysis of the Stall Flutter Instability of Helicopter Rotor Blades Carta, Franklin O., United Aircraft; Ham, Norman D., Massachusetts Institute of Technology May 10, 1967 2012-23-07
Forum 23 Stall Flutter of Helicopter Rotor Blades : A Special Case of the Dynamic Stall Phenomenon Norman D. Ham, Massachusetts Institute of Technology May 10, 1967 2019-25-02
Forum 23 The Influence of Blade Flapping Restraint on the Dynamic Stability of Low Disk Loading Propeller-Rotor Young, Maurice I., Advanced Technology; Lytwyn, Roman T. May 10, 1967 2012-23-07
Forum 23 Control Loads and Their Effects on Fuselage Vibrations Kidd, D. L, and Spivey, R. F., Bell Helicopter Company; Lawrence, K. L., University of Texas at Arlington May 10, 1967 2012-23-07
Forum 23 Comments on "Effects of Control Loads on Fuselage Vibration by D. Kidd, R. Spivey, K. Lawrence" Kenneth C. Mard, Sikorsky Aircraft May 10, 1967 2019-25-02
Forum 23 Response Characteristics of the Gyro-Controlled Lockheed Rotor System Sissingh, G. J., Lockheed-California Company May 10, 1967 2012-23-07
Forum 23 AAFSS (AH-56A) Application Of A Fully Integrated Avionics Aircrafts Weapons System George W. Hogelin, Avionics Laboratory AMSEL-YL-S, USA ECOM; Thomas W. Hancock, Lockheed-California Company May 10, 1967 2018-10-10
Forum 24 Development And Test Of The BO 105 Rigid Rotor Helicopter Emil F. Weiland May 8, 1968 2015-25-01
Forum 24 Status Report On Design Development Of The AH-56A Cheyenne P. W. Theriault May 8, 1968 2015-25-01
Forum 24 Blade Tip Aerodynamics-Profile And Planform Effects Richard F. Spivey May 8, 1968 2015-25-01
Forum 24 Dynamic Stall Of Airfoil Sections For High-Speed Rotors Jaan Liiva; Franklyn J. Davenport May 8, 1968 2019-17-12
Forum 24 Dynamic Stall Of Airfoil Sections For High-Speed Rotors Jaan Liiva; Franklyn J. Davenport May 8, 1968 2015-25-01
Forum 24 Model Studies Of Helicopter Rotor Flow Patterns In A Water Tunnel August F. Lehman May 8, 1968 2015-25-01
Forum 24 Model Studies Of Helicopter Rotor Flow Patterns In A Water Tunnel August F. Lehman May 8, 1968 2022-24-02
Forum 24 High-Speed Rotor Performance Correlation Vincent M. Paglino May 8, 1968 2015-25-01
Forum 24 Helicopter Rotor Noise Prediction And Control Ronald G. Schlegel; William E. Bausch May 8, 1968 2015-25-01
Forum 24 A Special Gas Turbine Cycle For The Compound Helicopter J. B. Nichols May 8, 1968 2015-25-01
Forum 24 An Analytical Approach To The Determination Of Particle Trajectories In A S-Bend Duct With Experimental Verification Murray I. Leitner May 8, 1968 2015-25-01
Forum 24 Allison T63 Regenerative Engine Program Edward J. Privoznik May 8, 1968 2015-25-01
Forum 24 The Toroidal Rotary Regenerator For Gas-Turbine Engines Henry J. Selfors May 8, 1968 2015-25-01
Forum 24 Helicopter Engine Augmentation Systems For Hot Day Altitude And Emergency Power Denis P. Edkins May 8, 1968 2015-25-01
Forum 24 Operational Experience With T53 Engines In U.S. Army Helicopters Michael S. Saboe; Max L. Kleiner May 8, 1968 2015-25-01
Forum 24 Flight Investigation Of The Wing-Rotor Lift-Sharing Characteristics Of A Hingeless Rotor Compound Helicopter Perry L. Deal; Julian L. Jenkins Jr. May 8, 1968 2015-25-01
Forum 24 Flying Qualities Considerations In The Design And Development Of The Hueycobra C. L. Livingston; M. R. Murphy May 8, 1968 2015-25-01
Forum 24 Handling Qualities With The Bolkow Rigid Rotor System G. Reichert; P. Oelker May 8, 1968 2015-25-01
Forum 24 Vtol Handling Qualities Criteria And Control Requirements-Analysis And Experiment Thomas E. Lollar; Gerhard K. L. Kriechbaum May 8, 1968 2015-25-01
Forum 24 Control Characteristics Of Vectored Thrust V/Stol Vehicles In The Transition Regime Alan V. Coles May 8, 1968 2015-25-01
Forum 24 An Analysis Of Blade-Motion Stability For An Articulated Rotor Julian L. Jenkins Jr. May 8, 1968 2015-25-01
Forum 24 The Effect Of Positive Pitch-Flap Coupling (Negative 3) On Rotor Blade Motion Stability And Flapping Troy M. Gaffey May 8, 1968 2015-25-01
Forum 24 A Self-Excited Rotor Blade Oscillation At High Subsonic Mach Numbers William F. Paul May 8, 1968 2015-25-01
Forum 24 Instabilities Associated With A Rotor Blade Stopped In Flight Richard P. White Jr. May 8, 1968 2015-25-01
Forum 24 Test Approaches To External Sling Load Instabilities Richard Gabel; Gregory J. Wilson May 8, 1968 2015-25-01
Forum 24 Resume Of United States Army Helicopter Operations In Vietnam William R. Watson Jr.; John R. Dunham Jr. May 8, 1968 2015-25-01
Forum 24 Integrated Operations Of Marine Corps Light, Medium And Heavy Helicopters In Vietnam U. W. Shadrick; W. R. Maloney; M. E. Edwards May 8, 1968 2015-25-01
Forum 24 Experimental Flight Tests Of The 300 MPH XH-51A Compound Helicopter W. E. Spreuer May 8, 1968 2015-25-01
Forum 24 Experience Of And Methods To Be Used In Clearing A Jet-Lift Aircraft For Service Use Ian A. Fisher May 8, 1968 2015-25-01
Forum 24 NONE NONE May 8, 1968 2015-25-01
Forum 24 NONE NONE May 8, 1968 2015-25-01
Forum 24 An Analysis Of Blade-Motion Stability For An Articulated Rotor Julian L. Jenkins Jr. May 8, 1968 2015-25-01
Forum 25 The Last Word In Vertability NONE May 14, 1969 2015-25-01
Forum 25 Validation Of Ground Based Simulation John B. Sinacori May 14, 1969 2015-25-01
Forum 25 Tail Rotor Design Part I - Aerodynamics R. R. Lynn; F. D. Robinson; N. N. Batra; J. M. Duhon May 14, 1969 2015-25-01
Forum 25 Measurement And Evaluation Of Helicopter Flight Loads Spectra Data John D. Porterfield; William T. Alexander May 14, 1969 2015-25-01
Forum 25 Performance Aspects Of Folding Proprotor V/Stol Aircraft F. V. Engle; K. W. Sambell May 14, 1969 2015-25-01
Forum 25 VFW-H3 "Sprinter"—A Semi-Compound With Pneumatic Rotor Drive Christoph Fischer May 14, 1969 2015-25-01
Forum 25 A Self-Monitored Stability Augmentation System For The CX-84 V/Stol Aircraft C. D. Griffith; V. M. Crosby May 14, 1969 2015-25-01
Forum 25 Terrain Following/Terrain In Avoidance Flight With The AH-56A Vehicle S. B. Ohrenstein; R. D. Lane May 14, 1969 2015-25-01
Forum 25 A-V-I-A-R-M-F-I-C-S Avionics-Armament-Fire Control System For The Cheyenne Weapon System Larry S. Klivans; David Baskind May 14, 1969 2015-25-01
Forum 25 An Integrated Display Concept For Helicopters And Vtol Aircraft* Theodor A. Dukes May 14, 1969 2015-25-01
Forum 25 Rotor Blade Radar In The Helicopter Multifunction Role Hubert W. Upton; Christian H. Witzke, III May 14, 1969 2015-25-01
Forum 25 A Computer Model For The Evaluation Of Helicopter Fire Control Systems John Elwell; George Mathewson May 14, 1969 2015-25-01
Forum 25 New Experimental Techniques In Rotorcraft Aerodynamics And Their Application W. H. Tanner; R. M. Wohlfeld May 14, 1969 2015-25-01
Forum 25 The Free Wake Analysis A Method For The Prediction Of Helicopter Rotor Hovering Performance. David R. Clark; Albert C. Leiper May 14, 1969 2015-25-01
Forum 25 Prediction Of Inflight Stalled Airloads From Oscillating Airfoil Data David W. Gross; Franklin D. Harris May 14, 1969 2015-25-01
Forum 25 Prediction Of Inflight Stalled Airloads From Oscillating Airfoil Data David W. Gross; Franklin D. Harris May 14, 1969 2020-21-04
Forum 25 Three-Dimensional Potential Flow Past The Surface Of A Rotor Blade Robert Sopher May 14, 1969 2015-25-01
Forum 25 The Design And Performance Prediction Of Propeller/Rotors For Vtol Applications John P. Magee; Martin D. Maisel; Frank J. Davenport May 14, 1969 2015-25-01
Forum 25 Propulsion Requirements For A Heavy-Lift Helicopter System R. J. Sullivan; B. A. Bachmann May 14, 1969 2015-25-01
Forum 25 A Family Of Advanced Turboshaft Engines W.L. Rodenbaugh May 14, 1969 2015-25-01
Forum 25 Helicopter Engine Dynamic Analysis Thomas Ress Warwick May 14, 1969 2015-25-01
Forum 25 Convertible Fan/Shaft Engines Michael E. Seery May 14, 1969 2015-25-01
Forum 25 The Influence Of Propulsion Systems On Extremely Large Helicopter Design J.J. Schneider May 14, 1969 2015-25-01
Forum 25 On The Dynamics Of Lifting Rotors With Thrust Or Tilting Moment Feedback Controls Raymond L. Johnson; Kurt H. Hohenemser May 14, 1969 2015-25-01
Forum 25 Dynamics Of Lifting Rotors With Thrust And Tilting Moment Feedback Controls K. H. Hohenemser; R. L. Johnson May 14, 1969 2015-25-01
Forum 25 A Comparison Of Dynamically Scaled Model Rotor Test Data With Discrete Azimuth Aeroelastic Stability Theory Charles F. Niebanck May 14, 1969 2015-25-01
Forum 25 A Comparison Of Dynamically Scaled Model Rotor Test Data With Discrete Azimuth Aeroelastic Stability Theory Norman D. Ham; Wayne Johnson May 14, 1969 2015-25-01
Forum 25 Tail Rotor Design Part Ii - Structural Dynamics R. W. Balke; R.L. Bennett; T. M. Gaffey; R. R. Lynn May 14, 1969 2015-25-01
Forum 25 Discussion By Dr. R. Carlson, Sikorsky Aircraft Of The Paper "Tail Rotor Design, Part II - Structural Dynamics" Lynn; Blake; Bennett; Gaffey May 14, 1969 2015-25-01
Forum 25 A Vector Airspeed Measuring System (Vams)* For Helicopters And Other V/Stol Aircraft E. J. Durbin; G. Born; R. Vause May 14, 1969 2015-25-01
Forum 25 Helicopter Noise Reduction And Its Effects On Operations C. R. Cox May 14, 1969 2015-25-01
Forum 25 The Development Of An Improved Method Of Conducting Height-Velocity Testing On Rotary Wing Aircraft John J. Shapley Jr.; Kenneth R. Ferrell; Robert A. Kyker May 14, 1969 2015-25-01
Forum 25 Development And Evaluation Of The Main Rotor Bifilar Absorber William F. Paul May 14, 1969 2015-25-01
Forum 25 Development Of Vtol Flying And Handling Qualities Requirements Using The Mission Task Performance Oriented Approach H. P. Harper; W. Sardanowsky; R. Scharpf May 14, 1969 2015-25-01
Forum 25 Flight Simulation Of The CH-46 Helicopter Bruce B. Blake; Nicholas Albion; Robert C. Radford May 14, 1969 2015-25-01
Forum 25 Development Of A Flying Qualities Specification For Military V/Stol Aircraft George H. Saunders; Charles R. Chalk May 14, 1969 2015-25-01
Forum 25 Fatigue Properties And Test Procedures Of Glass Reinforced Plastic Rotorblades E. Jarosch; A. Stepan May 14, 1969 2015-25-01
Forum 25 Stress Measurements In The Gear Teeth And Fatigue Strength Of Highly Loaded Gears F. Liard May 14, 1969 2015-25-01
Forum 25 A Simplified Empirical Method For Rotor Component Fatigue Design G. L. Garham; M. J. McGuigan May 14, 1969 2015-25-01
Forum 25 Development Of Fatigue Test Loading Spectra For Certification Of Helicopters Louis Young May 14, 1969 2015-25-01
Forum 25 Development Of The OH-6A Drive System For Rvn Load Spectrums Harold W. Ferris May 14, 1969 2015-25-01
Forum 25 Comparison Of Helicopter Combat Environments To Structural Criteria Requirements W. P Brown; E. P. Roeser May 14, 1969 2015-25-01
Forum 25 Fail-Safe Vs. Safe-Life Philosophy In V/Stol Design Fred H. Immen May 14, 1969 2015-25-01
Forum 25 Comparison Of A Mechanical Fatigue Life Indicator And A Resistance Type Fatigue Life Indicator Richard C. Rapson Jr.; Henry R. Velkoff May 14, 1969 2015-25-01
Forum 25 Technical Program And Exhibit Guide NONE May 14, 1969 2015-25-01
Forum 26 Metropolitan Air Transit System A. E. Andreoli, Calif. State Polytechnic College June 16, 1970 2012-10-03
Forum 26 Helicopter Structural Weight Prediction and Evaluation Theory vs Statistics H. G. Smith, Hughes Tool Co., Aircraft Div. June 16, 1970 2012-10-03
Forum 26 Noise Radiation From Helicopter Rotors Operating at High Tip Mach Numbers R. E. A. Arndt, Pennsylvania State University, and D. C. Borgman, U. S. Army Aeronautical Research Laboratory June 16, 1970 2012-10-03
Forum 26 The Application of Hingeless Rotors to Tilting Prop Rotor Aircraft D. A. Richardson, Boeing/Vertol June 16, 1970 2012-10-03
Forum 26 Airborne and Ground Resonance of Hingeless Rotors R. T. Lytwyn, and W. Miao, Boeing/Vertol, and W. Woitsch, Messerschmitt-Boelkow, GmbH June 16, 1970 2012-10-03
Forum 26 A Theoretical Method for Rotor Blade Flutter in Forward Flight K. W. Shipman, and E. R. Wood, Georgia Institute of Technology June 16, 1970 2012-10-03
Forum 26 Application of the Floquet Transition Matrix to Problems of Lifting Rotor Stability D. A. Peters, McDonnell-Douglas Corp., and Prof. K. H. Hohenemser, Washington University June 16, 1970 2012-10-03
Forum 26 Analytical Study of Helicopter Rotor Stall Flutter F. O. Carta, L. M. Casellini, P. J. Arcidiacono, United Aircraft Research Lab., and H. L. Elman, Sikorsky Aircraft Div. June 16, 1970 2012-10-03
Forum 26 Recent Advances in Helicopter Vibration Control D. L. Kidd, R. W. Balke, R. L. Wernicke, and W. F. Wilson, Bell Helicopter Co. June 16, 1970 2012-10-03
Forum 26 Helicopter Rotor Periodic Differential Pressures and Structural Response Measured in Transient and Steady-State Maneuvers J. F. Ward, NASA-Langley Research Center June 16, 1970 2012-10-03
Forum 26 New Insights Into Swept Tip Rotor Blade Design W. A. Spivey, Bell Helicopter Co.; and G. G. Morehouse, USAARL, Ames Research Center June 16, 1970 2012-10-03
Forum 26 A Study of Rotor Blade-Vortex Interaction Prof. B. W. McCormick Jr., Pennsylvania State University; and M. Surendraiah, Segner & Dalton June 16, 1970 2012-10-03
Forum 26 Dynamic Stall of Helicopter Blades L. E. Ericsson and J. P. Reding, Lockheed Missiles and Space Co. June 16, 1970 2012-10-03
Forum 26 Avionics, The Key to the Future of Army Aviation Maj. W. H. Maloney, U. S. Army CDCAA June 16, 1970 2012-10-03
Forum 26 Night Observation and Weapons Fire Control System R. J. Walker, Emerson Electric Co. June 16, 1970 2012-10-03
Forum 26 An Investigation of Heavy Lift Helicopter Display Problems A. T. Sherbert Jr., Boeing/Vertol June 16, 1970 2012-10-03
Forum 26 Miniature Laser Obstacle Warning Systems for Helicopters H. D. Eckhardt, RCA-Aerospace Systems Div.; and N. A. Luce, Quantel Opto-Electronic Systems, Inc. June 16, 1970 2012-10-03
Forum 26 Millimeter Radar for Landing Applications Dr. L. Kosowsky and K. Koester, Norden Div., UAC June 16, 1970 2012-10-03
Forum 26 A Simplified Study of High Speed Autorotation Entry Characteristics H. H. McIntyre, Kaman Aerospace Corp. June 16, 1970 2012-10-03
Forum 26 Control of Large Crane Helicopters D. S. Jenney, and L. S. Szustak, Sikorsky Aircraft Div. June 16, 1970 2012-10-03
Forum 26 Stability and Control Considerations for a Tilt-Fold-Proprotor Aircraft F. E. Tiller, Bell Helicopter Co., and R. Nicholson, Air Force Flight Dynamics Laboratory, WPAFB June 16, 1970 2012-10-03
Forum 26 Prediction of the Stability Derivatives of Large Flexible Proprotors by a Simple Analysis R. R. Pruyn, and J. P. Magee, Boeing/Vertol June 16, 1970 2012-10-03
Forum 26 Analysis of VTOL Transition Dynamics D. L. Key, Cornell Aeronautical Laboratory, Inc. June 16, 1970 2012-10-03
Forum 26 Combat Operational Flight Profiles on UH-1C, AH-1G, and UH-1H Helicopters G. L. Graham, Bell Helicopter Co. June 16, 1970 2012-10-03
Forum 26 Collection and Analysis of Helicopter Combat Flight Loads Data From AH-1G Helicopters in Southeast Asia F. J. Giessler, and J. F. Braun, Technology Inc.; and W. T. Alexander Jr., AVLABS June 16, 1970 2012-10-03
Forum 26 Simplified Procedures for Estimating Flapwise Bending Moments on Helicopter Rotor Blades A. J. Landgrebe, United Aircraft Research Laboratories June 16, 1970 2012-10-03
Forum 26 The Development of an Advanced Composite Tail Rotor Driveshaft H. Zinberg, Bell Helicopter Co.; and M. F. Symonds, Whittaker Corp., ASD June 16, 1970 2012-10-03
Forum 26 The Development of a Fiberglass Main Rotor Blade for the CH-47C Helicopter R. J. Spitko, Boeing/Vertol; and H. Young, AVLABS June 16, 1970 2012-10-03
Forum 26 The CH-47 Cruise Guide Indicator H. H. Steinmann, Boeing/Vertol June 16, 1970 2012-10-03
Forum 26 Power Available Calculation Procedures and Operational Aspects of a Tip-Jet-Propelled Rotor System B. A. Bachmann, Hughes Tool Co., Aircraft Div. June 16, 1970 2012-10-03
Forum 26 Optimization Study for VTOL Aircraft Powerplants W. J. McIntire and D. S. Monson, Allison Div., GM Corp. June 16, 1970 2012-10-03
Forum 26 Preliminary Design and Performance Analysis of an Advanced Convertible Fan/Shaft Engine for V/STOL Tactical and Transport Aircraft J. N. Tulino, P. C. Bosse, and W. H. Wiley, Pratt and Whitney Aircraft, Florida R&D Center June 16, 1970 2012-10-03
Forum 26 Design Optimization of a V/STOL 5000 HP Engine T. A. Dickey, and P. G. Schwaar, Avco Lycoming Div. June 16, 1970 2012-10-03
Forum 26 Aerodynamic Parameters That Affect Compressor Erosion in Gas Turbine Engines R. M. Wood, Allison Div., GM Corp.; and R. M. Gaertner, NASC June 16, 1970 2012-10-03
Forum 26 HucyCobra Maneuvering Investigations R. B. Lewis, II, U. S. Army ASTA June 16, 1970 2012-10-03
Forum 26 Airborne Flight Test Data Acquisition and Automatic Data Processing System for Helicopter Test and Development Program F. Kreutz, Sikorsky Aircraft Div. June 16, 1970 2012-10-03
Forum 26 Model Testing to Establish Ditching and Flotation Stability Characteristics of Helicopters J. C. Kidwell, Bell Helicopter Co.; and W. A. Crago, British Hovercraft Co. June 16, 1970 2012-10-03
Forum 26 Report on Flight Test of a Two-Point External Load Suspension System A. J. Hutto, Boeing/Vertol June 16, 1970 2012-10-03
Forum 26 Application of Vortex Visualization Test Techniques to Rotor Noise Research R. H. Spencer, Boeing/Vertol June 16, 1970 2012-10-03
Forum 27 Army Helicopter Performance Trends R. B. Lewis II, USAASTA May 19, 1971 2012-08-03
Forum 27 Full-Scale Proprotor Development K. G. Wernicke, and H. K. Edenborough, Bell Helicopter Co. May 19, 1971 2012-08-03
Forum 27 Horizontal Stoppable Rotor Conversion G. A. Watts, Lockheed-Calif. Co., and J. C. Biggers, NASA May 19, 1971 2012-08-03
Forum 27 HLH Primary Flight Control System Design Richard W. Sanford, Peter R. Venuti, Derek Wood, Boeing / Vertol May 19, 1971 2012-08-03
Forum 27 Development of the ABC Rotor R. K. Burgess, Sikorsky Aircraft May 19, 1971 2012-08-03
Forum 27 The Application of a Lifting Surface Theory to the Calculation of Helicopter Airloads W. Johnson, MIT May 19, 1971 2012-08-03
Forum 27 A Study of the Effects of Non-Uniform Swash-Plate Stiffness and Out-of-Blade Track on Rotor Dynamics and Stability V. J. Piarulli, RASA May 19, 1971 2012-08-03
Forum 27 The Method of Multiblade Coordinates in the Linear Analysis of Lifting Rotor Dynamic Stability and Gust Response at High Advance Ratio K. H. Hohenemser and S. K. Yin, Washington Univ. May 19, 1971 2012-08-03
Forum 27 Prediction of Control Loads Due to Blade Stall F. J. Tarzanin Jr., Boeing / Vertol May 19, 1971 2012-08-03
Forum 27 Preliminary Development of an Active Transmission Isolation System P. W. Von Hardenberg, and P. B. Saltanis, Sikorsky Aircraft May 19, 1971 2012-08-03
Forum 27 Analytical Investigation of the Effects of Blade Flexibility, Unsteady Aerodynamics, and Variable Inflow on Helicopter Rotor Stall Characteristics E. D. Bellinger, UARL May 19, 1971 2012-08-03
Forum 27 Detailed Aerodynamic Measurements on a Model Rotor in the Blade Stall Regime or Why at = 240 R. K. Fisher Jr., Boeing / Vertol, and W. J. McCroskey, USAAMR&D Lab May 19, 1971 2012-08-03
Forum 27 Tip Vortices-Velocity Distributions Dr. N. A. Chigier, and V. R. Corsiglia, NASA-Ames May 19, 1971 2012-08-03
Forum 27 A Method for Predicting Helicopter Wake Geometries, Wake-Induced Flow and Wake Effects on Blade Loads S. G. Sadler, RASA May 19, 1971 2012-08-03
Forum 27 Forward Flight Performance of a Coaxial Rigid Rotor V. M. Paglino, Sikorsky Aircraft May 19, 1971 2012-08-03
Forum 27 Day and Night Firepower of the Cheyenne B. J. Merritt, USAAMC and J. C. Kirby, Lockheed-Calif. May 19, 1971 2012-08-03
Forum 27 An Attack Helicopter Weapons Delivery Computer J. A. Simpson, Norden Div., UAC May 19, 1971 2012-08-03
Forum 27 Head-Mounted Display/Control System in V/STOL Operations D. D. Strother and H. W. Upton, Bell Helicopter Co. May 19, 1971 2012-08-03
Forum 27 AN/ASN-86 Inertial Navigation Set R. Creed, USA Electronics Command, and J. B. Hughes, Guidance & Control Div., Litton Industries May 19, 1971 2012-08-03
Forum 27 The Night Rescue Terminal Navigation Problem C. S. Richardson, Sikorsky Aircraft May 19, 1971 2012-08-03
Forum 27 IFR Hover for Heavy Lift Helicopters with Slung Loads W. P. Keane and R. J. Milelli, USAECOM May 19, 1971 2012-08-03
Forum 27 Feel Augmentation and Sensitivity Control in High Speed Helicopters S. J. O'Connor, Sikorsky May 19, 1971 2012-08-03
Forum 27 Rotor Stability Derivatives Determined from Wind Tunnel Tests of an Instrumented Helicopter R. E. Rohtert and S. V. LaForge, Hughes Tool Co., Aircraft Div. May 19, 1971 2012-08-03
Forum 27 Factors Affecting Handling Qualities of a Lift-Fan Aircraft During Steep Terminal Area Approaches R. M. Gerdes, and C. S. Hynes, NASA-Ames May 19, 1971 2012-08-03
Forum 27 Evaluation of Rotor Controls Designed for Increased Safety L. D. Barrett and J. C. Mack, Boeing / Vertol May 19, 1971 2012-08-03
Forum 27 Fail-Safety for the H-46 Rotor Blade G. H. Thompson and W. L. Weiss, Boeing / Vertol May 19, 1971 2012-08-03
Forum 27 Size Effects on the Design of Large Rotor Systems H. G. Smith, Hughes Tool Co., Aircraft Div. May 19, 1971 2012-08-03
Forum 27 Fatigue Strength Improvements in Ti-6A1-4V Forgings J. J. Lucas, Sikorsky Aircraft May 19, 1971 2012-08-03
Forum 27 Preliminary Design Methods of V/STOL Prop/Rotors W. Stratton, R. Sandford, and G. Miliziano, Boeing/Vertol May 19, 1971 2012-08-03
Forum 27 Factors Affecting Fuel Control Stability of a Turbine Engine/Helicopter Rotor Drive System C. Frederickson, Boeing/Vertol; K. Rumford, AVCO/Lycoming; and C. Stephenson, AVSCOM May 19, 1971 2012-10-03
Forum 27 Turbofan Engine Considerations for Reaction Drive Rotors R. J. Sullivan, Hughes Tool Co., Aircraft Div. May 19, 1971 2012-10-03
Forum 27 Strain Gauge Torquemeters for use in Helicopter Transmission Systems D. P. Hames, British Hovercraft Corp. Ltd. May 19, 1971 2012-10-03
Forum 27 VTOL Propulsion System Development P. C. Setze and J. L. Browne, General Electric Co. May 19, 1971 2012-10-03
Forum 27 Results of High-Speed Flight Research With the High Performance UH-1 Compound Helicopter W. G. O. Sonneborn and L. W. Hartwig, Bell Helicopter Co. May 19, 1971 2012-08-03
Forum 27 Boeing Model 347 Flying Qualities Demonstrator Program F. H. Duke and W. E. Hooper, Boeing / Vertol May 19, 1971 2012-08-03
Forum 27 USCG Evaluates Hovercraft Cdr T. C. Lutton, Air Cushion Vehicle Evaluation Unit May 19, 1971 2012-08-03
Forum 27 Army / Navy Operational Evaluation of Offshore Discharge of Containerships LtC. L. J. McConnell, USA May 19, 1971 2012-08-03
Forum 27 AH-56A Vehicle Development J. F. Johnston and J. R. Cook, Lockheed-Calif. Co. May 19, 1971 2012-08-03
Forum 28 Results Of Preliminary Studies of A Bearingless Helicopter Rotor Concept M. C. Cheney, United Aircraft Corp. Res. Labs May 17, 1972 2012-08-03
Forum 28 Flight Investigation of Design Features of the S-67 Winged Helicopter R. C. Dumond and D. R. Simon, Eustis Directorate, USAAMR&D Lab May 17, 1972 2012-08-03
Forum 28 New Hubs for Multi-Bladed Tail Rotors F. Robinson, Hughes Tool Co., Aircraft Div. May 17, 1972 2012-08-03
Forum 28 Design Considerations of Circulation Control Rotors R. M. Williams, E. O. Rogers, Naval Ship R&D Center May 17, 1972 2012-08-03
Forum 28 Design Requirements for a Quiet Helicopter N. B. Hirsh, H. W. Ferris, Hughes Tool Co., Aircraft Div. May 17, 1972 2012-08-03
Forum 28 Exploration Of Aeroelastic Stability Boundaries with a Soft In-Plane Hingeless Rotor Model J. E. Burkam, W. Miao, Boeing/Vertol May 17, 1972 2012-08-03
Forum 28 Hingeless Rotor Experimental Frequency Response and Dynamic Characteristics with Hub Moment Feedback Controls W. A. Kuczynski, D. L. Sharpe, G. J. Sissingh, Lockheed California Co. / AMRDL-Ames Directorate/Lockheed-California Co. May 17, 1972 2012-08-03
Forum 28 Determination Of Airfoil and Rotor Blade Dynamic Stall Response F. O. Carta, UARL; R. G. Carlson, Sikorsky Aircraft May 17, 1972 2012-08-03
Forum 28 The Controllable Twist Rotor, Performance and Blade Dynamics A. Z. Lemnios, Kaman Aerospace; W. E. Nettles, A. F. Smith, USAAMRDL May 17, 1972 2012-08-03
Forum 28 Parametric Studies of Instabilities Associated with Large, Flexible Rotor Propellers Dr. Robert A. Johnson, Sikorsky Aircraft May 17, 1972 2012-08-03
Forum 28 The Wake Geometry of a Hovering Helicopter Rotor and its Influence on Rotor Performance A. J. Landgrebe, UARL May 17, 1972 2012-08-03
Forum 28 Influence of Airfoils on Stall Flutter Boundaries Of Articulated Helicopter Rotors R. G. Benson, L. U. Dadone, R. E. Gormont, G. R. Kohler, Boeing/Vertol May 17, 1972 2012-08-03
Forum 28 Boundary Layer Velocity Profiles on a Helicopter Rotor Blade in Hovering and Forward Flight D. A. Blaser and H. R. Velkoff, Ohio State University May 17, 1972 2012-08-03
Forum 28 Wind Tunnel Simulation of Full Scale Vortices J. B. Rorke, R. C. Moffitt, Sikorsky Aircraft; J. F. Ward, NASA-Langley May 17, 1972 2012-08-03
Forum 28 Wind Tunnel Simulation of Full Scale Vortices J. B. Rorke, R. C. Moffitt, Sikorsky Aircraft; J. F. Ward, NASA-Langley May 17, 1972 2018-27-11
Forum 28 The Nemesis of the Trailed Tip Vortex--Is It Now Conquered? R. P. White Jr., J. C. Balcerak, Rochester Applied Science Associates, Inc. May 17, 1972 2012-08-03
Forum 28 Subcommittee Chairman's Rept, on Aerodynamic Sources of Rotor Noise C. R. Cox, Bell Helicopter Co. May 17, 1972 2012-08-03
Forum 28 Maneuvering Heavy Sling Loads Near Hover T. A. Dukes, Princeton University May 17, 1972 2012-08-03
Forum 28 Low Level Night Operations of Army Aircraft W. J. Kenneally, Maj. D. D. Garrison, USAEC May 17, 1972 2012-08-03
Forum 28 Flight Test Evaluation of a Forward Looking Radar System to Search and Rescue Applications F. J. Winter Jr., WPAFB; B. W. Schneckenburger, Norden Div. of UAC May 17, 1972 2012-08-03
Forum 28 Helicopter Testing of Inertial Navigation Systems J. Hughes, Litton Guidance and Control Systems May 17, 1972 2012-08-03
Forum 28 Military Flight Test Results of the Helicopter Multifunction System (HELMS) H. W. Upton, C. Witzke, Bell Helicopter/Texas Instruments; E. Stolinski, USAECOM May 17, 1972 2012-08-03
Forum 28 Maneuverability--Theory and Application C. D. Wells, T. L. Wood, Bell Helicopter Co. May 17, 1972 2012-08-03
Forum 28 Maneuverability--Theory and Application C. D. Wells, T. L. Wood, Bell Helicopter Co. May 17, 1972 2015-04-11
Forum 28 Helicopter Stability Derivative Extraction and Data Processing Using Kalman Filtering Techniques J. Molusis, Sikorsky Aircraft May 17, 1972 2012-08-03
Forum 28 An Experimental Investigation of STOL Longitudinal Flying Qualities in the Landing Approach Using the Variable Stability X-22A Aircraft J. M. Schuler, R. E. Smith, J. V. Lebacqz, Cornell Aeronautical Laboratory, Inc. May 17, 1972 2012-08-03
Forum 28 A Review of MIL-F-83300 for Helicopter Applications D. L. Green, PACER Systems, Inc. May 17, 1972 2012-08-03
Forum 28 A Pilot's Opinion: VTOL Control Design Requirements for Instrument Approach Task J. M. Patton Jr. NASA Langley Research Center May 17, 1972 2012-08-03
Forum 28 Helicopter / Ship Interface Testing LCDR H. W. Lineback, Lt R. Parkinson, USN, Patuxent R. May 17, 1972 2012-08-03
Forum 28 The World Speed Records of the SA. 341 Gazelle R. Mouille, Aerospatiale May 17, 1972 2012-08-03
Forum 28 Results of the Reliability and Maintainability Demonstration of the OH-58A Light Observation Helicopter J. A. Gean, J. H. Ringgold, Bell Helicopter May 17, 1972 2012-08-03
Forum 28 Flight Tests to Develop the S-67 Blackhawk TM R. L. McCutcheon, Sikorsky Aircraft Div. May 17, 1972 2012-08-03
Forum 28 An Integrated System of Airborne and Ground-Based Instrumentation for Flying Qualities Research With the X-22 Airplane J. L. Beilman, Cornell Aeronautical Laboratory May 17, 1972 2012-08-03
Forum 28 Reduction of Noise and Acoustic-Frequency Vibrations in Aircraft Transmissions Dr. R. H. Badgley, Mechanical Technology, Inc. May 17, 1972 2012-08-03
Forum 28 Prevention of Fretting Fatigue G. L. Rodriguez, H. M. Lawton, Bell Helicopter May 17, 1972 2012-08-03
Forum 28 Achieving Fail Safe Design in Rotors W. K. Stratton, D. M. Field, R. H. Finney, Boeing/Vertol May 17, 1972 2012-08-03
Forum 28 Ballistic Damage Tolerant Composite Flight Control Components Maj. L. A. Fry, S. Pociluyko, Eustis Directorate, U. S. Army Air Mobility R&D Lab. May 17, 1972 2012-08-03
Forum 28 The Starting of Turbine Engines in Helicopters B. Liff, R. B. Bossler Jr., Kaman Aerospace May 17, 1972 2012-08-03
Forum 28 Secondary Power System for Advanced Transport Helicopter G. J. Amarel, AiResearch Mfg. Co. of Arizona May 17, 1972 2012-08-03
Forum 28 Application of Boron/Epoxy to the CH-54B Skycrane R R. T. Welge, Sikorsky Aircraft May 17, 1972 2012-08-03
Forum 28 Full Scale Airframe Fatigue Testing of the CH-46 R. E. Bainbridge, Boeing/Vertol May 17, 1972 2012-08-03
Forum 29 An Investigation of the Flow Field and Drag of Helicopter Fuselage Configurations James Gillespie, USAAMR&DL, Ft. Eustis, Va. May 9, 1973 2012-08-03
Forum 29 An Experimental and Analytical Study of the Influence of Aerodynamic Design Parameters on the Static Performance of Ducted Fans for Tail Rotor Applications Jack E. Fairchild, Robert L. Stewart, and N. N. Batra, University of Texas at Arlington May 9, 1973 2012-08-03
Forum 29 A Detailed Experimental Analysis of Dynamic Stall on an Unsteady Two-Dimensional Airfoil J. M. Martin, R. W. Empey, and W. J. McCroskey, F. X. Caradonna, USAAMR&DL, Moffett Field, Calif. May 9, 1973 2012-08-03
Forum 29 Experimental Investigation of Model Variable-Geometry and OGEE-Tip Rotors A. J. Landgrebe, and E. D. Bellinger, UARL May 9, 1973 2012-08-03
Forum 29 The Application of Circulation Control Aerodynamics to a Helicopter Rotor Model Joseph B. Wilkerson, Kenneth R. Reader, and Drew W. Linck, NSRDC May 9, 1973 2012-08-03
Forum 29 The Heavy Lift Helicopter Rotor Blade T. Scarpati, R. Sandford, and B. Powell, Boeing Vertol Co./ USAARMDL (Eustis) May 9, 1973 2012-08-03
Forum 29 Design and Development of the Westland Sea Lynx D. K. Berrington, Westland Helicopters May 9, 1973 2012-08-03
Forum 29 Establishing a Designer's Cost Target M. Dubey and A. Yackle, Lockheed-California Co. May 9, 1973 2012-08-03
Forum 29 Development of H-53 Elastomeric Rotor Head W. J. Dutton, Sikorsky Aircraft Div. May 9, 1973 2012-08-03
Forum 29 Multi-Blade Ring Rotor Design Dr. Henry R. Velkoff, USAAMR&DL, Moffett Field, Calif. May 9, 1973 2012-08-03
Forum 29 Precision Survivor Locator for Search & Rescue Applications E. A. Harvey, WPAFB; and Maj. D. L. Jensen, Hill AFB, Utah May 9, 1973 2012-08-03
Forum 29 Redundant System Design for Helicopter Flight Control F. G. Kilmer and J. R. Sklaroff, IBM May 9, 1973 2012-08-03
Forum 29 Pilot-in-the-Loop Control Systems (A Different Approach) Capt. K. W. McElreath, J. A. Klein, and R. C. Thomas, WPAFB/Collins Radio Co. May 9, 1973 2012-08-03
Forum 29 The Application of System Analysis Techniques for the Solution of Complex Helicopter Crew Station Design Problems James J. Belcher, Litton Systems Inc. May 9, 1973 2012-08-03
Forum 29 Image and Superimposed Symbology - An Integrated Display for Helicopters T. A. Dukes, Princeton University; W. P. Keane, and C. M. Tsoubanos, USA, ECOM, Ft. Monmouth, N. J. May 9, 1973 2012-08-03
Forum 29 A Study of Stall-Induced Flap-Lag Instability of Hingeless Rotors R. A. Ormiston and W. G. Bousman, USAAMR&DL, Moffett Field, Calif. May 9, 1973 2012-08-03
Forum 29 Effect of Torsion-Flap-Lag Coupling on Hingeless Rotor Stability H. Huber, Messerschmitt Bolkow-Blohm GmbH May 9, 1973 2012-08-03
Forum 29 On the Question of Adequate Hingeless Rotor Modeling in Flight Dynamics Kurt H. Hohenemser and Sheng-Kuang Yin, Washington University, St. Louis, Mo. May 9, 1973 2012-08-03
Forum 29 Investigation of Reactionless Mode Stability Characteristics of a Stiff Inplane Hingeless Rotor System William D. Anderson, Lockheed-California Co. May 9, 1973 2012-08-03
Forum 29 An Investigation of the Vibratory and Acoustic Benefits Obtainable by the Elimination of the Blade Tip Vortex Richard P. White Jr., RASA, Inc. (Standby) May 9, 1973 2012-08-03
Forum 29 Applications of Antiresonance Theory to Helicopters Felton D. Bartlett Jr., and William G. Flannelly, Kaman Aerospace Corp. (Standby) May 9, 1973 2012-08-03
Forum 29 A Frequency Response Approach to Flying Qualities Criteria and Flight Control System Design N. Albion and W. R. Larson, Boeing Vertol Co. May 9, 1973 2012-08-03
Forum 29 Handling Qualities Comparison of Two Hingeless Rotor Control Systems A. J. Potthast and J. T. Blaha, Lockheed-California Co. May 9, 1973 2012-08-03
Forum 29 A Manual-Control Approach to Development of VTOL Automatic Landing Technology J. Kelly, NASA, Langley, Hampton, Va. May 9, 1973 2012-08-03
Forum 29 Flight Simulator Evaluation of Control Moment Usage and Requirements for V/STOL Aircraft W. Vinje, UARL May 9, 1973 2012-08-03
Forum 29 ABC Helicopter Stability, Control and Vibration Evaluation on the Princeton Track D. Halley, Sikorsky Aircraft Div. May 9, 1973 2012-08-03
Forum 29 Recognition and Control of Abusive Machining Effects on Helicopter Components W. A. Thomas, Bell Helicopter Co. May 9, 1973 2012-08-03
Forum 29 Human Side of Q. A. as Viewed from Helicopter Manufacturing Experience G. M. Powell, Bell May 9, 1973 2012-08-03
Forum 29 The Development and Qualification of a Magnetic Technique for the Nondestructive Measurement of Residual Stress in CH-47A Rotor Blade Spar" F. H. Bray and H. H. Fitz III, Boeing Vertol May 9, 1973 2012-08-03
Forum 29 Computer Graphics Used in Numerical Control Programming Richard N. Hayes, Sikorsky May 9, 1973 2012-08-03
Forum 29 Low Cost Manufacturing Methods for Highly Reliable Ballistic-Tolerant Composite Helicopter Control Components Maj. L. A. Fry, USAAMRDL (Eustis); and R. L. Van Auken, Whittaker May 9, 1973 2012-08-03
Forum 29 Wind Tunnel Test Technique to Establish Rotor System Aeroelastic Characteristics Franklin D. Harris, Boeing Vertol May 9, 1973 2012-08-03
Forum 29 Flight Test Development of the Tactical Aircraft Guidance System J. C. Deardorff, A. L. Freisner, and N. Albion, Boeing Vertol May 9, 1973 2012-08-03
Forum 29 Development of Conical Teflon-Lined Journal Bearings Frank Robinson, Hughes Helicopters May 9, 1973 2012-08-03
Forum 29 Army Vibration Survey Methods and Results Emmett J. Laing, USA, ASTA May 9, 1973 2012-08-03
Forum 29 Tail Rotor Performance in Presence of Main Rotor, Ground and Winds W. Wiesner, Boeing Vertol May 9, 1973 2012-08-03
Forum 29 Elastohydrodynamic Principles Applied to the Design of Helicopter Components D. P. Townsend, NASA Lewis Research Center May 9, 1973 2012-08-03
Forum 29 T700 Fuel and Control System - A Modern System Today for Tomorrow's Helicopters J. J. Curran, General Electric Co. May 9, 1973 2012-08-03
Forum 29 A Dynamics Approach to Helicopter Transmission Noise Reduction and Improved Reliability R. M. Hartman, Boeing Vertol May 9, 1973 2012-08-03
Forum 29 Power Transfer Systems for Future Helicopters Robert B. Bossler Jr. Kaman Aerospace; and W. Rutland Harris Jr., NASC May 9, 1973 2012-08-03
Forum 29 Vibratory Compatibility of Rotary Wing Aircraft Propulsion Components John M. Vance, Univ. of Florida; and James Gomez Jr., AMRDL, Ft. Eustis May 9, 1973 2012-08-03
Forum 29 The Integration of NASTRAN into Helicopter Airframe Design/Analysis D.A. Gallian and H. E. Wilson, Bell May 9, 1973 2012-08-03
Forum 29 A Consistent Crashworthiness Design Criteria Approach for Rotary Wing Aircraft G. Wittlin, Lockheed, Burbank May 9, 1973 2012-08-03
Forum 29 The Twin Beam Composite Rotor Blade M. J. Salkind, Sikorsky Aircraft May 9, 1973 2012-08-03
Forum 29 Development of the CH-53D High Performance Titanium Main Rotor Blade J. Bettino and R. Tracy, NASC; and R. Zincone, Sikorsky Aircraft May 9, 1973 2012-08-03
Forum 29 Advanced Technologies as Applied to the Design of the HLH Rotor Hub H. K. Reddick Jr., USAAMR&DL, Eustis; C. D. McCall, and D. M. Field, Boeing Vertol May 9, 1973 2012-08-03
Forum 29 An Advanced Composite Tail Boom for the AH-1G Helicopter H. Zinberg, Bell Helicopter Co. May 9, 1973 2012-08-03
Forum 30 Laser Velocimeter Measurements of the Helicopter Rotor-Induced Flow Field J. C. Biggers and K. L. Orloff, NASA-Ames Research Center. May 7, 1974 2012-08-03
Forum 30 The Prediction of Rotor Rotational Noise Using Measured Fluctuating Blade Loads R. N. Hosier, USAAMRDL, NASA-Langley; and R. Ramanakrishnan and R. J. Pegg, NASA-Langley Research Center. May 7, 1974 2012-08-03
Forum 30 Tail Rotor Thrust on a 5.5 Ft. Helicopter Model in Ground Effect R. W. Empey and R. A. Ormiston, USAAMRDL, NASA-Ames. May 7, 1974 2012-08-03
Forum 30 Can Helicopter Rotors be Designed for Low Noise and High Performance? D. R. Clark, Sikorsky Aircraft. May 7, 1974 2012-08-03
Forum 30 A Systematic Study of Helicopter Rotor Stall Using Model Rotors A. J. Landgrebe and E. D. Bellinger, UARL. May 7, 1974 2012-08-03
Forum 30 Design-to-Cost Applied to the Helicopter Structure L. J. Marchinski, Boeing Vertol Co. May 7, 1974 2012-08-03
Forum 30 Improved Cost Effectiveness of Helicopters Through a Two-Point Design Criterion A. Plaks, Kaman Aerospace Corp., H. I. MacDonald, USAAMRDL-Eustis, and R. C. Meier and R. F. Metzger, Kaman Aerospace Corp. May 7, 1974 2012-08-03
Forum 30 The Scissors Rotor W. Sonneborn and Jan Drees, Bell Helicopter Co. May 7, 1974 2012-08-03
Forum 30 Hingeless Circulation Control Rotor Blade Design P. H. Kesling, Lockheed-Calif. Co. May 7, 1974 2012-08-03
Forum 30 Hybrid Aircraft for Heavy Lift D. B. Doolittle, All American Engineering Co., and J. B. Nichols, The Aerospace Corp. May 7, 1974 2012-08-03
Forum 30 Pilot Workload During Instrument Flight A. L. Winn and R. B. Lewis II, USAASTA, Edwards AFB. May 7, 1974 2012-08-03
Forum 30 Visual and Manual Workload of the Helicopter Pilot D. D. Strother, Bell Helicopter Co. May 7, 1974 2012-08-03
Forum 30 Helicopter Command Instrument Systems J. Hatcher, USA Aviation Systems Command May 7, 1974 2012-08-03
Forum 30 U. S. Navy VTOL Automatic Landing System Development R. S. Buffum, R. W. Huff and G. L. Keyser, Naval Air Test Center. May 7, 1974 2012-08-03
Forum 30 Avionic and Fire Control Equipment Complement to Enhance Attack Helicopter Survivability E. D. Stepans, Lockheed-California Co. May 7, 1974 2012-08-03
Forum 30 Controls & Displays for Helicopter IFR Operation - Pilot Factor Considerations F. J. Winter Jr., USAFFDL-Wright-Patterson AFB.(Standby) May 7, 1974 2012-08-03
Forum 30 Helicopter Vibration Reduction with Pendulum Absorbers R. B. Taylor and P. A. Teare, Boeing Vertol Co. May 7, 1974 2012-08-03
Forum 30 On the Use of First-Order Rotor Dynamics in Multiblade Coordinates K. H. Hohenemser and S. K. Yin, Washington University. May 7, 1974 2012-08-03
Forum 30 Effect of Hub Impedance on the Oscillatory Blade Loads of a Two-Bladed Rotor System J. A. White and C. D. Lee, Bell Helicopter Co. May 7, 1974 2020-29-09
Forum 30 Effect of Hub Impedance on the Oscillatory Blade Loads of a Two-Bladed Rotor System J. A. White and C. D. Lee, Bell Helicopter Co. May 7, 1974 2012-08-03
Forum 30 The Effect of Blade Design Parameters on Helicopter Stall Boundaries R. H. Blackwell, Sikorsky Aircraft, and P. H. Mirick, USAAMRDL, Eustis. May 7, 1974 2012-08-03
Forum 30 AH-56A (AMCS) Compound Helicopter Vibration Reduction W. D. Anderson and E.R. Wood, Lockheed-California Co. May 7, 1974 2012-08-03
Forum 30 Aeroelastic Stability Characteristics of a V/STOL Tilt-Rotor Aircraft with Hingeless Blades: Analysis and Test Correlation H. R. Alexander and L. M. Hengen, Boeing Vertol Co. and W. J. Weiberg, NASA - Ames Res. Center. (Standby) May 7, 1974 2012-08-03
Forum 30 Handling Qualities Evaluations of the XV-15 Tilt-Rotor Aircraft R. L. Marr, Bell Helicopter Co., G. Churchill, NASA-Ames, and W. E. B. Roderick, NRC, Canada. May 7, 1974 2012-08-03
Forum 30 An Experimental Investigation of STOL Lateral-Directional Flying Qualities and Roll Control Power Requirements Using the Variable-Stability X -22A Aircraft J. V. Lebacqz and R. C. Radford, Calspan Corp., and R. E. Smith, NRC, Canada. May 7, 1974 2012-08-03
Forum 30 Rotor Moment and Blade Clearance Control with Flap Moment Feedback A. J. Potthast and Andrew W. Kerr, Lockheed-California Co. May 7, 1974 2012-08-03
Forum 30 Analysis and Simulation of Piloted Performance in Crane-Type Helicopters in Hover R. T. Lytwyn and F. White, Boeing Vertol Co., and R. P. Smith, USAAMRDL, Eustis. May 7, 1974 2012-08-03
Forum 30 Helicopter Icing Handling Qualities W. E. Griffith and L. K. Brewer, USAASTA-Edwards. May 7, 1974 2012-08-03
Forum 30 Fabrication of Boron-Hybrid Swashplates J. W. Jakubowski and A. Yankovoy, Boeing Vertol Co. May 7, 1974 2012-08-03
Forum 30 Zero-Zero-One Percent Performance! Quality Assurance by Objectives G. M. Powell and J. M. Gooch, Bell Helicopter Co. May 7, 1974 2012-08-03
Forum 30 Heat Transfer Modelling for Curing Process of Composite Rotor Blades Tia-Lang Huang and A. A. Peterson, Boeing Vertol Co. May 7, 1974 2012-08-03
Forum 30 Titanium Spar Processing - An Approach to Fabricating Blade Spars S. M. Silverstein, Sikorsky Aircraft. May 7, 1974 2012-08-03
Forum 30 Helicopter Reliability Testing T. L. House, USAAMRDL, Eustis. May 7, 1974 2012-08-03
Forum 30 RAPID - A Data Acquisition and Processing System for Flight Test Cost and Schedule Improvement V. G. Berecz, Sikorsky Aircraft. May 7, 1974 2012-08-03
Forum 30 Helicopter Flight Investigation to Determine the Effects of a Closed Circuit TV on Performance of a Precision Sling Load Handling Task D. J. DiCarlo and H. L. Kelly, USAAMRDL, NASA-Langley. May 7, 1974 2012-08-03
Forum 30 Experiment 43.7 - Attack Helicopter - Clear Night Defense W. L. Odneal, USA Combat Developments Experimentation Command. May 7, 1974 2012-08-03
Forum 30 UTTAS Flight Test: Real-Time Data Analysis H. H. Steinmann and D. L. Marshall, Boeing Vertol Co. May 7, 1974 2012-08-03
Forum 30 Heavy-Lift Helicopter Engine-Control System J. R. Alwang and T. Himka, Boeing Vertol Co., and R. D. McLain, GM Detroit Diesel Allison Div. May 7, 1974 2012-08-03
Forum 30 The Impact of Advanced Turboshaft Engine Technology on T700-Powered Helicopter Systems L. B. Veno, General Electric Co. May 7, 1974 2012-08-03
Forum 30 Small Turbine Advanced Gas Generators for Future Propulsion Requirements E. T. Johnson and G. A. Elliott, USAAMRDL, Eustis. May 7, 1974 2012-08-03
Forum 30 Balancing of High-Speed Interconnect Shafting for Operation Above Multiple Bending Critical Speeds R. H. Badgley and J. M. Tessarzik, Mechanical Technology, Inc. May 7, 1974 2012-08-03
Forum 30 Engine/Airframe Simulation: Digital Computer Techniques D. V. Lewis, Boeing Vertol Co. May 7, 1974 2012-08-03
Forum 30 Application of Advanced Composites for Helicopter Airframe Structure M. J. Rich, D. W. Lowry, and G. F. Ridgley, Sikorsky Aircraft. May 7, 1974 2012-08-03
Forum 30 The Application of Fracture Mechanics to the Design of Damage-Tolerant Components for the UTTAS Helicopter W. L. Weiss and J. C. Zola, Boeing Vertol Co. May 7, 1974 2012-08-03
Forum 30 Design, Testing and Performance of Elastomeric Bearings W. E. Schmidt, Lord Kinematics, Lord Corp. May 7, 1974 2012-08-03
Forum 30 Composite Material Geodesic Structures - A Structural Concept for Increased Helicopter Rotor Blade Survivability S. Pociluyko and I. E. Figge, USAAMRDL, Eustis, and C. F. Griffin and L. Blad, Lockheed-California Co. May 7, 1974 2012-08-03
Forum 31 Laser Velocimeter Measurements of Rotor Blade Loads and Tip Vortices James C. Biggers, Sing Chu, and Kenneth L. Orloff, NASA, Ames Research Center May 13, 1975 2012-08-03
Forum 31 The Development of Transonic Airfoils for Rotors J. W. Sloof, Netherlands National Aerospace Lab.; F. X. Wortmann, University of Stuttgart, Germany; and J. M. Duhon, Bell Helicopter Co. May 13, 1975 2012-08-03
Forum 31 A Model Rotor Validation for the CCR Technology Demonstrator Joseph B. Wilkerson and Drew W. Linck, Naval Ship R&D Center May 13, 1975 2012-08-03
Forum 31 Have We Overlooked the Full Potential of the Conventional Rotor? Franklin D. Harris and Frank McHugh, Boeing Vertol Co. May 13, 1975 2012-08-03
Forum 31 Aerodynamic Design Rationale for the Fan-in-Fin on the S-67 Helicopter David R. Clark, Sikorsky Aircraft May 13, 1975 2012-08-03
Forum 31 The Army YAH-63 Design and Development Charles M. Seibel and L. D. Kulik, Bell Helicopter Company May 13, 1975 2012-08-03
Forum 31 YAH-64 Advanced Attack Helicopter John C. Dendy and C. L. Landers, Hughes Helicopters May 13, 1975 2012-08-03
Forum 31 Candidate Rotary-Wing Aircraft for Selected Navy/Marine Missions of the 1980s George Unger, Naval Air Systems Command May 13, 1975 2012-08-03
Forum 31 Application of a Variable-Diameter Rotor System to Advanced VTOL Aircraft Evan A. Fradenburgh, Sikorsky Aircraft May 13, 1975 2012-08-03
Forum 31 Design Variables for a Controllable Twist Rotor Donald W. Robinson Jr., Kaman Aerospace Corp. ; W. E. Nettles, USAAMRDL, Eustis Directorate; and H. E. Howes, also of Kaman May 13, 1975 2012-08-03
Forum 31 New Concepts for Helicopter Main Rotors Rene Mouille, Aerospatiale (France) May 13, 1975 2012-08-03
Forum 31 Analysis of Navigation Requirements for Commercial VTOL Operations William C. Hoffman and John Zvara, Aerospace Systems Inc., and Walter M. Hollister, MIT May 13, 1975 2012-08-03
Forum 31 Recent Advances in Flight Director and Automatic Flight Control Systems for IFR Helicopter Operations Carl D. Griffith and Robert T. Riall, Sperry Flight Systems May 13, 1975 2012-08-03
Forum 31 Simulation and Flight Test Results of a Manual Precision Hover Task Utilizing Symbology Superimposed on a Flir Image R.J. Milelli, D. C. Johnson and C. M. Tsoubanos, U. S. Army Electronics Command May 13, 1975 2012-08-03
Forum 31 Heavy-Lift Helicopter Primary Flight Control System Bruce L. McManus and Alan J. Niven, Boeing Vertol Co. May 13, 1975 2012-08-03
Forum 31 Rotor Modulation of VOR Signals John G. Mast, Bell Helicopter Co. May 13, 1975 2012-08-03
Forum 31 Night Vision for Army Aviation Charles J. Arduini, U. S. Army Electronics Command May 13, 1975 2012-08-03
Forum 31 Pendulum Absorbers Stop Transition Vibration G. Reichert, Messerschmitt (Germany), and Richard Gabel, Boeing Vertol Co. May 13, 1975 2012-08-03
Forum 31 Rotor Stability Prediction: Correlation with Full-Scale Tests Robert A. Johnston, Sikorsky Aircraft May 13, 1975 2012-08-03
Forum 31 An Analytical Study of a Multicycle Controllable-Twist Rotor John L. McCloud III, NASA, Ames Research Center May 13, 1975 2012-08-03
Forum 31 Investigation of Helicopter Airframe Normal Modes R. J. Parker, T. Yarker, R. L. Mattravers, and R.W. White, Westland Helicopters Ltd. (England) May 13, 1975 2012-08-03
Forum 31 Rotor Blade Wake Flutter--A Comparison of Theory and Experiment William D. Anderson and George A. Watts, Lockheed-California Co. May 13, 1975 2012-08-03
Forum 31 Synthesized Unsteady Airfoil Data With Applications to Stall Flutter Calculations R. L. Bielawa, United Aircraft Research Laboratories May 13, 1975 2012-08-03
Forum 31 Development of Heavy-Lift Helicopter Handling Qualities for Precision Cargo Operations James M. Davis, Kenneth H. Landis, and John R. Leet, Boeing Vertol Co. May 13, 1975 2012-08-03
Forum 31 Use Of Programmable Force Feel For Handling Qualities Improvement in a Helicopter Velocity Flight Control System Ralph B. Trueblood and W. B. Bryant, C. S. Draper Lab. May 13, 1975 2012-08-03
Forum 31 Designing to Survive Tail Rotor Loss T. J. Horst and R. J. Reschak, Bell Helicopter Co. May 13, 1975 2012-08-03
Forum 31 Stability and Control of the YUH-61A Bruce B. Blake and I.B. Alansky, Boeing Vertol Co. May 13, 1975 2012-08-03
Forum 31 A Flight Investigation of Control, Display and Guidance Requirements for Decelerating Descending VTOL Instrument Transitions Using the X-22A Variable-Stability Aircraft J. V. Lebacqz and E. W. Aiken, Calspan Corp. May 13, 1975 2012-08-03
Forum 31 The Application and Control of Powdered Coatings G. M. VanDeventer, Bell Helicopter Co. May 13, 1975 2012-08-03
Forum 31 The Applied Manufacturing Technology Related to the XCH-62 Heavy-Lift Helicopter Prototype Airframe--the First All-Honeycomb-Primary-Structure Aircraft L. J. Ralston and A. C. Haggerty, Boeing Vertol Co. May 13, 1975 2012-08-03
Forum 31 Supplier-Designed Components--QA for User Satisfaction T. G. Hill, Bell Helicopter Co. May 13, 1975 2012-08-03
Forum 31 Diffusion-Bonded Ti-6A1-4V Helicopter Rotor Hub and Spar Technology J. J. Lucas and M. J. Bonassar, Sikorsky Aircraft, and P. J. Doyle, AMMRC-Watertown, Mass. May 13, 1975 2012-08-03
Forum 31 Product Assurance as Viewed by the Aviation Systems Command E. J. Hollman, AVSCOM May 13, 1975 2012-08-03
Forum 31 Navy Shipboard Trials of Helicopters and V/STOL Aircraft Cdr. Donald E. Beck, USN May 13, 1975 2012-08-03
Forum 31 Heavy-Lift Helicopter Flight Control System Flight Test Report A. J. Hutto, Boeing Vertol Co. May 13, 1975 2012-08-03
Forum 31 Army Preliminary Evaluation of the HLH ATC Demonstrator Fly-by-Wire Flight Control System AFCS D. R. Simon, J. L. Terry Jr., and J. C. Savage, USAAMRDL, Eustis Directorate May 13, 1975 2012-08-03
Forum 31 The Design and Testing of a Tip Shape to Reduce Blade Slap J. L. Tangler, Bell Helicopter Co. May 13, 1975 2012-08-03
Forum 31 Remotely Piloted Vehicle/Vertical Take-Off and Landing Demonstration Vehicle Warren H. Eilertson, Naval Ship R&D Center May 13, 1975 2012-08-03
Forum 31 Advanced Engine Controls and Accessories for Helicopter Applications Roger Furgurson, USAAMRDL Eustis Directorate May 13, 1975 2012-08-03
Forum 31 Integrated Airflow Concepts for Helicopter Engine and Drive System Richard D. Semple, Boeing Vertol Co. May 13, 1975 2012-08-03
Forum 31 The Design and Development of the GEM Engine C. H. Buck, Rolls-Royce (England) May 13, 1975 2012-08-03
Forum 31 Design and Development of a Free Planet Transmission E. R. Givens, USAAMRDL, Eustis Directorate, and N. A. DeBruyne and D. J. Folenta, Curtiss-Wright Corp. May 13, 1975 2012-08-03
Forum 31 Advancements in I.R. Suppressors for Helicopters Clifford Banthin, AVCO Lycoming May 13, 1975 2012-08-03
Forum 31 Titanium UTTAS Main Rotor Blade Robert Zincone and Peter J. Arcidiacono, Sikorsky Acft. May 13, 1975 2012-08-03
Forum 31 Prediction of Helicopter Control Load Structural Limits Richard Gabel and Robert B. Taylor, Boeing Vertol Co. May 13, 1975 2012-08-03
Forum 31 A Composite Pylon Support Structure for the JetRanger Helicopter Herbert Zinberg, Bell Helicopter Co. May 13, 1975 2012-08-03
Forum 31 A Study of Helicopter Landing Behavior on Small Ships R. M. Tuttle, Kaman Aerospace May 13, 1975 2012-08-03
Forum 31 Ballistic Design Support Tests--A Tool for Helicopter Vulnerability Reduction Robert E. Rohtert, Hughes Helicopters May 13, 1975 2012-08-03
Forum 31 Design Criteria for Elastomeric Bearings John R. Hinchman and Arnold R. Thompson of Thiokol Corp., and John Sobczak, USAAMRDL, Eustis Directorate May 13, 1975 2012-08-03
Forum 31 Aeroelastic Modeling of Large Wind Turbines Peretz Friedmann, University of California May 13, 1975 2012-08-03
Forum 31 A Rigid Body Model for Analysis of Aerogenerator Rotor Dynamics C. E. Smith, R. W. Thresher, R. E. Wilson, and R. B. MacDuff, Oregon State University May 13, 1975 2012-08-03
Forum 31 Wind Rotors--How to Select Them and Their Dynamic Characteristics Carl Wilcox, Allis Chalmers May 13, 1975 2012-08-03
Forum 31 Dynamic Response of Wind Turbine Rotor Systems Robert A. Ormiston, USAAMRDL, Ames Directorate May 13, 1975 2012-08-03
Forum 31 How Big is a Windmill--Glauert Revisited John L. McCloud III and James C. Biggers, NASA, Ames Research Center May 13, 1975 2012-08-03
Forum 31 Performance and Structural Design Aspects of A Counterweighted One-Bladed Electric Power Generating Windmill Richard R. Pruyn and Wayne Wiesner, Boeing Vertol Co., and Peter Sulzer, Consulting Engineer May 13, 1975 2012-08-03
Forum 31 An Approach to the Aerodynamic Design of Optimum Rotors for Wind-Power Generators Carl Rohrbach and Rose Worobel, UAC Hamilton Standard Div. May 13, 1975 2012-08-03
Forum 31 Concept Selection and Analysis of Large Wind Generator Systems Richard C. Meier, Kaman Aerospace Corp. May 13, 1975 2012-08-03
Forum 31 100 kW-Hingeless Metal Wind Turbine Blade Design, Analysis and Fabrication Bradford S. Linscott and Richard L. Puthoff of NASA - Lewis Research Center, and Robert E. Donham and Jaap Schmidt of Lockheed-California Co. May 13, 1975 2012-08-03
Forum 31 Some Important Practical Design Constraints Affecting Drag Reduction

Gormont, R.E., “Some Important Practical Design Constraints Affecting Drag Reduction,” Rotorcraft Parasite Drag Special Report, presented at the 31st Annual Forum of the American Helicopter Society, Washington, D.C., May 14–15, 1975.

May 13, 1975 2014-10-11
Forum 32 The Effect Of The Ground On Helicopter Hovering Power Required James S. Hayden May 10, 1976 2015-26-01
Forum 32 A Prescribed Wake Lifting Surface Hover Performance Analysis J. David Kocurek; James L. Tangler May 10, 1976 2015-26-01
Forum 32 A Prescribed Wake Lifting Surface Hover Performance Analysis J. David Kocurek; James L. Tangler May 10, 1976 2017-30-05
Forum 32 Prediction Of Helicopter Induced Flow Velocities Using The Rotorcraft Wake Analysis Anton J. Landgrebe; T. Alan Egolf May 10, 1976 2015-26-01
Forum 32 Circulation Control Applied To A High Speed Helicopter Rotor Kenneth R. Reader; Joseph B. Wilkerson; David W. Taylor May 10, 1976 2015-26-01
Forum 32 High-Speed Helicopter Impulsive Noise C. R. Vause; F. H. Schmitz; D. A. Boxwell May 10, 1976 2015-26-01
Forum 32 Design, Development, And Testing Of The Boeing Vertol/Army YUH-61A C. W. Ellis; J. Diamond; C. B. Fay May 10, 1976 2015-26-01
Forum 32 Survivability Of The Army/Sikorsky YUH-60A Helicopter James B. Foulk May 10, 1976 2015-26-01
Forum 32 Advancing Blade Concept (ABC Tm) Development Andrew J. Ruddell May 10, 1976 2015-26-01
Forum 32 Aerodynamic And Dynamic Design And Development Of The Main Rotor Of The YAH-64 Advanced Attack Helicopter Kenneth B. Amer; James R. Neff; Sally V. LaForge; Ray W. Prouty May 10, 1976 2015-26-01
Forum 32 High Energy Rotor System T. L. Wood May 10, 1976 2015-04-11
Forum 32 High Energy Rotor System T. L. Wood May 10, 1976 2015-26-01
Forum 32 Higher Harmonic Rotor Blade Pitch Control J. R. Ewans May 10, 1976 2015-26-01
Forum 32 Cockpit Design For Night Nap-Of-The Earth (Noe) Flight John H. Emery May 10, 1976 2015-26-01
Forum 32 An Electronic Integrated Pilot Display Is Evaluated In North Sea Operations R. J. van der Harten; Philip G. Cooper May 10, 1976 2015-26-01
Forum 32 Helicopter Vulnerability Reduction, Fly-By-Wire Backup Demonstration Stephen Pociluyko; Bruce L. McManus; Joseph E. Gonsalves May 10, 1976 2015-26-01
Forum 32 A Lightweight Doppler Navigation System Robert E. Chapman May 10, 1976 2015-26-01
Forum 32 Helicopter Night Low-Level Navigation: Study 1--Checkpoint Identification James A. Bynum; Brian D. Shipley; William C. White May 10, 1976 2015-26-01
Forum 32 Advanced Aircraft Electrical System And Its Application To Helicopters A. J. Marek; J. R. Perkins May 10, 1976 2015-26-01
Forum 32 Helicopter Rotor Isolation Evaluation Utilizing The Dynamic Antiresonant Vibration Isolator A. D. Rita; J. H. McGarvey; R. Jones May 10, 1976 2015-26-01
Forum 32 Aeroelastic Stability Of Complete Rotors With Application To A Teetering Rotor In Forward Flight Joseph Shamie; Peretz Friedmann May 10, 1976 2015-26-01
Forum 32 Aeroelastic Characteristics Of Composite Bearingless Rotor Blades Richard L. Bielawa May 10, 1976 2015-26-01
Forum 32 Rotor/Helicopter System Dynamic Aeroelastic Stability Analysis And Its Application To A Flexstrap Tail Rotor Lawrence R. Sutton; Santu T. Gangwani; William E. Nettles May 10, 1976 2015-26-01
Forum 32 A Critical Examination Of The Flap-Lag Dynamics Of Helicopter Rotor Blades In Hover And In Forward Flight K. R. V. Kaza; R. G. Kvaternik May 10, 1976 2015-26-01
Forum 32 An Experimental Study Of Techniques For Increasing The Lead-Lag Damping Of Soft Inplane Hingeless Rotors W. G. Bousman; D. L. Sharpe; R. A. Ormiston May 10, 1976 2015-26-01
Forum 32 The Effect Of Varying Freestream Velocity On Dynamic Stall Characteristics G. Alvin Pierce; Donald L. Kunz; John B. Malone May 10, 1976 2015-26-01
Forum 32 Rsra Flight Control And Stabilization Arthur W. Linden May 10, 1976 2015-26-01
Forum 32 Handling Qualities Considerations For Noe Flight L. W. Dooley May 10, 1976 2015-26-01
Forum 32 Flight Control System Development For The XV-15 Tilt Rotor Aircraft Roger L. Marr; J. Marvin Willis; Gary B. Churchill May 10, 1976 2015-26-01
Forum 32 Design And Flight Test Of The Active Arm External Load Stabilization System (AAELSS II) Theodore S. Garnett, Jr; James H. Smith; Richard Lane May 10, 1976 2015-26-01
Forum 32 A Study To Determine The Characteristic Shapes Of Helicopter Visual Approach Profiles Gene C. Moen; Daniel J. DiCarlo; Kenneth R. Yenni May 10, 1976 2015-26-01
Forum 32 Rigid Coaxial (Abc) Tm Rotor System Stability And Control Characteristics Robert F. Klingloff May 10, 1976 2015-26-01
Forum 32 Use Of Hlt As A Low-Cost Tool In Composite Fabrication Gerald A. Gorline; Bernard M. Halpin Jr. May 10, 1976 2015-26-01
Forum 32 Composite Main Rotor Blade For The 214 Helicopter R. G. Anderson; C. E. Covington May 10, 1976 2015-26-01
Forum 32 Production And Quality Control Of Infinite-Life Main Rotor Blades H. B. Epstein; Rene Mouille May 10, 1976 2015-26-01
Forum 32 Fatigue And Cost Improvements In Producing Titanium Leading Edges For Helicopter Rotor Blades C. S. Lin; R. L. Pinckney; N. M. Lukin May 10, 1976 2015-26-01
Forum 32 Economics Of Nondestructive Inspection Donald L. Duncan May 10, 1976 2015-26-01
Forum 32 Quality Assurance For Lastoflex Elastomeric Helicopter Bearings - Application Of New And Old Technologies Paul A. Hilbert May 10, 1976 2015-26-01
Forum 32 Helicopter Aerodynamics And Structural Loads Survey G. A. Shockey; J. W. Williamson; C. R. Cox May 10, 1976 2015-26-01
Forum 32 In-Flight Far-Field Measurement Of Helicopter Impulsive Noise F. H. Schmitz; D. A. Boxwell May 10, 1976 2015-26-01
Forum 32 Flight-Test Experience Of A Helicopter Encountering An Airplane Trailing Vortex R. Earl Dunham, Jr; G. Thomas Holbrook; Wayne R. Mantay; Richard L. Campbell; Roger W. Van Gunst May 10, 1976 2015-26-01
Forum 32 Full Scale Wind Tunnel Tests Of A Controllable Twist Rotor A. Z. Lemnios; William E. Nettles; H. E. Howes May 10, 1976 2015-26-01
Forum 32 YUH-60A Test Operations Kenneth C. Mard May 10, 1976 2015-26-01
Forum 32 Emergency Power Benefits To Multi-Engine Helicopters R. D. Semple; J.H. Yost; E. W. King; J. E. Gonsalves; W. Thompson May 10, 1976 2015-26-01
Forum 32 Selection Of A Fuel Handling System For A Small Advanced Turboshaft Engine Thomas L. Soule; William W. Hixson May 10, 1976 2015-26-01
Forum 32 Engine/Airframe Dynamic Interface Investigation Using T63/LOH Helicopter System W. H. Parker May 10, 1976 2015-26-01
Forum 32 Design, Fabrication And Testing An Advanced Composite AH-1G Tail Boom H. T. Lund; J. F. Needham May 10, 1976 2015-26-01
Forum 32 Nastran Correlation For The Model 214A Helicopter J. V. Howard May 10, 1976 2015-26-01
Forum 32 Full Scale Crash Testing Of A Ch-47C Helicopter George T. Singley III May 10, 1976 2015-26-01
Forum 32 UTTAS/HLH Rotor Blade Fabrication And Testing W. K. Stratton; T. S. Scarpati; R. J. Feenan May 10, 1976 2015-26-01
Forum 32 UTTAS/HLH Rotor Blade Fabrication And Testing W. K. Stratton; T. S. Scarpati; R. J. Feenan May 10, 1976 2015-26-01
Forum 32 Composite Bearingless Tail Rotor For Uttas Ronald R. Fenaughty; William L. Noehren May 10, 1976 2015-26-01
Forum 33 The Investigation of a Separation Model for the Prediction of C1max B. Maskew and F.A. Dvorak May 9, 1977 2012-07-03
Forum 33 A Semi-Empirical Correction for the Vortex Core Effect on Hovering Rotor Wake Geometries, S.S. Samant and R.B. Gray May 9, 1977 2012-07-03
Forum 33 Prediction of Helicopter Rotor Performance in Vertical Climb and Sidewards Flight R.C. Moffitt and T.W. Sheehy May 9, 1977 2012-07-03
Forum 33 Prediction of Helicopter Rotor Performance in Vertical Climb and Sidewards Flight R.C. Moffitt and T.W. Sheehy May 9, 1977 2016-18-11
Forum 33 Schlieren Studies of Rotors in Forward Flight J.L. Tangler May 9, 1977 2012-07-03
Forum 33 Aerodynamics of Helicopter Flight Near the Ground P.F. Sheridan and W. Wiesner May 9, 1977 2012-07-03
Forum 33 Measurements of Helicopter Tip Vortex Trajectories and Velocity Distributions J.C. Biggers, A. Lee, K.L. Orloff and O.J. Lemmer May 9, 1977 2012-07-03
Forum 33 Cost Performance Trade-Offs Hughes Helicopters, AH-64 Advanced Attack Helicopter M.A. Leone and C.L. Landers May 9, 1977 2012-07-03
Forum 33 The Army's Improved Main Rotor Blade for the AH-1 Helicopter P.F. Maloney, L.G. Dite and R.D. Powell May 9, 1977 2012-07-03
Forum 33 The AS-350 - A "Design-to-Cost" Exercise R. Mouille May 9, 1977 2012-07-03
Forum 33 Performance and Safety Aspects of the XV-15 Tilt Rotor Research Aircraft K.G. Wernicke May 9, 1977 2012-07-03
Forum 33 Efficient Civil Helicopters - The Payoff of Directed Research W. Wiesner and W. J. Snyder May 9, 1977 2012-07-03
Forum 33 The Concept of Remotely Piloted Helicopters I. A. Simons May 9, 1977 2017-31-07
Forum 33 The Concept of Remotely Piloted Helicopters I. A. Simons May 9, 1977 2012-07-03
Forum 33 A Review of Advanced Rotor Research M.W. Kelly and J.P. Rabbott May 9, 1977 2012-07-03
Forum 33 Tactile Displays for Helicopter Pilot Workload Reduction R.D. Gilson, P.B. Sun, and R. S. Dunn May 9, 1977 2012-07-03
Forum 33 A Flight Director/FLIR Helicopter Night Landing System P.G. Cooper May 9, 1977 2012-07-03
Forum 33 A Versatile Display System for NOE Operations W.P. Keane, N.K. Shupe, P.B. Sun, T. Robbins, and R. W. Campagna May 9, 1977 2012-07-03
Forum 33 Simulated and Natural Icing Tests of an Ice-protected UH-1H P.F. Kitchens and R. I. Adams May 9, 1977 2012-07-03
Forum 33 Advancing Blade Concept (ABC) TM Dynamics J. T. L. Abbe, R. H. Blackwell, and D. S. Jenney May 9, 1977 2012-07-03
Forum 33 The YUH-61A Tail Rotor: Development of a Stiff Inplane Bearingless Flexstrap Design J. Shaw Jr. and W. T. Edwards May 9, 1977 2012-07-03
Forum 33 Helicopter Vibration Requirements D. P. Schrage and R. E. Peskar May 9, 1977 2012-07-03
Forum 33 An Analytical Model for Describing the Response of an Unsymmetrical Rotor S. P. Viswanathan, A. W. Myers, and T.T. McLarty May 9, 1977 2012-07-03
Forum 33 A Transfer Function Method for Dynamic Stability Measurement W. Johnson May 9, 1977 2012-07-03
Forum 33 Relaxation of Rotor Limitations by Feedback Control M. Kretz May 9, 1977 2012-07-03
Forum 33 An Exploratory Investigation of the Effects of Large Variations in Rotor Systems Dynamics Design Parameters on Helicopter Handling Characteristics in NOE Flight R.T.N. Chen and P.D. Talbot May 9, 1977 2012-07-03
Forum 33 Parameter Identification of a Hingeless Rotor Helicopter O. Rix, H. Huber, and J. Kaletka May 9, 1977 2012-07-03
Forum 33 The Basic Flying Characteristics of the Rotor Systems Research Aircraft F. L. Moore and J. Occhiato May 9, 1977 2012-07-03
Forum 33 Digital Flight Control Design for a Tandem-Rotor Helicopter R. F. Stengel, J. R. Broussard, and P. W. Berry May 9, 1977 2012-07-03
Forum 33 Dynamic Stability and Control Characteristics of the Aerocrane Hybrid Heavy Lift Vehicle H.C. Curtiss Jr., W.F. Putman, and J.J. Traybar May 9, 1977 2012-07-03
Forum 33 UH-60 Handling Qualities D.E. Cooper and L. S. Cotton May 9, 1977 2012-07-03
Forum 33 Titanium Spar Manufacturing Development for Helicopter Blades L. R. Burroughs and S. A. Vitolo May 9, 1977 2012-07-03
Forum 33 Rotor Blade Bonding, Manufacturing and Tooling Development D. J. Ianniello and P. J. Jesson May 9, 1977 2012-07-03
Forum 33 Advanced Cladding for Helicopter Rotors D.P. Huey and A.R. Stetson May 9, 1977 2012-07-03
Forum 33 Computer Aided Process Planning R.C. Read Jr. May 9, 1977 2012-07-03
Forum 33 Automated Layup of Composite Structures E. Frank May 9, 1977 2012-07-03
Forum 33 Acoustic Emission Detection of Damage Occurring in Dynamically Loaded Fiberglass/Epoxy Laminates S.D. Lantieri May 9, 1977 2012-07-03
Forum 33 Icing Trials on the Front Fuselage and Engine Intakes of Helicopters at Conditions Simulating Forward Flight P.F. Ashwood and R. D. Swift May 9, 1977 2012-07-03
Forum 33 A Program for Increased Flight Fidelity in Helicopter Simulation LT C. W. Woomer, USN, and G. D. Carico May 9, 1977 2012-07-03
Forum 33 Summary of Helicopter Airframe Testing in the Shipboard Environment H.G. Kolwey May 9, 1977 2012-07-03
Forum 33 Status Report on XV-15 Tilt Rotor Test Program, LTC J.H. Brown Jr. and H.K. Edenborough May 9, 1977 2012-07-03
Forum 33 AEFA/Boeing Demonstration of the Effectivity of the YUH-61A in Moderate Icing Conditions MAJ J.F. Hagen, D.V. Lewis, and J.S. Reid May 9, 1977 2012-07-03
Forum 33 Blade Inspection System W.L. McKeown May 9, 1977 2012-07-03
Forum 33 Improved Analytical Design Technique for Low Power Loss Engine Inlets E.H. Staudt and F.B. Wagner, III May 9, 1977 2012-07-03
Forum 33 Advanced Design Infra-Red Suppressors for Turboshaft Engines W.H. Barlow and A. Petach May 9, 1977 2012-07-03
Forum 33 Simulated Flight Endurance Testing of a Small Helicopter Turboshaft Engine W.L. Flood and J.N. Cartwright May 9, 1977 2012-07-03
Forum 33 Development and Evaluation of a Method for Predicting the Vibration and Noise of Helicopter Transmissions, M.A. Bowes May 9, 1977 2012-07-03
Forum 33 A Design Handbook for Helicopter Transparent Enclosures B.F. Kay & J.H. McGarvey May 9, 1977 2012-07-03
Forum 33 Composite Rotor Hub R.J. Mayerjak and G.T. Singley, III May 9, 1977 2012-07-03
Forum 33 Application of an Empirical Fatigue Design Method to Predict Fatigue Life During a Development Program J.P. Norvell May 9, 1977 2012-07-03
Forum 33 Minimized Fuselage Vibrations Using Advanced Composites E.C. Durchlaub May 9, 1977 2012-07-03
Forum 33 Airframe Design of the S-76 Helicopter W. Whiteside and J.D. Ray May 9, 1977 2012-07-03
Forum 33 ZE41: A Magnesium Alloy with Improved Mechanical Properties for Use in Helicopter Transmission Castings M.J. Miles May 9, 1977 2012-07-03
Forum 34 Analytic Investigation of Advancing Blade Drag Reduction by Tip Modifications Tauber, Michael E., NASA May 15, 1978 2012-12-03
Forum 34 Full-Scale Wind Tunnel Test of a Modern Helicopter Main Rotor - Investigation of Tip Mach Number Effects and Comparisons of Four Tip Shapes Robert M. Stroub May 15, 1978 2012-12-03
Forum 34 Full-Scale Wind Tunnel Test of a Modern Helicopter Main Rotor Correlation with Model Rotor Test Data and with Theory Balch, David T., Sikorsky May 15, 1978 2012-12-03
Forum 34 Rotor Airfoil Optimization: An Understanding of the Physical Limits Leo Dadone, Boeing Vertol Company May 15, 1978 2012-12-03
Forum 34 Rotor Airfoil Flight Investigation: Preliminary Results Morris, Charles E. K. Jr., NASA May 15, 1978 2012-12-03
Forum 34 Aerodynamic Design of the Sikorsky S-76 Helicopter Fradenburgh, Evan A., Sikorsky Aircraft May 15, 1978 2012-12-03
Forum 34 Design and Development Tests of a Four-Bladed Light Helicopter Rotor System Cresap, Weesley L., Bell Helicopter Textron May 15, 1978 2012-12-03
Forum 34 What are the Lift and Propulsive Force Limits at High Speed for the Conventional Rotor? McHugh, Frank J., Boeing Vertol Company
May 15, 1978 2021-28-01
Forum 34 What are the Lift and Propulsive Force Limits at High Speed for the Conventional Rotor? McHugh, Frank J., Boeing Vertol Company
May 15, 1978 2018-17-07
Forum 34 The Sizing of a V/STOL Aircraft for Multimission Application Spencer, John W., Rockwell International May 15, 1978 2012-12-03
Forum 34 High Performance VTOL For Over-the-Horizon Targeting Schwoerer, Roger F., Grumman Aerospace Corporation May 15, 1978 2012-12-03
Forum 34 Helicopters for Interplanetary Space Flight MacNeal, Richard H., The MacNeqal-Schwendler Corporation; Hedgepeth, John M., Astro Research Corporation May 15, 1978 2016-21-10
Forum 34 Helicopters for Interplanetary Space Flight MacNeal, Richard H., The MacNeqal-Schwendler Corporation; Hedgepeth, John M., Astro Research Corporation May 15, 1978 2012-12-03
Forum 34 Rotor Systems Research Aircraft (RSRA) Emergency Escape System Bement, Laurence J., NASA May 15, 1978 2012-12-03
Forum 34 Helicopter Combat Mission Simulator Milelli, Joseph R., Martin Marietta Aerospace May 15, 1978 2012-12-03
Forum 34 Multiplex System for the Hughes Advanced Attack Helicopter - YAH-64 Booth, Frank, Hughes Helicopters; Espen, David, Sperry Flight Systems May 15, 1978 2012-12-03
Forum 34 Fly-by-Wire for Vertical Lift McManus, Bruce, L., Boeing Vertol Company May 15, 1978 2012-12-03
Forum 34 Pilot Night Vision System (PNVS) For Advanced Attack Helicopter (AAH) Tsoubanos, Chris M., US Army Avionics Research and Development Activity; Kelley, Michael B., US Army Night Vision and Electro-Optical Laboratory May 15, 1978 2012-12-03
Forum 34 A Versitile Approach to Cockpit Management Nieuwsma, Harlan J., Cockpit Management Systems; Cramer, Robert L., Rockwell International May 15, 1978 2012-12-03
Forum 34 Development of a Solid State Vertical Instrument Display System Meek, Thomas B. Jr., United Technologies Corporation May 15, 1978 2012-12-03
Forum 34 A Comparison of Predicted and Experimental Rotor Loads to Evaluate Flap-Lag Coupling with Blade Pitch Hansford, Robert E., Westland Helicopters Ltd. May 15, 1978 2012-12-03
Forum 34 Environmental Vibration Testing of Helicopter Stores and Equipment to the Procedures Outlined in MIL-STD-810C Schrage, Daniel P., U.S. Army; Lutz, Robert H., U.S. Army May 15, 1978 2012-12-03
Forum 34 An Aeromechanical Stability Analysis for Bearingless Rotor Helicopters Hodges, Dewey H., AVRADCOM May 15, 1978 2012-12-03
Forum 34 Examination of the Air Resonance Stability Characteristics of a Bearingless Main Rotor White, Richard P. Jr., Systems Research Laboratories, Inc.; Nettles, William E., AVRADCOM May 15, 1978 2012-12-03
Forum 34 Sikorsky S-76 Analysis, Design, and Development for Successful Dynamic Characteristics Niebanck, C., United Technologies Corporation; Girvan, W., United Technologies Corporation May 15, 1978 2012-12-03
Forum 34 Antiresonant Rotor Isolation for Vibration Reduction Desjardins, Rene A., Boeing Vertol Company; Hooper, Euan W., Beoing Vertol Company May 15, 1978 2012-12-03
Forum 34 Lag Damping in Autorotation by a Perturbation Method Wei, F-S, Washington University; Peters, D. A., Washington University May 15, 1978 2012-12-03
Forum 34 Handling Qualities - Aspects of the Bell Model 222 Design and Development Program Hester, M. L., Bell Helicopter Textron; Popelka, D. A., Bell Helicopter Textron; Maahs, D. C. Sr, Bell Helicopter Textron May 15, 1978 2012-12-03
Forum 34 Analytical Design of a High Performance Stability and Control Augmentation System for a Hingeless Rotor Helicopter Miyajima, Katsuyuki, NASA May 15, 1978 2012-12-03
Forum 34 Simulation of Automatic Flight Control System Failures Batra, N. N., Bell Helicopter Textron; Builta, K. E., Bell Helicopter Textron, Davis, J. M., AVRADCOM May 15, 1978 2012-12-03
Forum 34 A Piloted Simulator Investigation of Augmentation Systems to Improve Helicopter Nap-of-the-Earth Handling Qualities Chen, Robert T. N., Rotorcraft Flight Dynamics; Talbot, Peter D.; Gerdes, Ronald M., NASA; Dugan, Daniel C., NASA May 15, 1978 2012-12-03
Forum 34 Rotorcraft System Identification Techniques for Handling Qualities and Stability and Control Evaluation Hall, Earl W. Jr., Systems Control, Inc.; Gupta, Narendra K., Systems Control, Inc.; Hansen, Raymond S., Systems Control, Inc. May 15, 1978 2012-12-03
Forum 34 Handling Qualities of Army/Hughes YAH-64 Advanced Attack Helicopter Amer, K. B., Hughes Helicopters; Prouty, R. W., Hughes Helicopters; Walton, R. P., Hughes Helicopters; Engle, J. E., Sperry Flight Systems May 15, 1978 2012-12-03
Forum 34 Inertia Welding of YAH-64 Main Rotor Drive Shaft Leach, J. E. Jr., Hughes Helicopters May 15, 1978 2012-12-03
Forum 34 Service Quality Optimization: Engineering Production and Quality Control Converging Actions Sappa, A., Aerospatiale Helicopter Division May 15, 1978 2012-12-03
Forum 34 Ultrasonic Bonding - Panacea or Pie in the Sky Devine, Janet, Sonobond Corporation; Dingle, Gordon H., Hughes Helicopters; Vollmer, Robert G., US Army May 15, 1978 2012-12-03
Forum 34 Practical Application of Gel Permeation Chromatography Milon, Paul, Boeing Vertol Company; Rohner, Martin J., Boeing Vertol Company May 15, 1978 2012-12-03
Forum 34 Filament Wound Main Rotor Blade - The Army's New Production Blade for the AH-1 White, Mark L., Kaman Aerospace Corporation May 15, 1978 2012-12-03
Forum 34 The 214 Fiberglass Blade - Design for Inspectability Phillips, Nolan, Bell Helicopter Textron; Covington, C. E., Bell Helicopter Textron May 15, 1978 2012-12-03
Forum 34 Use of Helicopter Flight Simulation for Height-Velocity Test Predictions and Flight Test Risk Reduction Benson, Geoffrey, Boeing Vertol Company; Bumstead, Richard, Boeing Vertol Company; Hutto, A. J., Boeing Vertol Company May 15, 1978 2012-12-03
Forum 34 An Innovative Technique for Static and Dynamic V/STOL Testing Lewis, Ernest L., Naval Air Systems Command; Culpepper, Richard G., NASA; Hancock, Virgil R., Rockwell International Corporation May 15, 1978 2012-12-03
Forum 34 Testing of the Tow Missile-Configured AH-1T Helicopter Cash, Daniel G., Naval Air Test Center May 15, 1978 2012-12-03
Forum 34 Generalizing Helicopter Flight Test Performance Data (GENFLT) Boirun, Barclay H., US Army May 15, 1978 2012-12-03
Forum 34 Electronic Control for Helicopter Engines Caine, D. A., Lucas Aerospace; Rumford, K. J., AVCO/Lycoming May 15, 1978 2012-12-03
Forum 34 Damage Tolerant Design of the YAH-64 Drive System Edwards, Albert C., Hughes Helicopters; Neugebauer, Hughes Helicopters May 15, 1978 2012-12-03
Forum 34 800 Shaft Horsepower Advanced Technology Demonstrator Engine Elliott, G. A., AVRADCOM; Furgurson, R. G., AVRADCOM May 15, 1978 2012-12-03
Forum 34 Definition and Analytical Evaluation of a Power Management System for Tilt-Rotor Aircraft Morris, James J., Boeing Vertol Corporation; Alexander, Harold R., Boeing Vertol Corporation May 15, 1978 2012-12-03
Forum 34 Loss-of-Lubrication Operation of Helicopter Transmissions Hudgins, Wayne A., US Army; Schuetz, Harold A., US Army May 15, 1978 2012-12-03
Forum 34 Overstress Testing of Helicopter Transmissions Cormier, Kenneth R., Sikorsky Aircraft May 15, 1978 2012-12-03
Forum 34 Investigation of the Crash Impact Characteristics of Composite Airframe Structures Cronkhite, J. D., Haas, T. J., Bell Helicopter Textron; Winter, R., Cairo, R. R., Grumman Aerospace Corporation; Singley, G. T. III, AVRADCOM May 15, 1978 2012-12-03
Forum 34 Spacewound Composite Structures Good, Danny E., AVRADCOM May 15, 1978 2012-12-03
Forum 34 Composite Wing Technology on the AV-8B Advanced Aircraft Riley, B. L., McDonnell Douglas Corporation May 15, 1978 2012-12-03
Forum 34 The Application of Composites to Secondary Structures Marchinski, Leonard J., Boeing Vertol Company; Greco, Claudius A., Boeing Vertol Company May 15, 1978 2012-12-03
Forum 34 Structural Integrity Recording System for Helicopters Saylor, Duane M., AVRADCOM May 15, 1978 2012-12-03
Forum 34 Digital Simulation of the Operational Loads Survey Flight Tests Van Gaasbeek, James R., Bell Helicopter Textron; Austin, Edward E., USARTL May 15, 1978 2012-12-03
Forum 34 The Aeroelastically Conformable Rotor Concept Blackwell, R. H., United Technologies Corporation; Merkley, D. J., AVRADCOM May 15, 1978 2012-12-03
Forum 34 Wind-Tunnel Test Results of a Full-Scale Multicyclic Controllable Twist Rotor McCloud, John L., NASA; Weisbrich, Alfred L., Kaman Aerospace Corporation May 15, 1978 2012-12-03
Forum 34 Experimental Effects of Tip Shape on Rotor Control Loads Rabbott, John P. Jr., AVRADCOM; Niebanck, Charles, United Technologies Corporation May 15, 1978 2012-12-03
Forum 34 Theoretical Prediction of Dynamic Stall on Oscillating Airfoils Rao, Balusu M., Analytical Methods, Inc.; Maskew, Brian, Analytical Methods, Inc.; Dvorak, Frank A., Analytical Methods, Inc. May 15, 1978 2012-12-03
Forum 34 Onset of Leading Edge Seperation Effects Under Dynamic Conditions and Low Mach Number Beddoes, T. S., Westland Helicopters, Ltd. May 15, 1978 2012-12-03
Forum 34 Flap-Lag-Torsion Aeroelastic Stability of Circulation-Controlled Rotors in Hover Chopra, Inderjit, NASA; Johnson, Wayne, AVRADCOM May 15, 1978 2012-12-03
Forum 35 Effect Of Tip Shape On The Wake Structure And Spanloading Of A 2-Bladed Rotor In Hover

J. Ballard, K.L. Orloff, NASA AMES Research Center & A. Luebs, Gates Learjet Corp.

May 21, 1979 2012-06-03
Forum 35 Helicopter Performance Methodology At Bell Helicopter Textron

F.D. Harris, J.D. Kocurek & T.T. Mclarty, Bell Helicopter Textron

May 21, 1979 2012-06-03
Forum 35 Lifting Surface Method For Hover/Climb Airloads

J.M. Summa, D.R. Clark, Analytical Methods, Inc.

May 21, 1979 2012-06-03
Forum 35 Influence Of Sweep On The Unsteady Loading Of An Oscillating Wing

A.O. St. Hilaire, F.O. Carta, UTC Research Center, W.D. Jepson, Sikorsky Aircraft Div., UTC

May 21, 1979 2012-06-03
Forum 35 Integrated Analytical And Experimental Investigation Of Helicopter Hub Drag A.H. Logan, R. Marthe, Hughes Helicopters & D.R. Clark, Analytical Methods, Inc. & A. Phelps, US Army RTL, Langley May 21, 1979 2012-06-03
Forum 35 Rotor Wake Measurements At Very Low Advance Ratios (Stand-By)

H.R. Velkoff, D. Horak, Ohio State University

May 21, 1979 2012-06-03
Forum 35 Helicopter Obstacle Strike Tolerance

L.T. Burrows, US Army RTL, Eustis & B.P. Gupta, J.E. Brunken, Bell Helicopter Textron

May 21, 1979 2012-06-03
Forum 35 System For Interdisciplinary Analysis - A Key To Improved Rotorcraft Design

A.W. Kerr, J.M. Davis, US Army RTL, Ames

May 21, 1979 2012-06-03
Forum 35 Composite Helicopter Tail Booms

H.J. Brown, Fiber Science, Inc.

May 21, 1979 2012-06-03
Forum 35 Crashworthy Armored Crewseat For The UH-60A Black Hawk

S.P. Desjardins, D.H. Laananen, Simula, Inc. & R.J. Dummer, Norton Co.

May 21, 1979 2012-06-03
Forum 35 Designing With Experimental Mechanics

J. Cernosek, Bell Helicopter Textron

May 21, 1979 2012-06-03
Forum 35 Agricultural Helicopters H.E. Lemont, Bell Helicopter Textron May 21, 1979 2012-06-03
Forum 35 Meeting The Challenge Of Precise Navigation During Nap-Of-The-Earth Flight

S.P. Rogers & K.D. Cross, Anacapa Sciences, Inc.

May 21, 1979 2012-06-03
Forum 35 Helicopter Commands At The Touch Of A Hand

R.D. Gilson, Ohio State University, P.S. Sun, US Army Electronics Command & R.S. Dunn, US Army RTL, Ames

May 21, 1979 2012-06-03
Forum 35 Multiplex Technology Applied To Helicopters

L.A. Frazer, J.H. Emery, Bell Helicopter Textron

May 21, 1979 2012-06-03
Forum 35 Antennas For The Black Hawk

M.L. Parent, Sikorsky Aircraft Div, UTC

May 21, 1979 2012-06-03
Forum 35 Advances In Decelerating Steep Approach And Landing For Helicopter Instrument Approaches

P.S. Demko, J.H. Boschma, US Army Avionics R & D Activity

May 21, 1979 2012-06-03
Forum 35 Helmet Mounted Display And Sight Technology Development

C.J.G. Lewis, Marconi Avionics, LTD.

May 21, 1979 2012-06-03
Forum 35 Dynamics Of A Helicopter--Slung Load System

P. Sampath & Dr. J.B. Barlow, University Of Maryland

May 21, 1979 2012-06-03
Forum 35 Dynamics Requirements For An Advanced Scout Helicopter (ASH) D.P. Schrage & R.A. Wolfe, US Army AVRADCOM May 21, 1979 2012-06-03
Forum 35 Theoretical Flap-Lag Damping With Various Dynamic Inflow Models

D.A. Peters, Washington University & G.H. Gaonkar, India Institute Of Science

May 21, 1979 2012-06-03
Forum 35 Evaluation Of The Practical Aspects Of Vibration Reduction Using Structural Optimization Techniques

H.W. Hanson, Bell Helicopter Textron & N.J. Calapodas, US Army AVRADCOM

May 21, 1979 2012-06-03
Forum 35 S-76 Helicopter Handling Qualities Design And Development

G.P. Wright & N.D. Lappos, Sikorsky Aircraft Div., UTC

May 21, 1979 2012-06-03
Forum 35 Improved Method Of Predicting Helicopter Control Response And Gust Sensitivity F. White & B.B. Blake, Boeing Vertol Co. May 21, 1979 2012-06-03
Forum 35 Piloted Simulator Investigation Of Helicopter Control Systems Effects On Handling Qualities During Instrument Flight

R.D. Forrest, FAA & R.T.N. Chen, R.M. Gerdes, T.S. Alderete, D.R. Gee, NASA AMES Research Center

May 21, 1979 2012-06-03
Forum 35 Development Of A Fly-By-Wire Elevator For The Bell Helicopter Textron 214ST

S.W. Ferguson & K.E. Builta, Bell Helicopter Textron

May 21, 1979 2012-06-03
Forum 35 Advanced Scout Helicopter Flying Qualities Requirements--How Realistic Are They?

D.M. Pitt & F.E. Heacock, US Army AVRADCOM

May 21, 1979 2012-06-03
Forum 35 Handling Quality And Display Requirements For Low Speed And Hover In Reduced Flight Visibility

R.H. Hoh & I.L. Ashkenas, Systems Technology, Inc.

May 21, 1979 2012-06-03
Forum 35 Role Of Numerical Control Design In The Computer Aided Design/Manufacturing Interface At Sikorsky

G.O. Pranspill, Sikorsky Aircraft Div., UTC

May 21, 1979 2012-06-03
Forum 35 Model 206L Composite Litter Door

J.D. Crist, Bell Helicopter Textron

May 21, 1979 2012-06-03
Forum 35 Determining The Contour Of Helicopter Rotor Blades Automatically Using Electro-Optical Techniques

A. Pellman, Dreyfus-Pellman Corp. & T.J. Pojeta, US Army AVRADCOM

May 21, 1979 2012-06-03
Forum 35 Superplastic Forming/Diffusion Bonding Of Titanium Helicopter Airframe Components

B.A. Burroughs, Rockwell Intl & N.J. Mocerino, Hughes Helicopters Metal Matrix Composites

May 21, 1979 2012-06-03
Forum 35 Metal Matrix Composites R.L. Pinckney, Boeing Vertol Co. May 21, 1979 2012-06-03
Forum 35 Automatic Scanning Inspection Of Composite Helicopter Structures Using An Advanced Technology Fluoroscope System

R.H. Porter & B.J. Hunter, Bell Helicopter Textron

May 21, 1979 2012-06-03
Forum 35 Computer Assisted High Speed Balancing Of T53 And T55 Power Turbines

T.J. pojeta, US Army AVRADCOM & T.J. Walter, Mechanical Technology, Inc.

May 21, 1979 2012-06-03
Forum 35 Influence Of Engine/Fuel Control Design On Helicopter Dynamics And Handling Qualities

W.A. Kuczynski, D.E. Cooper, W.J. Twomey, & J.J. Howlett, Sikorsky Aircraft Div., UTC

May 21, 1979 2012-06-03
Forum 35 Rotorshaft Torquemeter

R.B. Bossler, Kaman Aerospace Corp.

May 21, 1979 2012-06-03
Forum 35 Self-Contained Grease Lubrication Systems For Aircraft Applications

A.S. Irwin, Marlin-Rockwell Corp & C.F. Inglee, J. Lenski, Boeing Vertol Co.

May 21, 1979 2012-06-03
Forum 35 Ground Test Vehicle Testing

H.D. Jones, US Army AVRADCOM

May 21, 1979 2012-06-03
Forum 35 Application Of Finite-Element And Holographic Techniques In The Design Of Turboshaft Engine Components P.S. Kuo, Avco Lycoming Div. May 21, 1979 2012-06-03
Forum 35 Development Of A No Adjustment Turboshaft Engine Control System

J.J. Curran & A.M. Levine, General Electric Co.

May 21, 1979 2012-06-03
Forum 35 Certification Of Composites In Civil Aircraft

R. Allen & J.R. Soderquist, FAA

May 21, 1979 2012-06-03
Forum 35 Qualification Program Of The Composite Main Rotor Blade For The 214B Helicopter D.J. Reddy, Bell Helicopter Textron May 21, 1979 2012-06-03
Forum 35 Operation And Test Of Composite Horizontal Stabilizer For The S-76 Helicopter

J.D. Ray, Sikorsky Aircraft Div, UTC

May 21, 1979 2012-06-03
Forum 35 Design And Development Of A Hybrid Composite Rotor Blade For The Circulation Control Rotor System

G.A. Mccoubrey, Kaman Aerospace Corp.

May 21, 1979 2012-06-03
Forum 35 Search For A Consistent Method Of S-N Curve Construction With Limited Test Data

W.D. Harris, Hughes Helicopters

May 21, 1979 2012-06-03
Forum 35 Sikorsky Elastomeric Rotor

R. Rybicki, Sikorsky Aircraft Div, UTC

May 21, 1979 2012-06-03
Forum 35 Helicopter Component Environmental Vibration Testing - The Poor Man's Fatigue Test

Dr. S.T. Crews, US Army AVRADCOM

May 21, 1979 2012-06-03
Forum 35 Realization Of A Helicopter Oriented Real Time Data System For Research, Experimental, And Prototype Flight Testing

K. Lunn, C. Hutchinson, Boeing Vertol Co. & J. Obbard, Raytheon Services Co.

May 21, 1979 2012-06-03
Forum 35 Flight Investigation Of Helicopter IFR Approaches To Oil Rigs Using Airborne Weather And Mapping Radar

J.S. Bull, D.M. Hegarty, J.D. Phillips, W.R. Sturgeon, NASA Ames Research Ctr & A.W. Hunting, D. Pate, FAA

May 21, 1979 2012-06-03
Forum 35 Ballistic Design Support Tests - A Key To Helicopter Survivability

A.C. Edwards, Hughes Helicopters

May 21, 1979 2012-06-03
Forum 35 Wind Tunnel And Flight Tests Of The XV-15 Tilt Rotor Research Aircraft

J.A. Weiberg, L.G. Schroers, NASA Ames Research Center & R.L. Marr, S Blackman, Bell Helicopter Textron

May 21, 1979 2012-06-03
Forum 35 Analytical & Experimental Investigation Of V-Type Empennage Contribution To Directional Control In Hover & Forward Flight

C.E. Freeman & W.T. Yeager, US Army RTL, Langley

May 21, 1979 2012-06-03
Forum 35 Design, Analysis, And Testing Of A New Generation Tail Rotor

K.W. Harvey & C.W. Hughes, Bell Helicopter Textron

May 21, 1979 2012-06-03
Forum 35 Ten Years Of Aerospatiale Experience With The Fenestron And Conventional Tail Rotor

R. Mouille, Aerospatiale

May 21, 1979 2012-06-03
Forum 35 Interactional Aerodynamics--A New Challenge In Helicopter Technology

P.F. Sheridan, Boeing Vertol Co. & R.P. Smith, US Army ATL, Eustis

May 21, 1979 2012-06-03
Forum 35 Effect Of Tip Shape On Blade Loading Characteristics For A Two-Bladed Rotor in Hover John D. Ballard and Kenneth L. Orloff, Ames Research Center, NASA; Allen B. Luebs, Gates Lear Corp. May 21, 1979 2018-09-10
Forum 35 The Circulation Control Rotor Flight Demonstrator Test Program Joseph B. Wilkerson and David W. Taylor, Naval Ship Research and Development Center, MD; David R. Barnes and Frank A. Bill, Kaman Aerospace Corp., CT May 21, 1979 2018-09-10
Forum 35 Full Scale Ground and Air Resonance Testing of the Army-Boeing Vertol Bearingless Main Rotor James A. Staley and Richard Gabel, Boeing Vertol Company; H.I. MacDonald, Applied Technology Laboratory, US Army AVRADCOM May 21, 1979 2018-09-10
Forum 35 Experimental Measurements of the Rotating Frequencies and Mode Shapes of a Full Scale Helicopter Rotor in a Vacuum and Correlations with Calculated Results Bill L. Lee, NASA Langley Research Center, VA May 21, 1979 2018-09-10
Forum 35 The Influence of Sweep on the Aerodynamic Loading of an Oscillating NACA 0012 Airfoil A. O. St. Hilaire and F. O. Carta, United Technologies Research Center; W. D. Jepson, Sikorsky Aircraft May 21, 1979 2020-17-03
Forum 36 Dynamic Stall on Advanced Airfoil Sections M.J. McCroskey, K.W. McAllister & W.L. Carr, USA RTL, Aeromechanics Lab & R. Indergand, U.S. Airforce May 13, 1980 2012-06-03
Forum 36 Computerized Three-Dimensional Aerodynamic Design of a Lifting Rotor Blade M.E. Tauber & R.M. Hicks, NASA/Ames Research Center May 13, 1980 2012-06-03
Forum 36 Computerized Three-Dimensional Aerodynamic Design of a Lifting Rotor Blade M.E. Tauber & R.M. Hicks, NASA/Ames Research Center May 13, 1980 2016-29-04
Forum 36 Hover Performance Methodology at Bell Helicopter Textron J.D. Kocurek, F.D. Harris & L.E. Berkowitz, Bell Helicopter Textron May 13, 1980 2012-06-03
Forum 36 Experimental and Analytical Definition of Helicopter Modeling Effects A.H. Logan, Hughes Helicopters, Inc., Dr. Clark, Analytical Methods, A.E.E. Phelps, USA RTL Aeromechanics Lab & F.D. Raitch, USA RTL ATL May 13, 1980 2012-06-03
Forum 36 Rotor/Body Interference Investigation (Robin) - Analysis & Test D.C. Freeman & J.C. Wilson, USA RTL Structures Laboratory May 13, 1980 2018-17-12
Forum 36 Rotor/Body Interference Investigation (Robin) - Analysis & Test D.C. Freeman & J.C. Wilson, USA RTL Structures Laboratory May 13, 1980 2012-06-03
Forum 36 Influence of Rotor Blade Tip Shape on Tip Vortex Shedding - An Unsteady Inviscid Analysis B. Maskew, Analytical Methods, Inc. May 13, 1980 2012-06-03
Forum 36 Helicopter Obstacle Strike Tolerance LeRoy T. Burrows, US Army; John E. Brunken and Bharat P. Gupta, Bell Helicopter Textron
May 13, 1980 2012-06-03
Forum 36 Development of A Twin Turbofan V/STOL Aircraft M.V. Ciminera, Grumman Aerospace Corporation May 13, 1980 2012-06-03
Forum 36 Development of A Heavy Lift Airship (HLA) D.E. Williams, Goodyear Aerospace Corporation May 13, 1980 2012-06-03
Forum 36 Preliminary Evaluation of RSRA Data Comparing Pure Helicopter Auxiliary Propulsion & Compound Helicopter Flight Characteristics P.J. Arcidiacono, J. Occhiato & G. Desimone, Sikorsky Aircraft Div., UTC May 13, 1980 2012-06-03
Forum 36 Mission Potential Derivatives of XV-15 Tilt Rotor VTOL Research Aircraft R.K. Wernicke & K.G. Wernicke, Bell Helicopter Textron & D.C. Borgman, USA AVRADCOM May 13, 1980 2012-06-03
Forum 36 ABC Development Status and Design Considerations for Navy Missions D.J. Halley, Sikorsky Aircraft Div., UTC May 13, 1980 2012-06-03
Forum 36 Development and Evolution of the Circulation Control Rotor D.G. Kirkpatrick, Naval Air Systems Command & D.R. Barnes, Kaman Aerospace Corporation May 13, 1980 2012-06-03
Forum 36 Integrated Avionics System for Tactical Helicopters J.F. Ellis, Sperry Flight Systems, J.H. Emery & R.R. Taylor, Bell Helicopter Textron May 13, 1980 2012-06-03
Forum 36 Achieving Full Benefits of Intergrated Multiplex in the 1980's D.B. Kanaly, Harris Corporation May 13, 1980 2012-06-03
Forum 36 Navigation Errors Encountered Using Weather Mapping Radar for Helicopter IFR Guidance to Oil Rigs J.D. Phillips, J.S. Bull & D.M. Hegarty, NASA/Ames Research Center May 13, 1980 2012-06-03
Forum 36 Advanced Subsystems Status Monitor J.P. McGee, Sikorsky Aircraft Div., UTC May 13, 1980 2012-06-03
Forum 36 Summary of Helicopter Interface Testing of the Digital AN/ASN-123 Tactical Navigation Avionics System in the SH-3H R.S. Blevins, Naval Air Test Center, Patuxent River May 13, 1980 2012-06-03
Forum 36 Helicopter Pilot Performance and Workload Using Integrated Symbology R.H. Wright, USA RTL Aeromechanics Lab May 13, 1980 2012-06-03
Forum 36 Microprocessor Control of Helicopter Weapon Systems F.J. Silverio & D.S. Anttila, Sikorsky Aircraft Div., UTC May 13, 1980 2012-06-03
Forum 36 Coupled Rotor/Airframe Vibration Analysis By A Combined Harmonic - Balance, Impedance - Matching Method T.K. Hsu & D.A. Peters, Washington University in St. Louis May 13, 1980 2012-06-03
Forum 36 Live-Liquid Inertia Vibration Eliminator D.R. Halwes, Bell Helicopter Textron May 13, 1980 2012-06-03
Forum 36 Wind Tunnel Evaluation of Aeroelastically Conformable Rotors R.H. Blackwell, Sikorsky Aircraft Div., W.T. Yeager, USA RTL Structures Lab & P.O. Mirick, USA RTL Applied Technology Lab May 13, 1980 2012-06-03
Forum 36 Aeroelastic Stability Analysis of Hingeless Rotor Helicopters in Forward Flight Using Blade & Airframe Normal Modes R.T. Lytwyn, Boeing Vertol Company May 13, 1980 2012-06-03
Forum 36 Model-Scale Experimental Investigation of Effects of VAR Couplings on Rotor-Body Stability of Soft Inplane Hingeless Rotor in Hover W.G. Bousman, USA RTL Aeromechanics Lab May 13, 1980 2012-06-03
Forum 36 Effects of Rotor-Body Coupling in a Linear Rotorcraft Model D.L. Kunz, USA RTL Aeromechanics Lab May 13, 1980 2012-06-03
Forum 36 X-Wing Stability and Control Development and Wind Tunnel Demonstrator Tests - Helicopter Conversion and Fixed Wing Flight A.J. Potthast, Lockheed California Company May 13, 1980 2012-06-03
Forum 36 Results of A Simulator Investigation of Control System and Display Variations For An Attach Helicopter Mission E.W. Aiken & LTC R.K. Merrill, USA RTL Aeromechanics Lab May 13, 1980 2012-06-03
Forum 36 Flight Test Results for Task Oriented Flying Qualities Evaluation H.J. Pausder, Dipl. Ing & B.L. Gmelin, Dipl. Ing, DFVLR May 13, 1980 2012-06-03
Forum 36 Piloted Simulator Invest/Static Stability & Control Augmentation Effects on Helicopter Handling Qualities for Instrumentation Approach J.V. Lebacqz, NASA/Ames Research Center & R.D. Forrest, FAA May 13, 1980 2012-06-03
Forum 36 Helicopter Gust Alleviation: An Optimal Sampled-Data Approach P.E. Zwicke, United Technologies Research Center May 13, 1980 2012-06-03
Forum 36 Load Snubbing: A Solution to the Problem of Terrain Flying with External Cargo T.S. Garnett Jr. Boeing Vertol Company & T.B. Allardice, USA RTL Applied Technology Lab May 13, 1980 2012-06-03
Forum 36 Measurement of Rotor Blades M.J. Rohner, Boeing Vertol Company May 13, 1980 2012-06-03
Forum 36 Computerized Gear Grinding System Development F.Z. Marcenaro, Bell Helicopter Textron May 13, 1980 2012-06-03
Forum 36 Hybrid Composite Horizontal Stabilizer for CCR UH-2 Helicopter F.B. Clark, Kaman Aerospace Corporation May 13, 1980 2012-06-03
Forum 36 Advancements in Dimensional Inspection of Helicopter Gearbox and Transmission Cases E.V. Maier, Bell Helicopter Textron May 13, 1980 2012-06-03
Forum 36 Tedlar Film Enables Productivity Improvement W.C. Tambussi, Boeing Vertol Company May 13, 1980 2012-06-03
Forum 36 Development of Small Fuel Efficeint Aircraft Engines P.E. Beam Jr., Detroit Diesel Allison, GM May 13, 1980 2012-06-03
Forum 36 Development of Small Fuel Efficeint Aircraft Engines P.E. Beam Jr., Detroit Diesel Allison, GM May 13, 1980 2012-06-03
Forum 36 Regenerative Engine for Helicopter Application A.E. Easterling, USA RTL Applied Technology Lab May 13, 1980 2012-06-03
Forum 36 Regenerative Engine for Helicopter Application A.E. Easterling, USA RTL Applied Technology Lab May 13, 1980 2012-06-03
Forum 36 New Approach to Turboshaft Engine Growth M.A. Compagnon, General Electric Company May 13, 1980 2012-06-03
Forum 36 New Approach to Turboshaft Engine Growth M.A. Compagnon, General Electric Company May 13, 1980 2012-06-03
Forum 36 Requirements for Efficient Small Turbine Engines - Taking up the Challenge R.S. Taylor, Hughes Helicopters, Inc. May 13, 1980 2012-06-03
Forum 36 Requirements for Efficient Small Turbine Engines - Taking up the Challenge R.S. Taylor, Hughes Helicopters, Inc. May 13, 1980 2012-06-03
Forum 36 NDEC-AN Engine Control Concept for Helicopters D.J. Hawes, Bendix Aviation Electric Ltd May 13, 1980 2012-06-03
Forum 36 NDEC-AN Engine Control Concept for Helicopters D.J. Hawes, Bendix Aviation Electric Ltd May 13, 1980 2012-06-03
Forum 36 Advanced Composite Airframe Program (ACAP) Preliminary Design L.T. Mazza, USA RTL Applied Technology Lab & Dr. R. L. Foye, USA RTL Aero Lab May 13, 1980 2012-06-03
Forum 36 Composite Flight Service Evaluation Program For Helicopters D.J. Baker, USA RTL Structures Lab & A.J. Gustafson, USA RTL Applied Technology Lab May 13, 1980 2012-06-03
Forum 36 All Composite Helicopter Airframe Roof Structure M.J. Rich & B.F. Kay, Sikorsky Aircraft Div., UTC May 13, 1980 2012-06-03
Forum 36 Model 206L Composite Vertical Fin R.G. Anderson & J.H. Harse, Bell Helicopter Textron May 13, 1980 2012-06-03
Forum 36 Advanced Structures Concepts R&M/Cost Assessments T.N. Cook, Sikorsky Aircraft Div., UTC & T.E. Condon, USA RTL Applied Technology Lab May 13, 1980 2012-06-03
Forum 36 Conceptual Study of A Highly Survivable Composite Truss Tailboom D.A. Gallian, Bell Helicopter Textron, G.T. McAllister, USA RTL Applied Technology Lab & Dr. M.N. Maheshwari, Brunswick Corporation May 13, 1980 2012-06-03
Forum 36 Substantiation of the Structural Integrity of the YAH-64 Control Actuators with Material Variation W.D. Harris, Hughes Helicopters May 13, 1980 2012-06-03
Forum 36 YCH-47D Tandem Cargo Hook Failure Testing L.J. Hartman, Boeing Vertol Company May 13, 1980 2012-06-03
Forum 36 NASA/FAA Flight Test Investigation of Helicopter Microwave Landing System Approaches L.L. Peach, J.S. Bull, D.J. Anderson, D.C. Dugan & V.L. Ross, NASA Ames, & A.W. Hunting, D.P. Pate, & J.C. Savage, FAA Flight Standards NFO May 13, 1980 2012-06-03
Forum 36 Design and Development Tests of the Model 412 Helicopters W.L. Cresap & A.W. Myers, Bell Helicopter Textron May 13, 1980 2012-06-03
Forum 36 Advancing Blade Concepts (ABC TM) High Speed Development A.J. Ruddell, Sikorsky Aircraft Div., UTC & J.A. Macrino, USA TRL Applied Technology May 13, 1980 2012-06-03
Forum 36 Reducing the Cost Impact of Helicopter Internal Noise Control L.S. Levine, Sikorsky Aircraft Div., UTC May 13, 1980 2012-06-03
Forum 36 Trailing Edge Noise From Hovering Rotors Y.N. Kim, University of Notre Dame & A.R. George, Cornell University May 13, 1980 2012-06-03
Forum 36 Helicopter-Model Scale Results of Blade-Vortex Interaction Impulsive Noise As Affected by Tip Modification D.R. Hoads, USA RTL Structures Lab May 13, 1980 2012-06-03
Forum 36 Acoustic Shock Waves Generated by a Transonic Helicopter Blade M.P. Isom, Polytechnic Institute of New York May 13, 1980 2012-06-03
Forum 36 Economic Impact of Noise Limits on New Design and Current Production Helicopters R.H. Spencer, Boeing Vertol Company May 13, 1980 2012-06-03
Forum 36 Simple System for Helicopter Individual-Blade-Control And Its Application To Gust Alleviation N.D. Ham & R.M. Mckillip Jr., MIT May 13, 1980 2012-06-03
Forum 36 Wind Tunnel Results Showing Rotor Vibratory Loads Reduction Using Higher Harmonic Blade Pitch C.E. Hammond, USA RTL Structures Lab May 13, 1980 2012-06-03
Forum 36 Practical Design Considerations for a Flightworthy Higher Harmonic Control System E.R. Wood & R. W. Powers, Hughes Helicopters May 13, 1980 2012-06-03
Forum 36 Active Control of The Helicopter Rotor for Vibration Reduction J. Shaw And N. Albion, Boeing Vertol Co. May 13, 1980 2012-06-03
Forum 36 Vibration Reduction With Higher Harmonic Blade Feathering for Helicopters With 2-Bladed Teetering and 4-Bladed Hingeless Rotors J.G. Yen, Bell Helicopter Textron May 13, 1980 2012-06-03
Forum 36 Vibration Reduction With Higher Harmonic Blade Feathering for Helicopters With 2-Bladed Teetering and 4-Bladed Hingeless Rotors J.G. Yen, Bell Helicopter Textron May 13, 1980 2021-01-01
Forum 36 Multicyclic Control for Helicopters-Research in Progress at Ames J.L. McCloud, III. NASA Ames Research Center May 13, 1980 2012-06-03
Forum 36 Active Control System for Helicopter Vibration Reduction By Higher Harmonic Pitch R.B. Taylor & F.A. Farrar, United Technologies Research Center & W. Miao, Sikorsky Aircraft Div., UTC May 13, 1980 2012-06-03
Forum 36 Multicyclic Control of a Helicopter Rotor Considering The Influence of Vibration Loads And Control Motion T.J. Brown & J.L. McCloud, III. NASA Ames Research Center May 13, 1980 2012-06-03
Forum 37 Prediction of Dynamic Stall and Unsteady Airloads for Rotor Blades S. Gangwani, UTC Research Center May 17, 1981 2012-06-03
Forum 37 Active Elimination of Stall Conditions M. Kretz, Giravions Dorand Industries May 17, 1981 2012-06-03
Forum 37 Optimization Theory Applied to Higher Harmonic Control of Circulation Controlled Rotors J. Abramson & E. Rogers, David W. Taylor Naval Ship R & D Center May 17, 1981 2012-06-03
Forum 37 The Aerodynamic Influences of Rotor Blade Airfoils, Twist, Taper, and Solidity on Hover and Forward Flight Performance G. Bingham, U.S. Army Structures Laboratory May 17, 1981 2012-06-03
Forum 37 Helicopter Airflow and Wake Characteristics for Low Speed and Hovering Flight from Rocket Interference Investigations A. Landgrebe, R. Taylor, T. Egolf & J. Bennett, UTC Research Center May 17, 1981 2012-06-03
Forum 37 Safety: A Prime Factor in the Design of Aerospatiale's Super-Puma AS 332 E. Lefort, Aerospatiale Helicopter Division (France) May 17, 1981 2012-06-03
Forum 37 An ABC Status Report A. Linden & A. Ruddell, Sikorsky Aircraft Division, UTC May 17, 1981 2012-06-03
Forum 37 An Evaluation of Advanced Rotorcraft Configurations for Emerging Military Applications K. Wernicke & J. Fischer, Bell Helicopter Textron May 17, 1981 2012-06-03
Forum 37 Late 80's Advanced Rotary Wing Aircraft Potential Based on ATDE, ACAP, and ITR J. White, U.S. Army Applied Technology Laboratory May 17, 1981 2012-06-03
Forum 37 Computer Aided Helicopter Design H. Rosenstein & K. Stanzione, Boeing Vertol Company May 17, 1981 2012-06-03
Forum 37 Fiber Optic Technology for Data Transmission in the Helicopter Environment J. Wyatt, F. Snyder & R. Giri, Harris Corporation May 17, 1981 2012-06-03
Forum 37 Fiber Optic Technology for Data Transmission in the Helicopter Environment J. Wyatt, F. Snyder & R. Giri, Harris Corporation May 17, 1981 2020-21-04
Forum 37 Electronic Master Monitor and Advisory Display System R. Kurowsky, U.S. Army Avionics Research & Development Activity, & R. McLane, General Electric Company May 17, 1981 2012-06-03
Forum 37 Comparison of Helicopter Copilot Workload While Using Three Navigation Systems During Nap-Of-The-Earth Flight D. Cote, R. Simmons & G. Krueger, U.S. Army Aeromedical Research Laboratory May 17, 1981 2012-06-03
Forum 37 CH-53 Helicopter Night Vision System Simulation Experiments G. Mowery & R. Milelli, Martin Marietta Corporation, L. McDonald, McDonald & Associates, C. Pentelandolfo, Naval Air Development Center, Warminster, Pa., & Lt. Col. P. Noggle, USMC, Naval Air Systems Command May 17, 1981 2012-06-03
Forum 37 Determination of In-Flight Helicopter Loads N. Giansante & R. Jones, Kaman Aerospace Corporation, & N. Calapodas, U.S. Army Applied Technology Laboratory May 17, 1981 2012-06-03
Forum 37 A Unified Approach to the Optimal Design of Adaptive and Gain Scheduled Controllers to Achieve Minimum Helicopter Rotor Vibration J. Molusis, University of Connecticut, C. Hammond, U.S. Army Applied Technology Laboratory, and J. Cline, U.S. Army Structures Laboratory May 17, 1981 2012-06-03
Forum 37 Full-Scale Wind-Tunnel Test of the Aeroelastic Stability of a Bearingless Main Rotor W. Warmbrodt & J. McCloud, NASA Ames Research Center, M. Sheffler & J. Staley, Boeing Vertol Company May 17, 1981 2012-06-03
Forum 37 Helicopter Trim by Periodic Shooting with Newton-Raphson Iteration D. Peters & A. Izadpanah, Washington University May 17, 1981 2012-06-03
Forum 37 Nonlinear Dynamic Characteristics of the Rotor Bifilar Absorber W. Miao & T. Mouzakis, Sikorsky Aircraft Division, UTC May 17, 1981 2012-06-03
Forum 37 A Flight Investigation of Static Stability, Control Augmentation, and Flight Director Influences on Helicopter IFR Handling Qualities J. Lebacqz & J. Weber, NASA Ames Research Center, & L. Corliss, U.S. Army Aeromechanics Laboratory May 17, 1981 2012-06-03
Forum 37 The Impact on Helicopter Cockpits of Integrated Advanced Flight Controls, Avionics, and Optics E. Diamond & J. Maciolek, Sikorsky Aircraft Division, UTC May 17, 1981 2012-06-03
Forum 37 New Designs for Improved Aerodynamic Stability on Recent Aerospatiale Helicopters P. Roesch & A. Vuillet, Aerospatiale Helicopter Divison (France) May 17, 1981 2012-06-03
Forum 37 A Preliminary Flight Investigation of Cross-Coupling and Lateral Damping for Nap-Of-The-Earth Helicopter Operations L. Corliss & G. Carico, U.S. Army Aeromechanics Laboratory May 17, 1981 2012-06-03
Forum 37 Handling Qualities of the SH-60B Seahawk I. Alansky, R. Faull & J. Skonieczny, Sikorsky Aircraft Division, UTC May 17, 1981 2012-06-03
Forum 37 Factors Influencing the Selection of Tooling and Fabrication Methods in Building a Composite Fuselage J. Barto, Sikorsky Aircraft Division, UTC May 17, 1981 2012-06-03
Forum 37 Factors Influencing the Selection of Tooling and Fabrication Methods in Building a Composite Fuselage J. Barto, Sikorsky Aircraft Division, UTC May 17, 1981 2019-22-03
Forum 37 Manufacturing Methods for a Composite Rotor Blade for the YAH-64 Helicopter R. Kiraly, Hughes Helicopters, & J. Tutka, U.S. Army AVRADCOM May 17, 1981 2012-06-03
Forum 37 Future Challenges in Helicopter Flight/Propulsion Control Integration L. Emerson, Pratt & Whitney Aircraft May 17, 1981 2012-06-03
Forum 37 Advanced Transmission Component Development K. Rosen & H. Frint, Sikorsky Aircraft Division, UTC May 17, 1981 2012-06-03
Forum 37 Suction Fuel Systems for Turbine Powered Aircraft D. Petro, Avco Lycoming Division May 17, 1981 2012-06-03
Forum 37 Exhaust Gas Reingestion During Hover In-Ground Effect M. Jackson & R. House, Sikorsky Aircraft Division, UTC May 17, 1981 2012-06-03
Forum 37 HH-65A Dolphin Engine Condition Monitoring System K. Ehlers, Aerospatiale Helicopter Corporation May 17, 1981 2012-06-03
Forum 37 Projected Power and Specific Fuel Consumption Development of the Rolls Royce Gem Engine A. Sanderson, Rolls Royce Aero Engine Division May 17, 1981 2012-06-03
Forum 37 Designing Safety Into Helicopter Transmissions C. Albrecht, Boeing Vertol Company May 17, 1981 2012-06-03
Forum 37 Some Results from a Crash Energy Absorption Test for Evaluating Composite Fuselage Construction R. Foye, U.S. Army Applied Technology Laboratory, & W. Hodges, U.S. Army Structures Laboratory May 17, 1981 2012-06-03
Forum 37 The Variable Stress Ratio Fatigue Strength Curve M. Symonds, Hughes Helicopters May 17, 1981 2012-06-03
Forum 37 Development of Composite Material Helicopter Structures M. Torres, Aerospatiale Helicopter Division (France) May 17, 1981 2012-06-03
Forum 37 Helicopter External Gondola System J. Porterfield, Kaman Aerospace Corporation, & S. Riggs, U.S. Army Applied Technology Laboratory May 17, 1981 2012-06-03
Forum 37 An Economical Approach to Automated Flight Test Data Reduction S. Walters, Aerospatiale Helicopter Corporation May 17, 1981 2012-06-03
Forum 37 Quarter-Scale Testing of an Advanced Rotor System for the UH-1 Helicopter Captain J. Berry, U.S. Army Structures Laboratory May 17, 1981 2012-06-03
Forum 37 Influence of Sideslip on the Kinematics of the Helicopter in Steady Coordinated Turns R. Chen & J. Jeske, NASA Ames Research Center May 17, 1981 2012-06-03
Forum 37 Reliability and Maintainability Evaluation of Rotor Systems R. Hall, U.S. Army Applied Technology Laboratory, & U. Garganese, Kaman Aerospace Corporation May 17, 1981 2012-06-03
Forum 37 A Piloted Simulation of the Backup Control System Engagement for the YAH-64 C. Blanken, E. Aiken & LTC R. Merrill, U.S. Army Aeromechanics Laboratory, & V. Ross, NASA Ames Research Center May 17, 1981 2012-06-03
Forum 37 Results of Structural Dynamic Testing of the XV-15 Tilt Rotor Research Aircraft J. Bilger, R. Marr & A. Zahedi, Bell Helicopter Textron May 17, 1981 2012-06-03
Forum 37 Helicopter Manufacturers Economic Impact Assessment of FAA Proposed Helicopter Certification Noise Rules (NPRM 79-13) R. Schlegel, Sikorsky Aircraft Division, UTC May 17, 1981 2012-06-03
Forum 37 Detectability and Annoyance of Repetitive Impulsive Sounds Sanford Fidell and Richard Noronjeff, Bolt Beranek and Newman Inc. May 17, 1981 2012-06-03
Forum 37 Prediction of Helicopter Rotor Noise from Measured Blade Surface Pressure G. Succi, Bolt, Beranek and Newman, Inc., & J. Brieger, Bell Helicopter Textron May 17, 1981 2012-06-03
Forum 37 An Evaluation of a Computer Code Based on Linear Acoustic Theory for Predicting Helicopter Main Rotor Noise J. Davis, Sikorsky Aircraft Division, UTC, & T. Egolf, UTC Research Center May 17, 1981 2012-06-03
Forum 37 Acoustic Performance Evaluation of an Advanced UH-1 Helicopter Main Rotor System D. Hoad & D. Conner, U.S. Army Structures Laboratory May 17, 1981 2012-06-03
Forum 38 Theory and Application of Optimum Airloads to Rotors in Hover and Forward Flight R.C. Moffitt, Sikorsky Aircraft Div., UTC May 4, 1982 2012-06-03
Forum 38 A New Transonic Airfoil Design Method and Its Application to Helicopter Rotor Airfoil Design J.C. Narramore & J.G. Yen, Bell Helicopter Textron May 4, 1982 2012-06-03
Forum 38 Recent Advances in Rotor Technology at Boeing Vertol M.A. McVeigh & F.J. McHugh, Boeing Vertol Company May 4, 1982 2012-06-03
Forum 38 Evaluation of an Asympototic Method for Helicopter Rotor Airloads A.R. Vaidyanathan & G.A. Pierce, Georgia Institute of Technology May 4, 1982 2012-06-03
Forum 38 An Evaluation of Vertical Drag and Ground Effect Using the RSRA Rotor Balance System R.J. Flemming, Sikorsky Aircraft Div., UTC and R.E. Erikson, NASA Ames Research Center May 4, 1982 2012-06-03
Forum 38 Effect of Tip Vanes on the Performance and Flow Field of a Rotor in Hover H.R. Velkoff & T.W. Parker, Ohio State University May 4, 1982 2012-06-03
Forum 38 An Experimental Investigation of a Bearingless Model Rotor in Hover S. Dawson, U.S. Army Research and Technology Laboratories May 4, 1982 2012-06-03
Forum 38 Whirl Mode Stability of the Main Rotor of the YAH-64 Advanced Attack Helicopter L.J. Silverthorn, Hughes Helicopters, Inc. May 4, 1982 2012-06-03
Forum 38 Helicopter Vibration Reduction by Rotor Blade Modal Shaping R.B. Taylor, United Technologies Research Center May 4, 1982 2012-06-03
Forum 38 Correlation of Predicted Vibrations and Test Data for a Wind Tunnel Helicopter Model R. Sopher & S. Kottapalli, Sikorsky Aircraft Div., UTC May 4, 1982 2012-06-03
Forum 38 Wind Tunnel Modeling of Rotor Vibratory Loads R. Gabel, M. Sheffler, F. Tarzanin & D. Hodder, Boeing Vertol Company May 4, 1982 2012-06-03
Forum 38 Finite Element Analysis for Bearingless Rotor Blade Aeroelasticity N.T. Sivaneri, Stanford University and I. Chopra, University of Maryland May 4, 1982 2012-06-03
Forum 38 Civil Helicopter Propulsion System Reliability and Engine Monitoring Technology Assessments J.A. Murphy, Bell Helicopter Textron and J. Zuk, Ames Research Center May 4, 1982 2012-06-03
Forum 38 Adaptive Fuel Control Feasibility Investigation R.L. Bolton, U.S. Army Research and Technology Laboratories May 4, 1982 2012-06-03
Forum 38 800 Shaft Horsepower Advanced Technology Demonstrator Engine (ATDE) Status Update D.B. Cale, U.S. Army Research and Technology Laboratories May 4, 1982 2012-06-03
Forum 38 TF 34 Convertible Engine System Technology Program K.L. Abdalla, NASA Lewis and A. Brooks, General Electric Company May 4, 1982 2012-06-03
Forum 38 Digital Full Authority Controls for Helicopter Engines E.S. Eccles, Dowty & Smiths Industries Controls Limited May 4, 1982 2012-06-03
Forum 38 Tandem Rotor Helicopter Characteristics in a Continuous Icing Environment P.J. Dunford, Boeing Vertol Company May 4, 1982 2012-06-03
Forum 38 An Evaluation of Helicopter Autorotation Assist Concepts A.H. Logan & R.D. Graves, Hughes Helicopters, Inc. and G.T. White, U.S. Army Applied Technology Laboratories May 4, 1982 2012-06-03
Forum 38 Predesign Study for an Advanced Flight Research Rotor R. Blackwell & T. Cambell Sikorsky Sircraft Div., UTC and R. Taylor, United Technologies Research Center May 4, 1982 2012-06-03
Forum 38 Sikorsky ACAP Preliminary Design B.F. Kay, Sikorsky Aircraft Div., UTC May 4, 1982 2012-06-03
Forum 38 Conceptual Design of the LHX Integrated Cockpit R.R. Pruyn & R.E. Domenic, Boeing Vertol Company May 4, 1982 2012-06-03
Forum 38 The YAH-64 Empennage and Tail Rotor - A Technical History R.W. Prouty & K.B. Amer, Hughes Helicopters, Inc. May 4, 1982 2012-06-03
Forum 38 Future Helicopter Cockpit Design S.D. Roy, Westland Helicopters May 4, 1982 2012-06-03
Forum 38 Concept Demonstration of Automatic Subsystem Parameter Monitoring R.V. Kurowsky, U.S. Army, AVRADA and M.S. Randolph, General Electric Company May 4, 1982 2012-06-03
Forum 38 Flight Test Evaluation of a Video Tracker for Enhanced Offshore Airborne Radar Approach Capability G.R. Clary, NASA Ames Research Center and P.G. Cooper, Cooper Avionics May 4, 1982 2012-06-03
Forum 38 Demonstration of Radar Reflector Detection and Ground Clutter Suppression Using Airborne Weather and Mapping Radar D.J. Anderson & J.S. Bull, NASA Ames Research Center and J.P. Chisholm, University of Nevada May 4, 1982 2012-06-03
Forum 38 Micro Heads-Up-Display J.R. Goodman & H.W. Upton, Research Electronics May 4, 1982 2012-06-03
Forum 38 Avionics Systems for Helicopter Integration D. Nelson, Collins Government Avionics Division, Rockwell International May 4, 1982 2012-06-03
Forum 38 NASA/FAA Helicopter ATC Simulation Investigation of RNAV/MLS Instrument Approaches L.L. Peach, L. Tobias & H.Q. Lee, NASA Ames Research Center May 4, 1982 2012-06-03
Forum 38 Hip and Heat Treated Titanium Castings for Forged Helicopter Component Replacement E.J. Sauer & S.M. Silverstein, Sikorsky Aircraft Div., UTC May 4, 1982 2012-06-03
Forum 38 Hip and Heat Treated Titanium Castings for Forged Helicopter Component Replacement E.J. Sauer & S.M. Silverstein, Sikorsky Aircraft Div., UTC May 4, 1982 2012-06-03
Forum 38 Adaptation of Pultrusion to the Manufacture of Helicopter Components E. Blake, Bell Helicopter Textron and N. Tessier, AMMRC May 4, 1982 2012-06-03
Forum 38 Adaptation of Pultrusion to the Manufacture of Helicopter Components E. Blake, Bell Helicopter Textron and N. Tessier, AMMRC May 4, 1982 2012-06-03
Forum 38 In-Motion Radiographic Inspection of Titanium Spar Tube Welds R.J. Milne, Sikorsky Aircraft Div., UTC May 4, 1982 2012-06-03
Forum 38 In-Motion Radiographic Inspection of Titanium Spar Tube Welds R.J. Milne, Sikorsky Aircraft Div., UTC May 4, 1982 2012-06-03
Forum 38 Development of the Sea King Composite Main Rotor Blade R. Sanders & P. Grainger, Westland Helicopters, Ltd. May 4, 1982 2012-06-03
Forum 38 Development of the Sea King Composite Main Rotor Blade R. Sanders & P. Grainger, Westland Helicopters, Ltd. May 4, 1982 2012-06-03
Forum 38 Computer Aided Coordinate Measuring Systems J.W. Nastri, Sikorsky Aircraft Div., UTC May 4, 1982 2012-06-03
Forum 38 Computer Aided Coordinate Measuring Systems J.W. Nastri, Sikorsky Aircraft Div., UTC May 4, 1982 2012-06-03
Forum 38 The Impact of Advanced Technology of VTOL Systems Upon Existing Product Support R.E. Walkup, Aerospatiale Helicopter Corporation May 4, 1982 2018-01-06
Forum 38 The Impact of Advanced Technology of VTOL Systems Upon Existing Product Support R.E. Walkup, Aerospatiale Helicopter Corporation May 4, 1982 2012-06-03
Forum 38 The Impact of Advanced Technology of VTOL Systems Upon Existing Product Support R.E. Walkup, Aerospatiale Helicopter Corporation May 4, 1982 2012-06-03
Forum 38 Ringfin Augmentation Effects H.E. Lemont, Bell Helicopter Textron May 4, 1982 2012-06-03
Forum 38 Performance of the Rotor Systems Research Aircraft Calibrated Rotor Loads Measurements System C.W. Acree Jr., NASA Ames Research Center May 4, 1982 2012-06-03
Forum 38 Error Minimization in Ground Vibration Testing E.J. Nagy, Kaman Aerospace Corporation May 4, 1982 2012-06-03
Forum 38 Results of the AH-64 Structural Demonstration K.R. Spruer, Hughes Helicopters, Inc. May 4, 1982 2012-06-03
Forum 38 Evaluation of an Automatic Subsystem Parameter Monitor R.V. Kurowsky & A.S. Santanelli, U.S. Army Avionics R&D Activity May 4, 1982 2012-06-03
Forum 38 The Prediction of Helicopter Rotor Discrete Frequency Noise F. Farrasat, NASA Langley & G.P. Succi, Bolt, Beranek & Newman May 4, 1982 2021-30-04
Forum 38 The Prediction of Helicopter Rotor Discrete Frequency Noise F. Farrasat, NASA Langley & G.P. Succi, Bolt, Beranek & Newman May 4, 1982 2012-06-03
Forum 38 A Semi-Empirical High-Speed Rotor Noise Prediction Technique K.R. Shenoy, Bell Helicopter Textron May 4, 1982 2012-06-03
Forum 38 Dynamic Surface Measurements on a Model Helicopter Rotor During Blade Slap at High Angles of Attack J.E. Hubbard Jr. & W.L. Harris, Massachusetts Institute of Technology May 4, 1982 2012-06-03
Forum 38 Helicopter Model Scale Results of Blade Vortex Interaction Impulsive Noise as Affected by Blade Planform D.A. Conner & R.D. Hoad, AVRADCOM May 4, 1982 2012-06-03
Forum 38 VTOL and VSTOL Handling Qualities Specifications An Overview Of The Current Status Kevin W. Goldstein, Aerospace Engineer, Naval Air Development Center May 4, 1982 2018-03-10
Forum 38 Applications Of System Identification Methods To The Prediction Of Helicopter Stability, Control And Handling Characteristics G.D. Padfield, RAE Bedford, UK; R.W. DuVal, NASA - Ames Research Center May 4, 1982 2018-03-10
Forum 38 A Pilot-In-The-Loop Analysis Of Several, Kinds Of Helicopter Acceleration-Deceleration Maneuvers Robert K. Heffley, Principal Research Engineer, Systems Technology, Inc. May 4, 1982 2018-03-10
Forum 38 Past Applications And Future Potential Of Variable Stability Research Helicopters William S. Hindson, Joint Institute of Aeronautics and Acoustics, Stanford University May 4, 1982 2018-03-10
Forum 38 Helicopter Simulation Technology- An Ames Research Center Perspective Richard S. Bray, Ames Research Center, NASA, CA May 4, 1982 2018-03-10
Forum 38 New Developments In Flying Qualities Criteria With Application To Rotary Wing Aircraft Roger H. Hoh, Principal Research Engineer, Systems Technology, Inc. May 4, 1982 2018-03-10
Forum 38 Integrated Cockpit For A-129 Dott. Ing. Filippo Reina, Costruzioni Aeronautichs Giovanni Agusta S.p.A., Italy; James A. Gracia and Bryce W. Koth, Harris Government Information Systems Division, Florida May 4, 1982 2018-03-10
Forum 38 Cockpit Integration From A Pilot's Point Of View David L. Green, Vice President, PACER Systems, Inc. May 4, 1982 2018-03-10
Forum 38 The Role Of Voice Technology In Advanced Helicopter Cockpits Howard P. Harper, Sr. Human Factors Engineer, Sikorsky Aircraft Division, United Technologies Corporation, CT May 4, 1982 2018-03-10
Forum 38 Synthesis Of An Integrated Cockpit Management System Joseph A. Dasaro and Charles T. Elliott, Avionics Laboratory, US Army Avionics Research and Development Activity, NJ May 4, 1982 2018-03-10
Forum 38 Performance Evaluation Of A Kinesthetic-Tactual Display Richard J. Jagacinski, Associate Professor; John M. Flach, Graduate Student; and Richard D.Gilson, Professor, The Ohio State University; Richard S. Dunn, Engineering Psychologist, US Army Research and Technology Laboratory May 4, 1982 2018-03-10
Forum 38 Civil (French/U.S.) Certification Of The Coast Guard's HH-65A Dauphin J.C. Hart, Aerospatiale Helicopter Corporation, Texas; J.M. Besse, Societe National Industrielle, Aerospatiale Marignane, France; K.W. McElreath, Rockwell Collins Government Avionics Division, Iowa May 4, 1982 2018-03-10
Forum 38 Boeing 234 Flight Control Development James J. Morris, Technology Manager,Commercial Chinook, Boeing Vertol Company May 4, 1982 2018-03-10
Forum 38 A Helicopter Handling-Qualities Study Of The Effects Of Engine Response Characteristics, Height-Control Dynamics, And Excess Power On Nap-Of-The-Earth Operations Lloyd D. Corliss, US Army Aeromechanics Laboratory, AVRADCOM, NASA Ames Research Center May 4, 1982 2018-03-10
Forum 38 Unified Results Of Several Analytical And Experimental Studies Of Helicopter Handling Qualities In Visual Terrain Flight Robert T.N. Chen, NASA Ames Research Center, CA May 4, 1982 2018-03-10
Forum 38 An Assessment Of Various Side-Stick Controller/Stability And Control Augmentation System For Night Nap-Of-Earth Flight Using Piloted Simulation Kenneth H. Landis, Engineering Specialist, Boeing Vertol Company; and Edwin W. Aiken, Aerospace Engineer, AVRADCOM, Ames Research Center May 4, 1982 2018-03-10
Forum 38 Definition Of Display/Control Requirements For Assault Transport Night/Adverse Weather Capability R. Joseph Milelli and Gary W. Mowery, Program Engineers, Martin Marietta Corporation; and Carmen Pontelandolfo, HNVS Project Engineer, Naval Air Development Center May 4, 1982 2018-03-10
Forum 38 Some Piloting Experiences With Multi Function Isometric Side-Arm Controllers In A Helicopter J. Murray Morgan, Airborne Simulator Facility Manager, National Research Council Canada May 4, 1982 2018-03-10
Forum 38 Influence Of Maneuverability On Helicopter Combat Effectiveness Michael Falco, Senior Staff Scientist, Grumman Aerospace Corporation; Dr. Roger Smith, Aerospace Engineer, US Army Aviation Research and Development Command May 4, 1982 2018-03-10
Forum 38 Flight Tests For The Assessment Of Task Performance And Control Activity Heinz-Jurgen Pausder and Dieter Hummes, DFVLR, Institut fur Flugmechanik, Braunschweig, FRG May 4, 1982 2018-03-10
Forum 38 Results Of NASA/FAA Ground- And Flight-Simulation Experiments Concerning Helicopter IFR Airworthiness Criteria J. Victor Lebacqz, Robert T.N. Chen, Ronald M. Gerdes, and Jeanine M. Weber, NASA Ames Research Center; Raymond D. Forrest, Federal Aviation Administration, NASA Ames Research Center May 4, 1982 2018-03-10
Forum 38 State-Of-The-Art Cockpit Design For The HH-65A Helicopter Daniel E. Castleberry, HX Program Manager, and Marsha Y. McElreath, Avionics Pilot Instructor, Collins Government Avionics Division of Rockwell International, Iowa May 4, 1982 2018-03-10
Forum 39 An Experimental Study of Main Rotor/Tail Rotor/Airframe Interaction in Hover D.T. Balch, Sikorsky Aircraft Division, UTC May 9, 1983 2012-06-03
Forum 39 Synthesized Airfoil Data Method For Prediction of Dynamic Stalls and Unsteady Airloads S.T. Gangwani, Hughes Helicopters, Inc. May 9, 1983 2012-06-03
Forum 39 Considerations in the Estimation of Full Scale Rotor Performance From Model Rotor Test Data M.A. McVeigh, L. Dadone, C.N. Keys, & F.J. McHugh, Boeing Vertol Company May 9, 1983 2012-06-03
Forum 39 High Speed Ice Accretion on Rotorcraft Airfoils R.J. Flemming & D.A. Lednicer, Sikorsky Aircraft Division, UTC May 9, 1983 2012-06-03
Forum 39 Aerodynamic Design of Advanced Rotors With New Tip Shapes J.J. Philippe, ONERA & A. Vuillet, Aerospatiale May 9, 1983 2012-06-03
Forum 39 Aerodynamic Design of the XV-15 Advanced Composite Tilt Rotor Blade M.A. McVeigh & H.J. Rosenstein, Boeing Vertol Company May 9, 1983 2012-06-03
Forum 39 Helicopter Product Liability - A Customer Support View H.B. Epstein & J.D. Knickerbocker, Aerospatiale Helicopter Corporation May 9, 1983 2012-06-03
Forum 39 Aviation Product Assessment As Viewed by the Aviation Research & Development Command E.J. Hollman, U.S. Army Aviation Research & Development Command May 9, 1983 2012-06-03
Forum 39 Influencing Direct Operating Costs: Where and How R.M. Devin, Bell Helicopter Textron May 9, 1983 2012-06-03
Forum 39 T700 Engine - Designed For The Pilot And Mechanic J.F. Wansong, General Electric Company May 9, 1983 2012-06-03
Forum 39 Logistic Challenges of the APACHE ATE V.M. Veeragoudar, Hughes Helicopters, Inc. May 9, 1983 2012-06-03
Forum 39 Black Hawk: A Logistic Success Story T.M. Donahue, Sikorsky Aircraft Division, UTC May 9, 1983 2012-06-03
Forum 39 Development of a Stochastic Model For Fatigue Cracks in Aircraft Structures B.R. Uppaluri & L.J. Marchinski, Boeing Vertol Company May 9, 1983 2012-06-03
Forum 39 A Procedure For the Adjustment of the Endurance Limit of a Component To Account For a Reduction in the Number of Fatigue Test Specimens W.D. Harris, Hughes Helicopters, Inc. May 9, 1983 2012-06-03
Forum 39 Surface Cracking of Quenched and Tempered Steel By Shear Instability - Cause of Premature Fatigue Cracks in Helicopter Main Rotor Spindle Lugs? G. Wold, Det norske Veritas & J. Skaar, Helikopter Service A/S May 9, 1983 2012-06-03
Forum 39 Westland Helicopters' Advanced Technology Fuselage Research Programme T.M.C.H. Bartley, Westland Helicopters, Ltd. May 9, 1983 2012-06-03
Forum 39 Measured and Calculated Inplane Stability Characteristics for an Advanced Bearingless Main Rotor W.H. Weller, Bell Helicopter Textron; R. Peterson, NASA-Ames Research Center May 9, 1983 2012-06-03
Forum 39 Hub Loads Reduction by Modification of Blade Torsional Response S.B.R. Kottapalli, Sikorsky Aircraft Division, UTC May 9, 1983 2012-06-03
Forum 39 Theoretical and Experimental Investigations Into Helicopter Air Resonance S.P. King, Westland Helicopters, Ltd. May 9, 1983 2012-06-03
Forum 39 Evaluation of Helicopter Ride Quality Prediction Methods J.D. Leatherwood & S.A. Clevenson, NASA-Langley Research Center & D.D. Hollenbaugh, U.S. Army Applied Technology Laboratory May 9, 1983 2012-06-03
Forum 39 Materials Deterioration Prevention And Control (MADPAC) J.T. Conroy & W.M. Baker, U.S. Army Aviation Research & Development Command May 9, 1983 2012-06-03
Forum 39 The Integrated Blade Inspection System (IBIS): Program Review and Status L.D. Meyer & R.A. Ekvall, General Electric Company May 9, 1983 2012-06-03
Forum 39 T-700 Blisk/Impeller Cutter Life Improvement Program N. Singh, U.S. Army Troop Support and Aviation Materiel Readiness Command May 9, 1983 2012-06-03
Forum 39 Automated Coordinate Measuring Machine to Inspect Twist and Contour of Main Rotor Blades at Bell Helicopter Textron M.G. Huffman, Bell Helicopter Textron May 9, 1983 2012-06-03
Forum 39 An Innovative Approach to Supplier Cost Control J.M. Rosen, Sikorsky Aircraft Division, UTC May 9, 1983 2012-06-03
Forum 39 Development and Flight Test of a Weather Radar Precision Approach Concept D.J. Anderson, Learfan, Inc., J.P. Chisholm, University of Nevada & G.R. Clary, NASA-Ames Research Center May 9, 1983 2012-06-03
Forum 39 Operation of a Single Channel Sequential NAVSTAR GPS Receiver In a Helicopter Mission Environment F.G. Edwards & J.R. Hamlin, NASA-Ames Research Center May 9, 1983 2012-06-03
Forum 39 Advanced Systems Applications - Foundations for LHX R.E. Parks & T.W. Ingram, Bell Helicopter Textron May 9, 1983 2012-06-03
Forum 39 Sensitivity Analysis of Helicopter IMC Decelerating Steep Approach and Landing Performance To Navigation System Parameters M.S. Karmali & A.V. Phatak, Analytical Mechanics Associates, Inc., J.S. Bull & L.L. Peach, NASA-Ames Research Center & P.S. Demko, U.S. Army May 9, 1983 2012-06-03
Forum 39 Development of Avionic Systems For Future Helicopters R.D. Von Reth, Messerschmitt-Bolkow-Blohm GmbH May 9, 1983 2012-06-03
Forum 39 Development of Large Rotorcraft Transmissions R.J. Drago & J.C. Mack, Boeing Vertol Company & N.E. Samanich, NASA-Lewis Research Center May 9, 1983 2012-06-03
Forum 39 NASA Transmission Research and Its Probable Effects on Helicopter Transmission Design E.V. Zaretsky, J.J. Coy & D.P. Townsend, NASA-Lewis Research Center May 9, 1983 2012-06-03
Forum 39 Convertible Engines For Fold Tilt Rotor Aircraft and ABC Rotorcraft J.C. Gill & J.D. Sauer, Detroit Diesel Allison Division of General Motors Corporation May 9, 1983 2012-06-03
Forum 39 Convertible Fan/Shaft Engine Demonstration G.B. Jasas, Teledyne CAE & J.C. Fourny, Turbomeca May 9, 1983 2012-06-03
Forum 39 Reliability and Maintainability Issues For Future Military Helicopter Engines T.L. House, U.S. Army Research and Technology Laboratory & J.M. Wellborn, General Electric Company May 9, 1983 2012-06-03
Forum 39 XV-15 Shipboard Evaluation J.C. Ball, U.S. Naval Air Test Center May 9, 1983 2012-06-03
Forum 39 Weapon Systems Integration, Test and Evaluation: The LAMPS MK III Experience M.B. Schoultz & O. Wright Jr., IBM Corporation May 9, 1983 2012-06-03
Forum 39 Preliminary Airworthiness Evaluation (PAE) of the Williams Aerial Systems Platform II (WASP II) Individual Lift Device (ILD) D.L. Underwood, U.S. Army Aviation Engineering Flight Activity May 9, 1983 2012-06-03
Forum 39 LHX Simulation - Evaluation of a Cockpit of the Future R.E. Domenic & C.K. Hutchinson, Boeing Vertol Company May 9, 1983 2012-06-03
Forum 39 Contemporary Techniques for Conduct of Helicopter Airframe Fatigue Tests G.R. Howland & J.J. Corso, Sikorsky Aircraft Division, UTC May 9, 1983 2012-06-03
Forum 39 Pneumatic Boot De-Icing System For Helicopters L.A. Haworth, U.S. Army Aviation Engineering Flight Activity May 9, 1983 2012-06-03
Forum 39 Wind Tunnel Test of a Soft, Stiff In-Plane Bearingless Tail Rotor Debashis Banerjee, Hughes Helicopters, Inc. May 9, 1983 2012-06-03
Forum 39 Aerodynamics and Aeroacoustics of Rotating Transonic Flow Fields J.W. Rutherford, U.S. Military Academy May 9, 1983 2012-06-03
Forum 39 Aerodynamics and Aeroacoustics of Rotating Transonic Flow Fields J.W. Rutherford, U.S. Military Academy May 9, 1983 2020-23-03
Forum 39 A Parametric Study of Blade/Vortex Interaction For Two, Three and Four-Bladed Model Rotors at Moderate Tip Speeds: Theory and Experiment K.P. Leighton & W.L. Harris, Massachusetts Institute of Technology May 9, 1983 2012-06-03
Forum 39 Towards A Better Understanding of Helicopter External Noise A. Damongeot, F. D'Ambra & B. Masure, Aerospatiale May 9, 1983 2012-06-03
Forum 39 Statistical Energy Analysis Modeling of Helicopter Cabin Noise C.A. Yoerkie, Sikorsky Aircraft Division, UTC & J.A. Moore, Cambridge Collaborative May 9, 1983 2012-06-03
Forum 39 Modelling the Effects of Blade Torsional Flexibility in Helicopter Stability and Control H.C. Curtiss Jr. & Z. Gao, Princeton University May 9, 1983 2012-06-03
Forum 39 A Practical Approach to Rotorcraft Systems Identification R.W. DuVal, Advanced Rotorcraft Technology, Inc. and J.E. Wang & M. Demiroz, San Jose State University May 9, 1983 2012-06-03
Forum 39 A Piloted Simulator Investigation of Side-Stick Controller/Stability and Control Augmentation System Requirements for Helicopter Visual Flight Tasks K.H. Landis & P.J. Dunford, Boeing Vertol Company and E.W. Aiken & K.B. Hilbert, U.S. Army Aeromechanics Laboratory May 9, 1983 2012-06-03
Forum 39 Design Considerations for Bearingless Rotor Hubs W.G. Bousman, R.A. Ormiston & P.H. Mirick, U.S. Army Research And Technology Laboratory May 9, 1983 2012-06-03
Forum 39 The Utility of Speed, Agility and maneuverability for an LHX Type Mission C.R. Vause, Sikorsky Aircraft Division, UTC, M. Harris, Flight Systems, Inc., M. Falco, Grumman Aerospace Corporation, D. Shaw, System Planning Corporation & R. McDaniel, Science & Technology Associates May 9, 1983 2012-06-03
Forum 39 Technology Advances in the AH-64 APACHE Advanced Attack Helicopter K.B. Amer & R.W. Prouty, Hughes Helicopters, Inc May 9, 1983 2012-06-03
Forum 39 Soviet vs. U.S. Helicopter Weight Prediction Methods W.Z. Stepniewski, International Technical Associates, Ltd. & R.A. Shinn, U.S. Army Aviation Research and Development Command May 9, 1983 2012-06-03
Forum 39 Development and Certification of the BK 117 Multi Purpose Helicopter V. Von Tein, Messerschmitt-Bolkow-Blohm Gmbh May 9, 1983 2012-06-03
Forum 39 On Developing and Flight Testing a Higher Harmonic Control System E.R. Wood & R.W. Powers, Hughes Helicopters, Inc. and C.E. Hammond & J.H. Cline, U.S. Army Aviation Research and Development Command May 9, 1983 2012-06-03
Forum 39 Helicopter Individual-Blade-Control And Its Applications N.D. Ham, Massachusetts Institute of Technology May 9, 1983 2012-06-03
Forum 39 The Importance of Nonlinearity on the Higher Harmonic Control of Helicopter Vibration J.A. Molusis, University of Connecticut May 9, 1983 2012-06-03
Forum 39 Predicting Structural Dynamic Behavior Using a Combined Experimental/Analytical Model M.R. Smith & F.S. Wei, Bell Helicopter Textron May 9, 1983 2012-06-03
Forum 39 Optimum Design of Rotor Blades for Vibration Reduction in Forward Flight P.P. Friedmann & P. Shanthakumaran, University of California at Los Angeles May 9, 1983 2012-06-03
Forum 39 Design of Helicopter Rotor Blades For Desired Placement of Natural Frequencies D.A. Peters & T. Ko, Washington University and A.E. Korn & M.P. Rossow, Southern Illinois University May 9, 1983 2012-06-03
Forum 39 A Study of the Aerodynamic Interaction Between a Main Rotor and a Fuselage C.A. Smith & M.D. Betzina, NASA-Ames Research Center May 9, 1983 2012-06-03
Forum 39 A Study of the Aerodynamic Interaction Between a Main Rotor and a Fuselage Authors: C.A. Smith & M.D. Betzina, NASA-Ames Research Center.
May 9, 1983 2012-06-03
Forum 39 Numerical Optimization Concepts and Definitions G. N. Vanderplaats, Naval Postgraduate School May 9, 1983 2012-06-03
Forum 39 Optimization in the Industrial Design Process J. A. Bennett, General Motors Research Laboratories May 9, 1983 2012-06-03
Forum 39 Fixed Wing Aircraft Applications of Optimization R. T. Haftka, Virginia Polytechnic Institute and State University May 9, 1983 2012-06-03
Forum 39 Structural Optimzation J. S. Arora, University of Iowa May 9, 1983 2012-06-03
Forum 39 Future of Optimzation J. Sobieski, NASA-Langley Research Center May 9, 1983 2012-06-03
Forum 39 An Investigation of the Aerodynamics of an RAE Swept Tip Using A Model Rotor P. G. Wilby, RAE and J. J. Philippe, ONERA May 9, 1983 2012-06-03
Forum 40 Application of a Turbulence Distortion Theory to Predict Helicopter Broadband Noise Due to Inflow Turbulence as a Function of Rotor Thrust M. Williams and W. Harris, Massachusetts Institute of Technology May 16, 1984 2012-06-03
Forum 40 Comparison of Noise Prediction for the X-Wing System and a Conventional Rotor in Hover R. Martin, NASA Langley Research Center May 16, 1984 2012-06-03
Forum 40 Acoustic Vibration Characteristics of High Contact Ratio Planetary Gears C. Yoerkie and A. Chory, Sikorsky Aircraft Division, United Technologies Corporation May 16, 1984 2012-06-03
Forum 40 Stability and Control of the Twin Lift Helicopter System H.C. Curtiss Jr., Princeton University and F.W. Warburton, Sikorsky Aircraft Division, United Technologies Corporation May 16, 1984 2012-06-03
Forum 40 A Piloted Simulator Investigation of Decoupling Helicopters by Using a Model Following Control System G. Bouwer, DFVLR and K.B. Hilbert, U.S. Army Research and Technology Laboratories (AVSCOM) May 16, 1984 2012-06-03
Forum 40 Assessment of Simulation Fidelity Using Measurements of Piloting Technique in Flight S.W. Ferguson, W.F. Clement, Systems Technology Inc., W.B.Cleveland, NASA Ames Research Center, and D.L. Key, U.S. Army Aeromechanics Laboratory (AVRADCOM) May 16, 1984 2012-06-03
Forum 40 Insights into Helicopter Air Combat Maneuverability N.D. Lappos, Sikorsky Aircraft Division, United Technologies Corporation May 16, 1984 2012-06-03
Forum 40 Environmental and Structural Assessment of Four Year In-Commercial Service Composite Helicopter Structures M.B. Ezzo and D.W. Lowry, Sikorsky Aircraft Division, United Technologies Corporation May 16, 1984 2012-06-03
Forum 40 A Balanced Approach to the Establishment of Structural Component Lives R.W. Arden, U.S. Army Aviation Systems Command May 16, 1984 2012-06-03
Forum 40 Designing for a Crashworthy All-Composite Helicopter Fuselage J.K. Sen, Hughes Helicopters, Inc May 16, 1984 2012-06-03
Forum 40 The Application of Geodetic Construction to Helicopter Airframes M.E. Lisle, Westland Helicopters Ltd May 16, 1984 2012-06-03
Forum 40 Delamination Control of Composite Rotor Hubs W.S. Chan, C. Rogers, J.D. Cronkhite and J. Martin, Bell Helicopter Textron May 16, 1984 2012-06-03
Forum 40 The Sikorsky Dynaflex Rotor - An Advanced Main Rotor System for the 1990s E.A. Fradenburgh and R.G. Carlson, Sikorsky Aircraft Division, United Technologies Corporation May 16, 1984 2012-06-03
Forum 40 Flight Test of the 4-Valve Fly-By-Wire/Fly-By-Optics Control System M.R. Murphy, Bell Helicopter Textron May 16, 1984 2012-06-03
Forum 40 Development of an On-Board Computer for Flight Test Data Analysis C.K. Hutchinson and A. Miller, Boeing Vertol Company May 16, 1984 2012-06-03
Forum 40 Development Flight Test of the Full Authority Digital Fuel Control in the HH-65A Helicopter S.L. Chisom, Aerospatiale Helicopter Corporation May 16, 1984 2012-06-03
Forum 40 Techniques for the Early Detection of Gear and Bearing Failures in Helicopter Drive Trains D. Gore and G. Edgar, RCA Corporation May 16, 1984 2012-06-03
Forum 40 Civil Certification of a U.S. Government Procured Helicopter J.C. Hart, Aerospatiale Helicopter Corporation May 16, 1984 2012-06-03
Forum 40 Blade Design Parameters Which Affect Helicopter Vibrations B.P. Gupta, Hughes Helicopters, Inc May 16, 1984 2012-06-03
Forum 40 Blade Design Parameters Which Affect Helicopter Vibrations B.P. Gupta, Hughes Helicopters, Inc May 16, 1984 2019-18-11
Forum 40 Impact of Emerging Technology on the Weight of Future Rotorcraft R.A. Shinn, U.S. Army Aviation Systems Command May 16, 1984 2012-06-03
Forum 40 Technology Impact on Helicopter, Tilt Rotor, and Tilt Fold Rotor Concepts C.G. Matthys and E.E. Scroggs Jr., Bell Helicopter Textron May 16, 1984 2012-06-03
Forum 40 Integrating New Technology into Weight Methodology R.H. Swan and A.H. Schmidt, Boeing Vertol Company May 16, 1984 2012-06-03
Forum 40 Advance Technology Impacts on Rotorcraft Weight E. Vega, Hughes Helicopters, Inc May 16, 1984 2012-06-03
Forum 40 An Assessment of the Impact of Technology on VTOL Weight Prediction D.K. Unsworth and J. Sutton, Sikorsky Aircraft Division, United Technologies Corporation May 16, 1984 2012-06-03
Forum 40 An Assessment of the Impact of Technology on VTOL Weight Prediction D.K. Unsworth and J. Sutton, Sikorsky Aircraft Division, United Technologies Corporation May 16, 1984 2017-26-09
Forum 40 Some Weight Aspects of Soviet Helicopters W.Z. Stepniewski, International Technical Associates, Ltd May 16, 1984 2012-06-03
Forum 40 Advanced Methodology for Quality Control of Composite Rotor Blades at Bell Helicopter Textron B. Rupe and B.J. Hunter, Bell Helicopter Textron May 16, 1984 2012-06-03
Forum 40 Impact of Criticality of Strategic Materials in Aerospace E.P. Laughlin, U.S. Army Aviation Systems Command May 16, 1984 2012-06-03
Forum 40 Evaluation of Automated Eddy Current System Reliability A. Thompson, General Electric Aircraft Engine Business Group May 16, 1984 2012-06-03
Forum 40 Automated Inspection and Precision Grinding of Spiral Bevel Gears A.J. Lemanski and H. Frint, Sikorsky Aircraft Division, United Technologies Corporation May 16, 1984 2012-06-03
Forum 40 AH-64A Production Line Automatic Test Equipment J.B. Davies, Hughes Helicopters, Inc. and D. Talley, Design Engineering Laboratories, Inc. May 16, 1984 2012-06-03
Forum 40 Army Aviation Maintenance Data and Supportability Interface T.A. Geoffroy and T.V. Stokes, U.S. Army Aviation Systems Command May 16, 1984 2012-06-03
Forum 40 New Model Introduction - The Operators' Perspective or Getting Straight "A's" in the School of Hard Knocks (A-vailable, A-ffordable, A-ccepted) D.A. Ford, Bell Helicopter Textron May 16, 1984 2012-06-03
Forum 40 JVX LCC Reduction Through Front-End Logistics J.J. Dougherty, Boeing Vertol Company, C.D. Elmore, Naval Air Systems Command, and A.W. Moffatt, Bell Helicopter Textron May 16, 1984 2012-06-03
Forum 40 Cost-Effective Airframe Depot Level Repair Through the Airframe Condition Evaluation (ACE) Program L. Neri, U.S. Army Aviation Systems Command, and H. Law, CACI, Inc. May 16, 1984 2012-06-03
Forum 40 The Development of Maintenance and Supply Support of Multi-Mission Helicopters Operating From Multiple Locations R.E. Walkup, Aerospatiale Helicopter Corporation May 16, 1984 2012-06-03
Forum 40 Impact of Main Rotor Tip Geometry on Main Rotor/Tail Rotor Interaction in Hover D.T. Balch, Sikorsky Aircraft Division, United Technologies Corporation May 16, 1984 2012-06-03
Forum 40 Generalized Wake Geometry for a Helicopter Rotor in Forward Flight and Effect of Wake Deformation on Airloads T.A. Egolf and A.J. Landgrebe, United Technologies Research Center May 16, 1984 2012-06-03
Forum 40 Evaluation of a 10-Foot Diameter X-Wing Rotor K.R. Reader, David Taylor Naval Ship Research and Development Center, and W.J. Dixon Jr., Boeing Vertol Company May 16, 1984 2012-06-03
Forum 40 The Prediction of Transonic Flows on Advancing Rotors C. Tung, F.X. Caradonna, D.A. Boxwell, Aeromechanics Laboratory, USARTL-AVSCOM, and W.R. Johnson, NASA Ames Research Center May 16, 1984 2012-06-03
Forum 40 Computerized Aerodynamic Design of a Transonically "Quiet" Blade M.E. Tauber, NASA Ames Research Center May 16, 1984 2012-06-03
Forum 40 Analytic and Experimental Verification of the NOTAR Circulation Control Tail Boom K.M. Morger, Hughes Helicopters, Inc. and D.R. Clark, Analytical Methods, Inc. May 16, 1984 2012-06-03
Forum 40 Development of a Generic Architecture C.E. Berggren, IBM Federal Systems Division May 16, 1984 2012-06-03
Forum 40 Fault Detection/Location System (FD/LS) How Much, How Little and How to Implement H.E. Pohlenz, T.D. DuHamel and G.C. Wiltsey, Hughes Helicopters, Inc. May 16, 1984 2012-06-03
Forum 40 NASA-FAA Helicopter Microwave Landing System Curved Path Flight Test H.N. Swenson, NASA Ames Research Center, J.R.Hamlin, U.S. Air Force, and G.W. Wilson, U.S. Army Research and Technology Laboratory, AVSCOM May 16, 1984 2012-06-03
Forum 40 On-Line Determination of Optimal Flight Paths for Helicopters G.L. Slater and M. Stoughton, University of Cincinnati May 16, 1984 2012-06-03
Forum 40 Design Considerations for Helicopter Effectiveness in Air-to-Air Combat D. DeLong, Sikorsky Aircraft Division, United Technologies Corporation and W.B. Herbst, Messerschmidt- Bolkow-Blohm GmbH May 16, 1984 2012-06-03
Forum 40 A Design Methodology for a Compliant Matrix Composite Bearingless Main Rotor C.J. Saddler and D.L. Hawkings, Westland Helicopters Ltd. May 16, 1984 2012-06-03
Forum 40 Are Two Always Better Than One? S.A. Hanvey and C.A. Parlier, Hughes Helicopters, Inc. May 16, 1984 2012-06-03
Forum 40 Advanced Technology Impact on LHX Helicopter Preliminary Design J.P. Rogers, R.A. Shinn and R.L. Smith, U.S. Army Aviation Systems Command May 16, 1984 2012-06-03
Forum 40 JVX Design Update S. Martin Jr. and W.B. Peck, Bell-Boeing Tilt Rotor Team May 16, 1984 2012-06-03
Forum 40 The AH-64 Back-Up Control System R.W. Prouty, Hughes Helicopters, Inc. May 16, 1984 2012-06-03
Forum 40 Toward a Unified Aerodynamic Model for Use in Rotor Blade Stability Analyses D.A. Peters, Washington University May 16, 1984 2012-06-03
Forum 40 Aeroelastic Stability Analysis of a Composite Blade C.-H. Hong and I. Chopra, University of Maryland May 16, 1984 2012-06-03
Forum 40 Aeromechanical Stability of a Full-Scale Hingeless Rotor in Hover R.L. Peterson and W. Warmbrodt, NASA Ames Research Center, and J. Hoover, Boeing Vertol Company May 16, 1984 2012-06-03
Forum 40 Pitch-Flap-Lag Instability of Elastic Modes of an Articulated Rotor Blade J.R. Neff, Hughes Helicopters, Inc. May 16, 1984 2012-06-03
Forum 40 Development and Evaluation of a Generic Active Helicopter Vibration Controller M.W. Davis, United Technologies Research Center May 16, 1984 2012-06-03
Forum 40 Contingency Power Concepts for Helicopter Turboshaft Engine R. Hirschkron, R.H. Davis, D.N. Goldstein and J.F. Haynes, General Electric Company, and J.W. Gauntner, NASA Lewis Research Center May 16, 1984 2012-06-03
Forum 40 Contingency Power Concepts for Helicopter Turboshaft Engine R. Hirschkron, R.H. Davis, D.N. Goldstein and J.F. Haynes, General Electric Company, and J.W. Gauntner, NASA Lewis Research Center May 16, 1984 2018-23-04
Forum 40 TF34 Convertible Engine Control System Design D.R. Gilmore Jr., General Electric Company May 16, 1984 2012-06-03
Forum 40 Designing Reliability into Derivative Engines J.A. Byrd, Allison Gas Turbine Operations May 16, 1984 2012-06-03
Forum 40 Definition of Requirements for 5000 Horsepower Class Demonstrator Engine E.T. Johnson, U.S. Army Research and Technology Laboratories (AVSCOM) May 16, 1984 2012-06-03
Forum 41 Higher Harmonic Control: Wind Tunnel Demonstration of Fully Effective Vibratory Hub Force Suppression J. Shaw, N. Albion, E.J. Hanker Jr., R.S. Teal, Boeing Vertol Co May 15, 1985 2012-05-03
Forum 41 Correlation of Stability Test Results and Analysis for the 1/5 Scale V-22 Aeroelastic Model D. Popelka, J. Bilger, Bell Helicopter Textron and M. Scheffler, Boeing Vertol Co May 15, 1985 2012-05-03
Forum 41 Helicopter Gust Alleviation, Attitude Stabilization, and Vibration Alleviation Using Individual-Blade-Control Through a Conventional Swash Plate N.D. Ham, Massachusetts Institute of Technology May 15, 1985 2012-05-03
Forum 41 Gust Response of Hingeless Rotors G.S. Bir and I. Chopra, University of Maryland May 15, 1985 2012-05-03
Forum 41 A Unified Formulation of Rotor Load Prediction Methods R.E. Hansford, Westland Helicopters Ltd May 15, 1985 2012-05-03
Forum 41 Effects of Analytical Modeling Assumptions on the Predicted Stability of a Model Hingeless Rotor R. Sopher and S.J. Cassarino, Sikorsky Aircraft Division, United Technologies Corp May 15, 1985 2012-05-03
Forum 41 Stored Terrain Data Base Aided Pilotage for Helicopters N.C. Seller and J.A. Gracia, Harris Government Aerospace Systems Division May 15, 1985 2012-05-03
Forum 41 Aircraft Lighting Systems J.F. Verney, Sikorsky Aircraft Division, United Technologies Corp May 15, 1985 2012-05-03
Forum 41 Development and Flight Test of a Helicopter, X-Band, Portable Precision Landing System Concept T.J. Davis, G.R. Clary, NASA Ames Research Center and J.P. Chisholm and S.L. Macdonald, Sierra Nevada Corp May 15, 1985 2012-05-03
Forum 41 FAA Certification Criteria for Lightning Protection of Helicopter Digital Engine Control R.L. Vaughn, Federal Aviation Administration May 15, 1985 2012-05-03
Forum 41 Precision IMC Approaches to Heliports Using Collocated MLS S. Shollenberg, J.H. Enias, Federal Aviation Administration Technical Center and P.S. Demko, U.S. Army Avionics Research and Development Activity May 15, 1985 2012-05-03
Forum 41 Establishment and Maintenance of Certification Standards for Helicopter and Turboprop Power Transmission Systems H.W. Ferris, Federal Aviation Administration May 15, 1985 2012-05-03
Forum 41 Gearbox Configuration Analysis H. Cocking, Westland Helicopters Ltd. May 15, 1985 2012-05-03
Forum 41 Application of CFD Design Technology in Development of the JVX Engine Inlet G.C. Paynter, J.L. Koncsek, Boeing Military Airplane Co., B. Turczeniuk, Boeing Vertol Co. and D.R. Clark, D.J. Strash, Analytical Methods Inc May 15, 1985 2012-05-03
Forum 41 The Health and Usage Monitoring of Helicopter Systems - The Next Generation J.D. Roe and D.G. Astridge, Westland Helicopters Ltd May 15, 1985 2012-05-03
Forum 41 The Application of LQR Synthesis Techniques to the Turboshaft Engine Control Problem W.H. Pfeil, G. de los Reyes, General Electric Co. and G.A. Bobula, U.S. Army Aviation Systems Command Research and Technology Laboratories May 15, 1985 2012-05-03
Forum 41 Adaptive Fuel Control Testing D.M. Achgill, Allison Gas Turbine Division, General Motors Corp. and R.D. Zagranski, Chandler Evans Control Systems Division, Colt Industries May 15, 1985 2012-05-03
Forum 41 Reconstruction of a Three-Dimensional, Transonic Rotor Flow Field from Holographic Interferogram Data Y.H. Yu, J.K. Kittleson, U.S. Army Aviation Systems Command Research and Technology Laboratories and F. Becker, Max-Plank-Institut fuer Stroemungsforschung May 15, 1985 2012-05-03
Forum 41 The Role of Scale Models in the Design of "Low BVI Noise" Rotorcraft K.R. Shenoy, Sikorsky Aircraft Division, United Technologies Corp May 15, 1985 2012-05-03
Forum 41 A Comparative Study of Tail Rotor Noise Mechanisms A.R. George and S.-T. Chou, Cornell University May 15, 1985 2012-05-03
Forum 41 FAA/HAI Helicopter Flight Operations Noise Tests and Initial Results S.A. Yoshikami, Federal Aviation Administration and C.R. Cox, Bell Helicopter Textron May 15, 1985 2012-05-03
Forum 41 Helicopter Cabin Noise: Actual vs. Statistical Energy Predictions C.A. Yoerkie and P.J. Gintoli, Sikorsky Aircraft Division, United Technologies Corp May 15, 1985 2012-05-03
Forum 41 Model Helicopter Blade Slap at Low Tip Speeds: Theoretical and Experimental Correlations D.C.-L. Chan, General Motors Corp. and J.E. Hubbard Jr., Massachusetts Institute of Technology May 15, 1985 2012-05-03
Forum 41 Directional Handling Qualities Requirements for NAP of the Earth (NOE) Tasks C.C. Bivens, U.S. Army Aviation Systems Command Research and Technology Laboratories May 15, 1985 2012-05-03
Forum 41 Directional Handling Qualities Requirements for NAP of the Earth (NOE) Tasks C.C. Bivens, U.S. Army Aviation Systems Command Research and Technology Laboratories May 15, 1985 2012-05-03
Forum 41 Assessment of Rotorcraft Agility and Maneuverability with a Pilot-in-the-Loop Simulation L.S. Levine, F.W. Warburton, Sikorsky Aircraft Division, United Technologies Corp. and H.C. Curtiss Jr., Princeton University May 15, 1985 2012-05-03
Forum 41 Assessment of Rotorcraft Agility and Maneuverability with a Pilot-in-the-Loop Simulation L.S. Levine, F.W. Warburton, Sikorsky Aircraft Division, United Technologies Corp. and H.C. Curtiss Jr., Princeton University May 15, 1985 2012-05-03
Forum 41 Flight Investigation of Bell Model 206 Ring Fin H.K. Harr, P.J. Hollifield, Bell Helicopter Textron and R.P. Smith, U.S. Army Aviation Systems Command Research and Technology Laboratories May 15, 1985 2012-05-03
Forum 41 Flight Investigation of Bell Model 206 Ring Fin H.K. Harr, P.J. Hollifield, Bell Helicopter Textron and R.P. Smith, U.S. Army Aviation Systems Command Research and Technology Laboratories May 15, 1985 2012-05-03
Forum 41 Helicopter Handling Requirements Based on Analysis of Flight Maneuvers R.K. Heffley and S.M. Bourne, Manudyne Systems Inc May 15, 1985 2012-05-03
Forum 41 Helicopter Handling Requirements Based on Analysis of Flight Maneuvers R.K. Heffley and S.M. Bourne, Manudyne Systems Inc May 15, 1985 2012-05-03
Forum 41 A Piloted Simulation of One-on-One Helicopter Air Combat at NOE Flight Levels M.S. Lewis, U.S. Army Aviation Systems Command Research and Technology Laboratories May 15, 1985 2012-05-03
Forum 41 A Piloted Simulation of One-on-One Helicopter Air Combat at NOE Flight Levels M.S. Lewis, U.S. Army Aviation Systems Command Research and Technology Laboratories May 15, 1985 2012-05-03
Forum 41 A Comparative Study of an Articulated Integrated Side-Arm Controller in a Variable Stability Helicopter J.M. Morgan, National Aeronautical Establishment May 15, 1985 2012-05-03
Forum 41 A Comparative Study of an Articulated Integrated Side-Arm Controller in a Variable Stability Helicopter J.M. Morgan, National Aeronautical Establishment May 15, 1985 2012-05-03
Forum 41 Application of Helicopter Air-to-Air Combat Test (AACT) Data to Current LHX Concerns F.J. Ebert and N.D. Lappos, Sikorsky Aircraft Division, United Technologies Corp May 15, 1985 2012-05-03
Forum 41 Free-Tip-Rotor Wind-Tunnel Test Results R.H. Stroub, L.A. Young, National Aeronautics and Space Administration and C. Keys, M. Cawthorne, Boeing Vertol Co May 15, 1985 2012-05-03
Forum 41 The Design of the EH101 for Safety and Performance R.I. Case and K.J. Andrews, Westland Helicopters Ltd May 15, 1985 2016-26-02
Forum 41 The Design of the EH101 for Safety and Performance R.I. Case and K.J. Andrews, Westland Helicopters Ltd May 15, 1985 2012-05-03
Forum 41 Design Aspects of the XV-15 Advanced Technology Blade Program K.E. Smith, H.R. Alexander, Boeing Vertol Co. and M.D. Maisel, Aeromechanics Laboratory, AVSCOM May 15, 1985 2012-05-03
Forum 41 X-Wing Potential for Navy Applications A.W. Linden, Sikorsky Aircraft Division, United Technologies Corp. and J.C. Biggers, David W. Taylor Naval Ship Research and Development Center May 15, 1985 2012-05-03
Forum 41 Influences of Two Landing Gear Designs on Helicopter Crashworthiness and Weights J.K. Sen, M.W. Votaw, Hughes Helicopters Inc. and G.R. Downer, Applied Technology Laboratory, AVSCOM May 15, 1985 2012-05-03
Forum 41 A New Approach to the Free Wake Problem for Hovering Rotors D.B. Bliss, D.A. Wachspress, Continuum Dynamics Inc. and Todd R. Quackenbush, Princeton University May 15, 1985 2012-05-03
Forum 41 Applied Aerodynamics of Circulation Control Airfoils and Rotors E.O. Rogers, A.W. Schwartz and J.S. Abramson, David W. Taylor Naval Ship Research and Development Center May 15, 1985 2012-05-03
Forum 41 Aerodynamic Performance of a 27-Percent-Scale AH-64 Wind-Tunnel Model with Baseline/Advanced Rotor Blades H.L. Kelley and J.C. Wilson, Army Structures Laboratory, AVSCOM May 15, 1985 2012-05-03
Forum 41 Full Scale Tilt Rotor Hover Performance F.E. Felker, M.D. Maisel and M.D. Betzina, NASA Ames Research Center May 15, 1985 2012-05-03
Forum 41 Hovering Rotor Airload Prediction Using a Full Potential Flow Analysis with Realistic Wake Geometry T.A. Egolf and S.P. Sparks, United Technologies Research Center May 15, 1985 2012-05-03
Forum 41 Calculation of Helicopter Airfoil Characteristics for High Tip-Speed Applications W.J. McCroskey, J.D. Baeder and J.O. Bridgeman, Aeromechanics Laboratory, AVSCOM May 15, 1985 2012-05-03
Forum 41 A Skin-Stringer Design for a Crashworthy Composite Fuselage for the Hughes 500E Helicopter J.K. Sen and M.W. Votaw, Hughes Helicopters Inc May 15, 1985 2012-05-03
Forum 41 Effects of Variations in Crashworthiness Criteria on Sikorsky S-75 ACAP Landing Gear Weights B.L. Lee and S.P. Garbo, Sikorsky Aircraft Division, United Technologies Corp May 15, 1985 2012-05-03
Forum 41 Preliminary Estimate of Fatigue Life for Dynamic Components of a New Helicopter K.B. Amer, D.H. Mancill and J.R. Neff, Hughes Helicopter Inc May 15, 1985 2012-05-03
Forum 41 Effect of Fiber and Matrix Maximum Strain on the Energy Absorption of Composite Materials G.L. Farley, Army Structures Laboratory, AVSCOM May 15, 1985 2012-05-03
Forum 41 Process Development and Test Evaluation of Cast, HIP and Heat Treated Titanium UH-60A M.R. Damper Bracket J. Kopchik, M.M. Schwartz and S. Silverstein, Sikorsky Aircraft Division, United Technologies Corp May 15, 1985 2012-05-03
Forum 41 Survey of Crashworthiness Achievements on Aerospatiale Helicopters J. Mens, Aerospatiale May 15, 1985 2012-05-03
Forum 41 Postbuckling and Crippling Behavior of Graphite/Epoxy Thin-Walled Airframe Members A.D. Reddy and L.W. Rehfield, Georgia Tech May 15, 1985 2012-05-03
Forum 41 Helicopter Customer Support - Are We Aware of How Great It Can Be J.J. Alexandrer, Aerospatiale Helicopter Corp May 15, 1985 2012-05-03
Forum 41 The Field Representative "Front Line Actioneer" W.G. Tripp, Sikorsky Aircraft Division, United Technologies Corp May 15, 1985 2012-05-03
Forum 41 Computer Simulation and Modeling - A Tool for Inventory Management J.G. Williams, Bell Helicopter Textron May 15, 1985 2012-05-03
Forum 41 Spare Parts Pricing: Impact on Logistics Support J.K. Hancock, Boeing Vertol Co May 15, 1985 2012-05-03
Forum 41 Combining Analysis and Test for Rotor Blade Development R. Jones and N. Giansante, Kaman Aerospace Corp May 15, 1985 2012-05-03
Forum 41 Development of a Composite Tail Rotor Blade for the MH-53E A.J. Lapati and A.E. Thompson, Sikorsky Aircraft Division, United Technologies Corp May 15, 1985 2012-05-03
Forum 41 An Avionics Software Test and Evaluation Technique T.B. Priest Jr. and B.P. Douglass, Bell Helicopter Textron May 15, 1985 2012-05-03
Forum 41 Assessment of Structural Damage in Composites Utilizing Acoustic Emission Technology W.C. Boyce, Sikorsky Aircraft and R.K. Miller, United Technologies Researche Center, Divisions of United Technologies Corp May 15, 1985 2012-05-03
Forum 41 Description and Initial Flight Experiments Boeing ARTI Test Bed C. Hutchinson, E. Baney-Barton and R. Gradle, Boeing Vertol Co May 15, 1985 2012-05-03
Forum 41 RSRA Flight Development Test in the Airplane Configuration R.E. Erickson, R.M. Kufeld, J.L. Cross and C.W. Acree, NASA Ames Research Center May 15, 1985 2012-05-03
Forum 41 Helicopter Rotor Icing Protection Methods H.J. Coffman Jr., Bell Helicopter Textron May 15, 1985 2012-05-03
Forum 41 VSTOL Aircraft Ice Protection Design Considerations Andrew Peterson, Boeing Vertol Company May 15, 1985 2012-05-03
Forum 41 Flight Tests of the Helicopter Pneumatic Deicing System L.A. Haworth and M.S. Graham, U.S. Army Aviation Engineering Flight Activity May 15, 1985 2012-05-03
Forum 41 The Aerodynamics of Rotor Blades with Ice Shapes Accreted in Hover and in Level Flight J.D. Lee, Ohio State University and R.J. Shaw, NASA Lewis Research Center May 15, 1985 2012-05-03
Forum 41 The Performance Characteristics of Simulated Ice on Rotorcraft Airfoils R.J. Flemming, Sikorsky Aircraft Division, United Technologies Corp., R.J. Shaw, NASA Lewis Research Center and J.D. Lee, Ohio State University May 15, 1985 2012-05-03
Forum 41 Robotics and Automated Measuring in Grinding Operations B.A. Manty, Pratt & Whitney Aircraft, T.R. Gosling, Kongsberg Bapenfabrikk and T.K. Lien, SINTEF/Norwegian Institute of Technology May 15, 1985 2012-05-03
Forum 41 Establishing Software QA - An Exercise in Frustration K.W. Froberg, Bell Helicopter Textron May 15, 1985 2012-05-03
Forum 41 Advanced Structural Casting Applications for a Gas Turbine Engine E.F. Bishop, J.N. Fleck and T.M. Regan, General Electric Co May 15, 1985 2012-05-03
Forum 41 Application of Closed-Loop Machining in the Manufacture of Gas Turbines S.M. Burgess and M.H. Wollowitz, General Electric Co May 15, 1985 2012-05-03
Forum 41 Robotics in Aircraft Manufacturing J.J. Barto Jr., Sikorsky Aircraft Division, United Technologies Corp May 15, 1985 2012-05-03
Forum 41 Tilt Rotor Crashworthiness J.D. Cronkhite, Bell Helicopter Textron and A.E. Tanner, Boeing Vertol Co May 15, 1985 2012-05-03
Forum 41 The Design and Development of New Crashworthy Seats for Navy Helicopters B.L. Carnell, Sikorsky Aircraft Division, United Technologies Corp May 15, 1985 2012-05-03
Forum 41 The Hughes Integrated Approach to Helicopter Crashworthiness - Past, Present and Future A.H. Logan and M.W. Votaw, Hughes Helicopters Inc May 15, 1985 2012-05-03
Forum 41 Army Helicopter Crashworthiness: Loading the Battlefield Dice in Our Favor K.F. Smith, Applied Technology Laboratory, AVSCOM May 15, 1985 2012-05-03
Forum 41 Crashworthy Design of Rotorcraft: A Basic Research Approach S. Hanagud, J.I. Craig, D. Schrage and P. Sriram, Georgia Tech May 15, 1985 2012-05-03
Forum 41 The Effect of HHC to a Four Bladed Hingeless Model Rotor G. Lehmann, German Aerospace Research and Test Establishment May 15, 1985 2012-05-03
Forum 41 Civil Helicopter Handling Qualities Requirements For Visual And Instruments Flight Dennis A. Tuck, P.E., Tuck Aircraft Engineering May 15, 1985 2018-10-10
Forum 41 An Assessment Of Current Helicopter Theory In Terms Of Early Developments Alfred Gessow, Professor and Chairman, Department of Aerospace Engineering, University of Maryland May 15, 1985 2018-10-10
Forum 42 Rotor-Fuselage Coupling by Impedance R. Gabel and V. Sankewitsch, Boeing Vertol Co June 2, 1986 2012-05-03
Forum 42 Rotor Load Correlation with the A.S.P. Blade R.E. Hansford, Westland Helicopters Ltd June 2, 1986 2012-05-03
Forum 42 Application of Design Optimization Techniques to Rotor Dynamics Problems M.W. Davis and W.H. Weller, United Technologies Research Center June 2, 1986 2012-05-03
Forum 42 AH-1G Flight Vibration Correlation Using Nastran and The C81 Rotor/Airframe Coupled Analysis R.V. Dompka and J.J. Corrigan, Bell Helicopter Textron, Inc June 2, 1986 2012-05-03
Forum 42 Use of Hierarchical Elastic Blade Equations and Automatic Trim for Helicopter Vibration Analysis S.N. Karunamoorthy, Parks College of St. Louis University and D.A. Peters, Georgia Institute of Technology June 2, 1986 2012-05-03
Forum 42 Calculated and Measured Blade Structural Response on a Full-Scale Rotor J. Esculier, STPA, Helicopters Department and W.G. Bousman, U.S. Army Aeroflightdynamics Directorate June 2, 1986 2012-05-03
Forum 42 Flight Demonstration of Higher Harmonic Control (HHC) on S-76 W. Miao, S.B.R. Kottapalli, H.M. Frye, Sikorsky Aircraft Division, United Technologies Corporation June 2, 1986 2019-07-10
Forum 42 Automated Tuning of Airframe Vibration by Structural Optimization H. Miura and M. Chargin, NASA Ames Research Center June 2, 1986 2012-05-03
Forum 42 Applications of Operational Analysis to the Preliminary Design Process M. Dinneen, Sikorsky Aircraft Division, UTC and P. Donnelly, Boeing Vertol Co June 2, 1986 2012-05-03
Forum 42 The Effects of Gun Accuracy and Rotorcraft Maneuverability on Air-to-Air Combat Effectiveness K.W. Harvey, Bell Helicopter Textron, Inc June 2, 1986 2012-05-03
Forum 42 Combat Support Requirements for Future Army Aircraft G.L. Daugherty, Martin Marietta Orlando Aerospace June 2, 1986 2012-05-03
Forum 42 Helicopter Launched Penguin Anti-Ship Missile H. Ekre, A/S Kongsberg Vapenfabrikk June 2, 1986 2012-05-03
Forum 42 Model for Analysis of Combat Sustainability T.N. Cook, Sikorsky Aircraft Division, UTC June 2, 1986 2012-05-03
Forum 42 Marine Corps Helicopter Air Combat Development: The First Ten Years P.J. Blemberg and M.B. Potter, U.S. Marine Corps June 2, 1986 2012-05-03
Forum 42 Composite Innovative Tooling R.L. Metcalf and G.P. Jones, McDonnell Douglas Helicopter Co June 2, 1986 2012-05-03
Forum 42 V-22 Tilt Rotor Transition Structure Fabrication and Assembly D.L. Petersen, Bell Helicopter Textron, Inc June 2, 1986 2012-05-03
Forum 42 Design of McDonnell Douglas Helicopter Company's New Composite Development Center K.L. Obrachta, McDonnell Douglas Helicopter Co June 2, 1986 2012-05-03
Forum 42 Machine Vision Inspection of Combustor Holes A.R. Hill Jr., Garrett Turbine Engine Co June 2, 1986 2012-05-03
Forum 42 Rotational Molding of High Temperature Thermoplastics R.A. Lofland, McDonnell Douglas Helicopter Co. and R. Gardiner, RMB Products June 2, 1986 2012-05-03
Forum 42 Cost Effectiveness Analysis Model of Army's Warranties S.A. Choo, U.S. Army Aviation Systems Command June 2, 1986 2012-05-03
Forum 42 Automated Composite Tape Laying D.W. Murrell, Bell Helicopter Textron, Inc June 2, 1986 2012-05-03
Forum 42 Wind Tunnel Test of a Pressure Instrumented Model Scale Advanced Rotor J.Cowan, L. Dadone and S. Gangwani, Boeing Vertol Co June 2, 1986 2012-05-03
Forum 42 Notar T.M. (No Tail Rotor) Hover Testing Using A Scale Model in Water J.R. Van Horn, McDonnell Douglas Helicopter Co June 2, 1986 2012-05-03
Forum 42 A Generalised Model for Airfoil Unsteady Aerodynamic Behaviour and Dynamic Stall Using the Indicial Method J.G. Leishman and T.S. Beddoes, Westland Helicopter Ltd June 2, 1986 2012-05-03
Forum 42 Ten Years of Rotor Flows Studies at Onera: State of the Art and Future Studies A. Desopper, P. Lafon, P. Ceroni and J.J. Philippe, ONERA June 2, 1986 2012-05-03
Forum 42 Rotor/Wing Aerodynamic Interactions in Hover F.F. Felker and J.S. Light, NASA Ames Research Center June 2, 1986 2012-05-03
Forum 42 Analysis of V-22 Tilt-Rotor Aircraft Using Panel Methods G.J. Carlin Jr., W.E. Staedeli and R.M. Hodges Jr., Boeing Vertol Co June 2, 1986 2012-05-03
Forum 42 Correlation of Acoustic Emission and Strain/Deflection Measurement During Composite Airframe Static Tests J.P. Perschbacker and W.C. Boyce, Sikorsky Aircraft Division UTC June 2, 1986 2012-05-03
Forum 42 Results of the V-22 Preliminary Design Wing Test Program C.A. Sprangers and M.K. Stevenson, Bell Helicopter Textron, Inc June 2, 1986 2012-05-03
Forum 42 Strengthening the Weak Link of Fatigue Qualification K.M. Rotenberger, U.S. Army Aviation Systems Command June 2, 1986 2012-05-03
Forum 42 Design and Structural Features of the SH-2F Composite Main Rotor Blade W.F. Alex and G.A. McCoubrey, Kaman Aerospace Corp June 2, 1986 2012-05-03
Forum 42 Design and Development of A Composite Rotor Head E. Schneider, R.C. Childs and F. McArdle, Boeing Vertol Co June 2, 1986 2012-05-03
Forum 42 Composite Applications in the Drive System H. Faust and J. Mack, Boeing Vertol Co June 2, 1986 2012-05-03
Forum 42 A Design-Support Team Views Forty Years of Commercial Helicopter Value G.M. Powell and F.J. Wagner, Bell Helicopter Textron, Inc June 2, 1986 2012-05-03
Forum 42 AH-64A Apache Helicopter Reliability, Availability, Maintainability/Logistics RAM/LOG Data System H.E. Pohlenz, McDonnell Douglas Helicopter Co June 2, 1986 2012-05-03
Forum 42 Embedded Training: The Enhancement and Sustainment of Mission Performance Capabilities D.L. Jones, Boeing Vertol Co June 2, 1986 2012-05-03
Forum 42 Summary of "The Human's Influence on Design Through Manprint" D.D. Strother and R. Carroll, Bell Helicopter Textron, Inc June 2, 1986 2012-05-03
Forum 42 Logistics/Engineering Community Cooperation: A Case Study C. Luchun and P.H. Renson, Avco Lycoming Textron and J.P. Demase and C.E. Langston Jr., Pratt & Whitney June 2, 1986 2012-05-03
Forum 42 Supportability and Aircraft Design M.A. Barnes, Boeing Vertol Co June 2, 1986 2012-05-03
Forum 42 The Computer in Electrical Load Analysis N. Caulfield, Kaman Aerospace Corp June 2, 1986 2012-05-03
Forum 42 Non-Iterative Parameter Identification Techniques P.M. Fitzsimons, V.R.P. Jonnalagadda, B.H. Tongue and D.P. Schrage, Georgia Institute of Technology June 2, 1986 2012-05-03
Forum 42 Integrated System Identification Methodology for Helicopter Flight Dynamics G.D. Padfield, U.K. Royal Aircraft Establishment June 2, 1986 2012-05-03
Forum 42 Structural Dynamic System Identification Techniques A. Berman, Kaman Aerospace Corp June 2, 1986 2012-05-03
Forum 42 System Identification Techniques for Helicopter Higher Harmonic Control S.A. Jacklin, NASA Ames Research Center June 2, 1986 2012-05-03
Forum 42 Basic Research in Structural Dynamic System Identification S. Hanagud, M. Meyyappa, J.I. Craig, Georgia Institute of Technology June 2, 1986 2012-05-03
Forum 42 Kinematic Observers for Rotor Vibration Control R.M. McKillip Jr., Princeton University June 2, 1986 2012-05-03
Forum 42 Application of the Cepstrum to Remove Echoes from Rotor Acoustic Spectra R.M. Martin, NASA Langley Research Center and C.L. Burley, PRC Kentron International June 2, 1986 2012-05-03
Forum 42 The Role of Wind Tunnel Models in Helicopter Noise Research H. Sternfeld Jr. and E.G. Schaeffer, Boeing Vertol Co June 2, 1986 2012-05-03
Forum 42 Application of Sound Intensity Technique in Helicopter Acoustics G.P. Mathur, M.C. Joshi and C.R. Cox, Bell Helicopter Textron, Inc June 2, 1986 2012-05-03
Forum 42 Progress in Tail Rotor Noise Analysis S. Chou and A.R. George, Cornell University June 2, 1986 2012-05-03
Forum 42 Acoustic Propagation Using Computational Fluid Dynamics J.D. Baeder and W.J. McCroskey, U.S. Army Aeroflightdynamics Directorate and G.R. Srinivasan, JAI Associates Inc June 2, 1986 2012-05-03
Forum 42 Folding Tilt Rotor Demonstrator Feasibility Study J.D. Eisenberg, NASA Lewis Research Center and J.V. Bowles, NASA Ames Research Center June 2, 1986 2012-05-03
Forum 42 AHIP: The OH-58D From Conception to Production (as published) F.D. Harris, Bell Helicopter Textron, Inc. Note: this was later expanded into a corrected, 2nd edition that spanned 112 pages. June 2, 1986 2017-31-01
Forum 42 AHIP: The OH-58D From Conception to Production (2nd edition, corrected, enlarged) F.D. Harris, Bell Helicopter Textron, Inc. 
Note: the original, 10 page paper as published is also available.
June 2, 1986 2012-05-03
Forum 42 The "Fenestron" A Shrouded Tail Rotor Concept for Helicopters R. Mouille and F. d'Ambra, Aerospatiale Helicopters Division June 2, 1986 2012-05-03
Forum 42 LHX - New Opportunity for Helicopter Design S.G. Cockerham June 2, 1986 2012-05-03
Forum 42 The Development of Dynamic Performance Standards for Civil Rotorcraft Seats J.H. Major and S.J. Soltis, Federal Aviation Administration June 2, 1986 2012-05-03
Forum 42 Pilot Use of Simulator Cues for Autorotation Landings W.A. Decker, C.F. Adam and R.M. Gerdes, NASA Ames Research Center June 2, 1986 2012-05-03
Forum 42 An Investigation of Single-Piloted Advanced Cockpit and Control Configurations for Nap-of-the-Earth Helicopter Combat Mission Tasks L.A. Haworth, C.C. Bivens and R.J. Shively, U.S. Army Aeroflightdynamics Directorate June 2, 1986 2012-05-03
Forum 42 V-22 Control Law Development K.W. Goldstein, Boeing Vertol Co. and L.W. Dooley, Bell Helicopter Textron, Inc. June 2, 1986 2012-05-03
Forum 42 Flight Evaluation of Height Response Characteristics for the Hover Bob-Up Task and Comparison with Proposed Criteria W.S. Hindson, Stanford University and G.E. Tucker, J.V. Lebacqz and K.B. Hilbert, NASA Ames Research Center June 2, 1986 2012-05-03
Forum 42 Advanced Flight Control Development for Single-Pilot Attack Helicopters R. Hendrick, G. Ramohalli and D. Yanke, Honeywell, Inc. and R. Fortenbaugh and T. Freeman, Bell Helicopter Textron, Inc June 2, 1986 2020-21-01
Forum 42 Advanced Flight Control Development for Single-Pilot Attack Helicopters R. Hendrick, G. Ramohalli and D. Yanke, Honeywell, Inc. and R. Fortenbaugh and T. Freeman, Bell Helicopter Textron, Inc June 2, 1986 2012-05-03
Forum 42 Handling Qualities Evaluation of the ADOCS Primary Flight Control System S.I. Glusman, K.H. Landis and C. Dabundo, Boeing Vertol Co June 2, 1986 2012-05-03
Forum 42 Flight Tests of an Open Loop Higher Harmonic Control System on an S-76A Helicopter D.M. Walsh, Sikorsky Aircraft Division, UTC June 2, 1986 2012-05-03
Forum 42 New Capabilities and Recent Research Programs of the NASA/Army CH-47B Variable-Stability Helicopter W.S. Hindson, Stanford University and K.B. Hilbert, G.E. Tucker, R.T.N. Chen and E.B. Fry, NASA Ames Research Center June 2, 1986 2012-05-03
Forum 42 Static Test and Flight Test of the Army/Bell ACAP Helicopter D. Reisdorfer, Bell Helicopter Textron, Inc. and L.T. Mazza, U.S. Army Aviation Applied Technology Directorate June 2, 1986 2012-05-03
Forum 42 Early Evaluation of the V-22 Osprey Through Piloted Simulation N.N. Batra and Dwayne F. Kimball, Bell Helicopter Textron, Inc. and T.A. Sheehan, Boeing Vertol Co June 2, 1986 2012-05-03
Forum 42 The Design and Test of a Human Powered Helicopter W.B. Patterson, California Polytechnic State University June 2, 1986 2012-05-03
Forum 42 Helicopter De-Icing System Development and Qualification Flight in Natural Icing Versus Simulation and Analysis K. Lunn, P.J. Dunford and G.E. Henschke, Boeing Vertol Co June 2, 1986 2012-05-03
Forum 42 Ice Protection Thermal Modelling Techniques A.A. Peterson, R.C. Johnson and A.D. Cipolloni, Boeing Vertol Co June 2, 1986 2012-05-03
Forum 42 A Numerical and Experimental Investigation of Electrothermal Aircraft Deicing K.L. Leffel, K.C. Masiulaniec, K.J. DeWitt and T.G. Keith Jr., University of Toledo June 2, 1986 2012-05-03
Forum 42 Application of Rotor Icing Analyses to the Design of a Rotorcraft Deicing System R.J. Flemming, Sikorsky Aircraft Division, UTC June 2, 1986 2012-05-03
Forum 42 Deicing the McDonnell Douglas AH-64A T.C. Knight and J.E. Ritter, McDonnell Douglas Helicopter Co June 2, 1986 2012-05-03
Forum 42 Sand Separator Efficiency Calculation for the JVX Tilt Rotor Aircraft Inlet J.J. Kim, M.D. Breer and D. Kneeling, Boeing Military Airplane Co. and J. Gass, Boeing Computer Services Co June 2, 1986 2012-05-03
Forum 42 A Review of Current Finite Difference Rotor Flow Methods F.X. Caradonna and C. Tung, U.S. Army Aeroflightdynamics Directorate June 2, 1986 2012-05-03
Forum 42 Euler Calculations for Rotor Configurations in Unsteady Forward Flight L.N. Sankar, Georgia Institute of Technology and C. Tung, U.S. Army Aeroflightdynamics Directorate June 2, 1986 2012-05-03
Forum 42 A Full Potential Rotor Analysis with Wake Influence Using an Inner-Outer Domain Technique T.A. Egolf and S.P. Sparks, United Technologies Research Center June 2, 1986 2012-05-03
Forum 42 Dynamic Stall of Oscillating Airfoils J.C. Wu, C.M. Wang, J. Wu and L.N. Sankar, Georgia Institute of Technology June 2, 1986 2012-05-03
Forum 42 Control and Display Requirements for Decelerating Approach and Landing of Fixed- and Rotary-Wing VSTOL Aircraft J.V. Lebacqz, V.K. Merrick and J.A. Franklin, NASA Ames Research Center June 2, 1986 2012-05-03
Forum 42 Critical Propulsion System Parameters for Future STOVL Combat Aircraft R.M. Denning and N.A. Mitchell, Rolls-Royce Ltd June 2, 1986 2012-05-03
Forum 42 The Marine's AV-8B: Why and How? M.D. Ryan, U.S. Marine Corps June 2, 1986 2012-05-03
Forum 42 STOVL in the European Operational Environment R.E. Johns, Royal Air Force June 2, 1986 2012-05-03
Forum 42 Supersonic STOVL Fighter Concepts Featuring the Hybrid Tandem-Fan Propulsion System P.A. Gelhausen and S.B. Wilson, III, NASA Ames Research Center June 2, 1986 2012-05-03
Forum 42 A Modular Flight Control and Navigation System for the Next Generation of Army Aviation C.T. Bye, J.T. Bakken and S.I. Snyder, Honeywell, Inc June 2, 1986 2012-05-03
Forum 42 System Sensory Perception (SSP) H.A. Becker, IBM Federal Systems Division June 2, 1986 2012-05-03
Forum 42 Shadow P.J. Emiro, Sikorsky Aircraft Division, UTC June 2, 1986 2012-05-03
Forum 42 HH-60 Avionics, A Progress Report C. Richardson, IBM and R. Lambdin, U.S. Air Force Rescue and Special Operations Directorate June 2, 1986 2012-05-03
Forum 42 Design Verification and Flight Testing of a Bearingless Soft Inplane Tail Rotor B. Enenkl and V. Kloppel, Messerschmitt-Bolkow-Blohm GmbH June 2, 1986 2012-05-03
Forum 43 The Aerodynamics of the Helicopter World Speed Record F.J. Perry, Westland Helicopters May 18, 1987 2012-05-03
Forum 43 Rotor Wake Modeling for High Speed Applications D.B. Bliss, Duke University, L. Dadone, Boeing Vertol Company, and D.A. Wachpress, Continuum Dynamics, Inc. May 18, 1987 2012-05-03
Forum 43 Circulation Control Airfoils in Unsteady Flow V. Raghavan, S.I. Pai and I. Chopra, University of Maryland May 18, 1987 2012-05-03
Forum 43 Airfoil Design, Test and Evaluation for the V-22 Tilt Rotor Vehicle J.C. Narramore, Bell Helicopter Textron May 18, 1987 2012-05-03
Forum 43 The Aerodynamics of an Oscillating Jet Flap P.F. Lorber and F.O. Carta, United Technologies Research Center, and R.G. Carlson, Sikorsky Aircraft May 18, 1987 2012-05-03
Forum 43 Marine Corps Helicopter Tactical Aircrew Training System (TACTS) Major P.J. Blemberg, USMC May 18, 1987 2012-05-03
Forum 43 Effect of Improved Maneuverability and Agility on AACT Air-to-Air Engagements S.D. Kershner and K.L. McVicar, Sikorsky Aircraft, and G.T. White, U.S. Army Aviation Applied Technology Directorate May 18, 1987 2012-05-03
Forum 43 Estimating Pilot Workload and Its Impact on System Performance F. Gozzo and R. Vienneau, IBM-Federal Systems Division May 18, 1987 2012-05-03
Forum 43 Helicopter Wiring System Battle Damage Repair J.A. Bleakney, Sikorsky Aircraft, M.-L. Lau, Applied Aviation Technology Directorate, and C. Brady, U.S. Army Aviation Logistics School May 18, 1987 2012-05-03
Forum 43 Tiltrotor Evolution Leads to Effectiveness Revolution R.F. Spivey, D.J. Barbour and D. Atkins, Bell Helicopter Textron, and LTC. J.H. Schaefer, USMC May 18, 1987 2012-05-03
Forum 43 Design of a Helicopter Remotely Piloted Vehicle K.J. Heigel Jr. and B.J. Scallan, Parks College of St. Louis University May 18, 1987 2012-05-03
Forum 43 The Effect of Simulated Helicopter Vibration on Voice Recognition System Performance T.W. Dennison, Sperry Corporation May 18, 1987 2012-05-03
Forum 43 The Effect of Simulated Helicopter Vibration on Voice Recognition System Performance T.W. Dennison, Sperry Corporation May 18, 1987 2015-28-10
Forum 43 A Pilot's Perspective of Automated Mission Management D.R. Bailey and N.J. Pekelsma, TAU Corporation May 18, 1987 2012-05-03
Forum 43 The EH101 Electronic Instrument System K.N. Atkin, Smiths Industries, and J. Revell, Westland Helicopters May 18, 1987 2012-05-03
Forum 43 Automatic Flight Control System for the Anglo-Italian EH101 Helicopter J. Meadows and G.R. Parr, Smiths Industries May 18, 1987 2012-05-03
Forum 43 Testing of the Advanced Digital Optical Flight Control System (ADOCS) L. Hartman, P.V. La Sala and J.S. Tulloch, Boeing Vertol Company May 18, 1987 2012-05-03
Forum 43 Design, Development and Flight Evaluation of Advanced Digital Flight Control System B.P. Gupta, B. Barnes, R. Hodge, C. Morse and G. Dockter, McDonnell Douglas Helicopter Company May 18, 1987 2012-05-03
Forum 43 AH-64 Shake Test and Correlation with NASTRAN Finite Element Model Predictions M. Toossi, D. Ferg, R. Weisenberger and F. Straub, McDonnell Douglas Helicopter Company May 18, 1987 2012-05-03
Forum 43 AH-64 Shake Test and Correlation with NASTRAN Finite Element Model Predictions M. Toossi, D. Ferg, R. Weisenberger and F. Straub, McDonnell Douglas Helicopter Company May 18, 1987 2018-29-08
Forum 43 Statistical Analysis of Structural Flight Test Data D.O. Adams, Sikorsky Aircraft May 18, 1987 2012-05-03
Forum 43 Approach Vibration Control of the RSRA/X-wing Vehicle Using A Time Domain Approach R.W. DuVal and H.A. Saberi, Advanced Rotorcraft Technology, Inc. May 18, 1987 2012-05-03
Forum 43 Simulation and Correlation of a Helicopter AIR-OIL Strut Dynamic Response W.A. Welsh, Sikorsky Aircraft May 18, 1987 2012-05-03
Forum 43 Application of a Comprehensive Analytical Model of Rotorcraft Aerodynamics and Dynamics (CAMRAD) to the MDHC AH-64 Helicopter C.B. Callahan and D.E. Bassett, McDonnell Douglas Helicopter Company May 18, 1987 2012-05-03
Forum 43 Aeroelastic Modeling of Swept Tip Rotor Blades Using Finite Elements R. Celi and P. Friedmann, UCLA May 18, 1987 2012-05-03
Forum 43 Aeroelastic Modeling of Swept Tip Rotor Blades Using Finite Elements R. Celi and P. Friedmann, UCLA May 18, 1987 2021-27-09
Forum 43 Correlation of Analytical Calculations from GRASP with Torsionally-Soft Rotor Data D.L. Kunz, U.S. Army Aeroflightdynamics Directorate, and D.H. Hodges, Georgia Institute of Technology May 18, 1987 2012-05-03
Forum 43 V-22 Development Status S. Martin Jr., Bell Helicopter Textron, A.H. Schoen, Boeing Vertol Company, And CDR. R. Vehorn, V-22 Asst. Program Manager for Systems Engineering May 18, 1987 2012-05-03
Forum 43 Rotor Aerodynamic Optimization for High Speed Tiltrotors D.J. Paisley, Boeing Vertol Company May 18, 1987 2012-05-03
Forum 43 Vertical Lift Aircraft Air to Air Combat, The Attributes for Success C.L. Peterson and S.J. Sutter, Multinational Technology May 18, 1987 2012-05-03
Forum 43 Reduction of Hub and Pylon Fairing Drag L.A. Young, D.R. Graham, and R. Stroub, NASA-Ames Research Center, and A. Louie, Sterling Software, Inc. May 18, 1987 2012-05-03
Forum 43 Rotor Performance Optimization for a Future Light Helicopter S. Kumar and D. Bassett, McDonnell Douglas Helicopter Company May 18, 1987 2012-05-03
Forum 43 Finite Element Stress Analysis of Helicopter Planetary Gears R.J. Drago and R.N. Margasahayam, Boeing Vertol Company May 18, 1987 2012-05-03
Forum 43 Substantiation of Damage Tolerant Designs in Civil Helicopters R.T. Weaver, Federal Aviation Administration May 18, 1987 2012-05-03
Forum 43 Investigation of Fatigue Methodology C.T. Gunsallus, W.G. Flannelly, P.G. Stennett and E.J. Nagy, Kaman Aerospace Corporation May 18, 1987 2012-05-03
Forum 43 Development of a Totally Computerized Interactive Fatigue Life Analysis Program M.D. Jones, A.P. Stewart, and B. Altman, McDonnell Douglas Helicopter Company May 18, 1987 2012-05-03
Forum 43 Prediction of Helicopter Rotor Impulsive Noise Using Measured Blade Pressures K.J. Schultz and W.R. Splettstoesser, DFVLR Braunschweig May 18, 1987 2012-05-03
Forum 43 Rotor Noise Prediction and Validation D.S. Janakiram and H. Tadghighi, McDonnell Douglas Helicopter Company May 18, 1987 2012-05-03
Forum 43 Acoustic Characteristics of Tail Rotors and the Effect of Empennage Interactions E.W. Jacobs, J.M. Fitzgerald and R.K. Shenoy, Sikorsky Aircraft May 18, 1987 2012-05-03
Forum 43 Predictions and Measurement of Blade-Vortex Interaction Noise M.C. Joshi, Bell Helicopter Textron and D.A. Boxwell, Army Aeroflightdynamics Directorate May 18, 1987 2012-05-03
Forum 43 Treated Cabin Acoustic Predictions Using Statistical Energy Analysis C.A. Yoerkie Jr., S.T. Ingraham, Sikorsky Aircraft and J.A. Moore, Cambridge Collaborative, Inc. May 18, 1987 2012-05-03
Forum 43 Calculations of Quadropolar Transonic Rotor Noise Using a Formulation in the Frequency Domain J. Prieur, ONERA May 18, 1987 2012-05-03
Forum 43 Model 360 Rotor Test at DNW - Review of Performance and Blade Airload Data Leo Dadone, Boeing Vertol Company; Seth Dawson, Donald Boxwell, Ames Research Center; Don Ekquist, Boeing Vertol Company
May 18, 1987 2013-23-01
Forum 44 Effect Of An Anhedral Swept Back Tip On The Performance Of A Helicopter Rotor A. Desopper, Aerospatiale Corp. June 16, 1988 2012-05-03
Forum 44 Free Wake Calculation of Rotor Flow Fields for Interactional Aerodynamics T .R. Quackenbush, Continuum Dynamics, Inc., and D.B. Bliss, Duke University June 16, 1988 2012-05-03
Forum 44 Rotor/Airframe Interactions on Tiltrotor Aircraft M.A. McVeigh, W.K. Grauer and D.J. Paisley, Boeing Helicopters June 16, 1988 2012-05-03
Forum 44 Rotor Inflow Variability with Advance Ratio D. R. Hoad, S.L. Althoff, and J .W. Elliot, NASA Langley Research Center June 16, 1988 2012-05-03
Forum 44 A Correlation Study of Rotor Inflow In Forward Flight B.D. Charles and Dr. A.A. Hassan, McDonnell Douglas Helicopter Co. June 16, 1988 2012-05-03
Forum 44 An Entropy and Viscosity Corrected Potential Method for Rotor Performance Prediction J . 0 . Bridgeman, Woodside Summit Group, R.C. Strawn and F.X. Caradonna, U.S. Army Aerof1ightdynamics Directorate June 16, 1988 2012-05-03
Forum 44 An Examination Of Some Rotor Aerodynamic Models Using The RSRA/X-Wing Model Test Data S.J. Davis, J.P. Shanley and P. Buettiker, Sikorsky Aircraft Division, UTC June 16, 1988 2012-05-03
Forum 44 Air Combat Tactics for the Evaluation of Rotorcraft Characteristics in the Low Air War of 2010 J.V. Mackmull, Defense Consultant and D.L. Green, STARMARK Corp. June 16, 1988 2012-05-03
Forum 44 U.S. Army Aircraft Combat Maintenance/Battle Damage Repair (ACM/BDR) Program M-L. Lau, U.S. Army Aviation Applied Technology Directorate June 16, 1988 2012-05-03
Forum 44 Orchidee: Planning The Development of a Battlefield Surveillance System J.L. Mascle, Aerospatiale Helicopter Division June 16, 1988 2012-05-03
Forum 44 Tiltrotor Evolution Leads to ASW Revolution J. Latchford, M. Jagielski and R. Spivey, Bell Helicopter Textron, and CMDR R. P. Krulis, U.S. Navy June 16, 1988 2012-05-03
Forum 44 Airframe and Propulsion Assessment of Light Helicopter Technologies (LHX) K.A. Stanzione and R.F. Smith, Praxis Technologies Corp. June 16, 1988 2012-05-03
Forum 44 Software Development for Large Scale Avionics Integration Programs R. P. Hampp and C.W. Richardson, IBM June 16, 1988 2012-05-03
Forum 44 Human Factors Impact on the V-22 Osprey Cockpit Development: An Overview Dr. V.A. Graf and C D . Holley, Bell Helicopter Textron June 16, 1988 2012-05-03
Forum 44 Rotorcraft Pilot's Associate (RPA) J.W. Wasson and D.G. Telles, McDonnell Douglas Helicopter Co. June 16, 1988 2012-05-03
Forum 44 Dynamic Perspective Displays and the Control of Tilt-Rotor Aircraft In Simulated Flight LTC C.T. Bennett and W.W. Johnson, NASA Ames Research Center and K.A. O'Donnell, U.S. Army Aeroflightdynamics Directorate June 16, 1988 2012-05-03
Forum 44 Airborne Integrated Monitoring System A.H. Neubauer Jr., Teledyne Controls June 16, 1988 2012-05-03
Forum 44 AH-64A Contractor Logistics Support: The Contractors' Perspective J. Reagan and J. Wood, McDonnell Douglas Helicopter Co. June 16, 1988 2012-05-03
Forum 44 Corrosion and Corrosion Control of Selected Field Problems H. Jacobs and M. Lloyd, McDonnell Douglas Helicopter Co. June 16, 1988 2012-05-03
Forum 44 Capitalizing on Today's Technology by Using Computer Based Training/Interactive Video Disc to Enable Effective and Efficient Training to Be Conducted and Managed in the Work Place T.C. Helmacy, Sikorsky Aircraft Division, UTC June 16, 1988 2012-05-03
Forum 44 Improved Life Cycle 'REPS' and Services: V-22 Engineering Technical Services and Logistics Planning C D . Elmore, Naval Air Systems Command June 16, 1988 2012-05-03
Forum 44 Experimental Verification of Helicopter Blade Designs Optimized For Minimum Vibration W.H. Weller and M.W. Davis, United Technologies Research Center June 16, 1988 2012-05-03
Forum 44 Developments in Dynamics Methodology at Bell Helicopter Textron J.J. Corrigan, J.J. Schillings, S.K. Yin, and P.Y. Hsieh, Bell Helicopter Textron June 16, 1988 2012-05-03
Forum 44 Bearingless Rotors and Higher Harmonic Control Modeling Using RACAP K.B. Sangha, McDonnell Douglas Helicopter Co. June 16, 1988 2012-05-03
Forum 44 Design of A Simple Active Controller To Suppress Helicopter Air Resonance M. Takahashi and Prof. P.P. Friedmann, UCLA June 16, 1988 2012-05-03
Forum 44 Structural Dynamics of a Helicopter Rotor Blade System Dr. A.V. Srinivasan, D.G. Cutts, and H.T. Shu, United Technologies Research Center, and D. L. Sharpe, U.S. Army Aerof1ightdynamics Directorate June 16, 1988 2012-05-03
Forum 44 Investigation of Difficult Component Effects on Finite Element Model Vibration Prediction for Helicopters R.V. Dompka, Bell Helicopter Textron June 16, 1988 2012-05-03
Forum 44 Design and Fabrication of an Advanced Light Rotor H.W. Friedman, Bell Helicopter Textron June 16, 1988 2012-05-03
Forum 44 The Pointer - A Revolutionary Idea To Improve RPV Capabilities R.S. Taylor, Bell Helicopter Textron June 16, 1988 2012-05-03
Forum 44 Civil Tiltrotor Aircraft: A Comparison of Five Candidate Designs J.B. Wilkerson, Boeing Helicopters and R.S. Taylor, Bell Helicopter Textron June 16, 1988 2012-05-03
Forum 44 Development of the V-22 Osprey Crewseat Assembly H.A. Lindsay and J.W. Coltman, Simula, Inc., and C.V. Ednie, Boeing Helicopters June 16, 1988 2012-05-03
Forum 44 Optimal Design of an Advanced Composite Rotating Flexbeam B.K. Hamilton, J.R. Peters and C. Callahan, McDonnell Douglas Helicopter Co. June 16, 1988 2012-05-03
Forum 44 Design, Analysis and Test of Composite Material Fuel Tank Pods for the CH-46E Helicopter J.P. Kelleher and S. Moszer, Boeing Helicopters June 16, 1988 2012-05-03
Forum 44 Aluminum Lithium Alloys - Processing and Properties P.C. Inguanti, Sikorsky Aircraft Division, UTC June 16, 1988 2012-05-03
Forum 44 The Effect of Structural Tailoring by Edge Alteration on Free-Edge Delamination A. Vizzini and W. Pogue, University of Maryland June 16, 1988 2012-05-03
Forum 44 Advancements in Erosion Testing of Rotor Blade Leading Edges D.A. Haynie, Bell Helicopter Textron June 16, 1988 2012-05-03
Forum 44 Material Characterization Problems Leading to Inaccurate Composite Design Allowables A.K. Munjal, Kaman Aerospace Corp. June 16, 1988 2012-05-03
Forum 44 Six Degree of Freedom Crew Isolation Design, Bench Test, and Flight Test R. Gabel , R.A. Desjardins, and V. Sankewitsch, Boeing Helicopters June 16, 1988 2012-05-03
Forum 44 Dynamic Modeling of a Helicopter Lubrication System W.A. Welsh, Sikorsky Aircraft Division, UTC June 16, 1988 2012-05-03
Forum 44 Aeroelastic Optimization of a Helicopter Rotor J.W. Lim and I. Chopra, University of Maryland June 16, 1988 2012-05-03
Forum 44 Dynamic Characteristics of Advanced Bearingless Rotors at McDonnell Douglas Helicopter Company J.L. Sorensen and L.J. Silverthorn, McDonnell Douglas Helicopter Co., and T.H. Maier, U.S. Army Aerof1ightdynamics Directorate June 16, 1988 2012-05-03
Forum 44 Testing and Correlation on an Advanced Technology Bearingless Rotor K.S. Perry and J.A. White, Bell Helicopter Textron June 16, 1988 2012-05-03
Forum 44 Tip Loss and Blade Strike Simulations Using DYSCO B.A. Gustavson, Kaman Aerospace Corp. June 16, 1988 2012-05-03
Forum 44 A Piloted Simulation Investigation of Yaw Dynamics Requirements for Turreted Gun Use in Low-Level Helicopter Air-to-Air Combat W.A. Decker, NASA Ames Research Center, P.M. Morris, Sikorsky Aircraft Division, UTC, and J.N. Williams, USA June 16, 1988 2012-05-03
Forum 44 The Impact of Yaw Axis Control Modes, Flight Directors and Automatic Control Coupling on Decelerating IFR Approaches for Rotorcraft S.W. Baillie and S. Kereliuk, National Research Council of Canada, and R. H. Hoh, Systems Technology, Inc. June 16, 1988 2012-05-03
Forum 44 Determination of Control Laws for a Single Pilot, Attack Helicopter P.J. Hollifield and A.M. Oetting, Bell Helicopter Textron June 16, 1988 2012-05-03
Forum 44 A Comparison between Various Side-Arm Controller Configurations in a Fly-by-Wire Helicopter J.M. Morgan, National Research Council of Canada June 16, 1988 2012-05-03
Forum 44 Advanced Transmission Studies Dr. J.J. Coy, NASA Lewis Research Center and Dr. R.C. Bill, U.S. Army Propulsion Directorate June 16, 1988 2012-05-03
Forum 44 Advanced Lube System Diagnostics for V-22 H.M. Belman and F. DiPasquale, TEDECO Division, Aeroquip Corp. June 16, 1988 2021-30-03
Forum 44 Advanced Lube System Diagnostics for V-22 H.M. Belman and F. DiPasquale, TEDECO Division, Aeroquip Corp. June 16, 1988 2012-05-03
Forum 44 Dual Centrifugal Compressors: The Helicopter Solution to Sand and Ice Ingestion J.D. Pugnale, Garrett Engine Division, Allied-Signal Aerospace Co. June 16, 1988 2012-05-03
Forum 44 Analytical Determination & Experimental Comparison of Performance Degredation on a Helicopter Main Rotor Due to Ice Accretion R.C. Johnson and A.A. Peterson, Boeing Helicopters and K.D. Korkan and R.K. Britton, Texas A&M University June 16, 1988 2012-05-03
Forum 44 Dolphin Eats Snow J.A. Murphy, Aerospatiale Helicopter Corp. June 16, 1988 2012-05-03
Forum 44 Helicopter Air Intake: Protection For Flight In Snow and Icing Conditions X. De La Servette and P. Cabrit, Aerospatiale Corp. June 16, 1988 2012-05-03
Forum 44 Analytical Prediction and Flight Test Evaluation of Bell ACAP Helicopter Cabin Noise Dr. G.P. Mathur, Bell Helicopter Textron and Dr. J.E. Manning and L.R. Quartararo, Cambridge Collaborative, Inc. June 16, 1988 2012-05-03
Forum 44 Experimental Assessment of a Turbulence Ingestion Noise Theory Dr. J.C. Simonich and Dr. R.H. Schlinker, United Technologies Research Center, and Dr. R.K. Amiet, Consultant June 16, 1988 2012-05-03
Forum 44 Experimental Assessment of a Turbulence Ingestion Noise Theory Dr. J.C. Simonich and Dr. R.H. Schlinker, United Technologies Research Center, and Dr. R.K. Amiet, Consultant June 16, 1988 2015-05-08
Forum 44 A Comparison of Acoustic Predictions With Model Rotor Test Data From The NASA 14' x 22' Wind Tunnel C.J. Schwindt and J.M. Fitzgerald, Sikorsky Aircraft Division, UTC June 16, 1988 2012-05-03
Forum 44 Tip-path-plane Angle Effects On Rotor Blade-Vortex Interaction Noise Levels and Directivity C.L. Burley, Planning Research Corp. and R.M. Martin, NASA Langley Research Center June 16, 1988 2012-05-03
Forum 44 Mechanisms of Active Control in Cylindrical Fuselage Structures (AIAA Guest Paper) R . J . Silcox and Dr. H.C. Lester, NASA Langley Research Center, and Dr. C.R. Fuller, Virginia Polytechnic University June 16, 1988 2012-05-03
Forum 44 Improvements To Transonic Flowfield Calculations D . Prichard and L.N. Sankar, Georgia Institute of Technology June 16, 1988 2012-05-03
Forum 44 An Evaluation of a Navier-Stokes Code For Calculations of Retreating Blade Stall on a Helicopter Rotor J.C. Narramore, Bell Helicopter Textron, L.N. Sankar, Georgia Institute of Technology, and R.E. Vermeland, CRAY Research, Inc. June 16, 1988 2012-05-03
Forum 44 A Unified Theoretical-Computational Approach For Viscous Unsteady Rotor Aerodynamics Dr. J.C. Wu and I.H. Tuncer, Georgia Institute of Technology June 16, 1988 2012-05-03
Forum 44 Helicopter Free Wake Prediction of Complex Wake Structures Under Blade-Vortex Interaction Operating Conditions T.A. Egolf, United Technologies Research Center June 16, 1988 2012-05-03
Forum 44 Rotorcraft Aeromechanical Analysis Using A Nonlinear Unsteady Aerodynamic Model Dr. A.S. Elliot, McDonnell Douglas Helicopter Co., Dr. J.G. Leishman and Dr. I. Chopra, University of Maryland June 16, 1988 2012-05-03
Forum 44 Bell ACAP Full-Scale Aircraft Crash Test and KRASH Correlation J.D. Cronkhite, Bell Helicopter Textron and L.T. Mazza, U.S. Army Aviation Applied Technology Directorate June 16, 1988 2012-05-03
Forum 44 Application of Damage Tolerance Methodology to Helicopter Dynamic Components Using the Example of a Main Rotor Pitch Link for the AH-1S Helicopter B.R. Krasnowski and W.W. Spence, Bell Helicopter Textron, and K.M. Rotenberger, U.S. Army Aviation Systems Command June 16, 1988 2012-05-03
Forum 44 Holometrics: An Information Transformation Methodology C.T. Gunsallus, W.G. Flannelly, and W.L. Pellum, Kaman Aerospace Corp. June 16, 1988 2012-05-03
Forum 44 Evolution of the ACAP Crash Energy Management System C.W. Clarke, Sikorsky Aircraft Division, UTC June 16, 1988 2012-05-03
Forum 44 Methodology For Fatigue Substantiation of Alternate Sources and Degraded Modes on Helicopter Dynamic Components D. Adams, Sikorsky Aircraft Division, UTC, and C. Albrecht, Boeing Helicopters, and W . D . Harris, McDonnell Douglas Helicopter Co. June 16, 1988 2012-05-03
Forum 44 Environmentally Induced Cracking In Aluminum L.R. Rodriguez, Kaman Aerospace Corp. June 16, 1988 2012-05-03
Forum 44 Matrix Analysis Method for Composite Flexbeam Dr. S. Datta and R. Filler, McDonnell Douglas Helicopter Co. June 16, 1988 2012-05-03
Forum 44 Damage Tolerance Improvement Approaches for Composite Components A. Munjal, Kaman Aerospace Corp. June 16, 1988 2012-05-03
Forum 44 Development and Qualification Testing, Teaming for the V-22 Multi-Service Aircraft System K. Lunn and P. Dunford, Boeing Helicopters, R. Magnuson, Bell Helicopter Textron, and S. Porter, Naval Air Test Center June 16, 1988 2012-05-03
Forum 44 Air-To-Air Combat Helicopter Development J.M. McCollough, C. Stroncek, and H. Ward, Bell Helicopter Textron June 16, 1988 2012-05-03
Forum 44 AH-64A Apache, Development of Capabilities for the Aerial Combat Role J.A. Buresh, C.A. Parlier, and W . E . Wilson, McDonnell Douglas Helicopter Co. June 16, 1988 2012-05-03
Forum 45 Design, Evaluation and Proof-of-Concept Flights of a Main Rotor Interblade Viscoelastic Damping System B. Guimbal, Aerospatiale, Helicopter Division May 22, 1989 2016-30-08
Forum 45 Design, Evaluation and Proof-of-Concept Flights of a Main Rotor Interblade Viscoelastic Damping System B. Guimbal, Aerospatiale, Helicopter Division May 22, 1989 2012-04-03
Forum 45 Helicopter Ground/Air Resonance Including Rotor Shaft Flexibility and Control Coupling R.G. Loewy and M. Zotto, Rensselaer Polytechnic Institute May 22, 1989 2012-04-03
Forum 45 Examination of Dynamic Characteristics of UH-60A and EH-60A Airframe Structures J.A. Durno and R.K. Goodman, Sikorsky Aircraft Division, UTC May 22, 1989 2012-04-03
Forum 45 A Review of the V-22 Dynamics Validation Program J.E. Brunken Jr., D.A. Popelka, and R.J. Bryson, Bell Helicopter Textron May 22, 1989 2012-04-03
Forum 45 Higher Harmonic and Trim Control of the X-Wing Circulation Control Wind Tunnel Model Rotor W.A. Welsh and R.H. Blackwell Jr., Sikorsky Aircraft Division, UTC May 22, 1989 2012-04-03
Forum 45 Application of Higher Harmonic Control (HHC) to Rotors Operating at High Speed and Maneuvering Flight K.Q. Nguyen and I. Chopra, University of Maryland May 22, 1989 2012-04-03
Forum 45 High Resolution Flow Field Prediction For Tail Rotor Aeroacoustics T.R. Quackenbush, Continuum Dynamics, Inc. and D.B. Bliss, and A. Mahajan, Duke University May 22, 1989 2012-04-03
Forum 45 Prediction and Measurement of Low Frequency Hovering Harmonic Noise of a Modern Helicopter Rotor F.H. Schmitz, NASA Ames Research Center, H.R. Aggarwal, Helicopter Aerodynamics & Noise, and D.A. Boxwell, U.S. Army Aeroflightdynamics Dir. May 22, 1989 2012-04-03
Forum 45 Aeroacoustic Flowfield and Acoustics of a Model Helicopter Tail Rotor at High Advance Ratio R.K. Shenoy, Sikorsky Aircraft Division, UTC May 22, 1989 2012-04-03
Forum 45 A Finite Element Method to Predict Internal Noise Levels at Discrete Frequencies for a Partially Composite Helicopter Fuselage F. Chabas, J.M. David, A. Desanti, N. Meidinger, and C. Soize, ONERA, and M. Dussac, P. Martin and H.J. Marze, Aerospatiale May 22, 1989 2012-04-03
Forum 45 The Prediction of the Noise Generating Mechanisms of an Aerospatiale 365N-1 Dauphin Helicopter D.S. Weir, Planning Research Corp. and R.A. Golub, NASA Langley Research Center May 22, 1989 2012-04-03
Forum 45 Digital X-ray Inspection F.H. Little, General Electric Co. May 22, 1989 2012-04-03
Forum 45 MDHC Factory of the Future Project T. Poindexter, McDonnell Douglas Helicopter Co. May 22, 1989 2012-04-03
Forum 45 Rotor Smoothing Expert System P. Benson, McDonnell Douglas Helicopter Co. May 22, 1989 2012-04-03
Forum 45 Carbon/Epoxy Tooling Evaluation and Usage M.D. Cimbalista Jr., McDonnell Douglas Helicopter Co. May 22, 1989 2012-04-03
Forum 45 The Effects of Aerial Combat on Helicopter Structural Integrity C.G. Schaefer Jr., Naval Air Systems Command May 22, 1989 2012-04-03
Forum 45 HARP Model Rotor at DNW S. Dawson, U.S. Army Aeroflightdynamics Dir., D. Jordan and C. Smith, NASA Ames Research Center, and J. Ekins, L. Silverthorn and B. Tuttle, McDonnell Douglas Helicopter Co. May 22, 1989 2012-04-03
Forum 45 Adaptive Electronic Fuel Control Test Techniques C.E. Greenberg, Sikorsky Aircraft Division, UTC May 22, 1989 2012-04-03
Forum 45 Air-To-Air Combat Test IV (AACT IV) and the AACT Data Base D.A. Skrinjorich and G.T. White, U.S. Army Aviation Applied Technology Dir. May 22, 1989 2012-04-03
Forum 45 The Pointer(tm): Test and Evaluation of the Tiltrotor UAV R.D. McClure and P.G. Hall, Bell Helicopter Textron May 22, 1989 2012-04-03
Forum 45 Efficient Free Wake Calculations Using Analytical/Numerical Matching and Far-Field Linearization D.B. Bliss and W.O. Miller, Duke University May 22, 1989 2012-04-03
Forum 45 Identification of Retreating Blade Stall Mechanisms Using Flight Test Pressure Measurements N.C.G. Isaacs and R.J. Harrison, Westland Helicopters Ltd May 22, 1989 2012-04-03
Forum 45 A Comprehensive Hover Test of the Airloads and Airflow of an Extensively Instrumented Model Helicopter Rotor P.F. Lorber, R.C. Stauter and A.J. Landgrebe, United Technologies Research Center May 22, 1989 2012-04-03
Forum 45 BELLTECH - A Multi-Purpose Navier-Stokes Code for Rotor-Blade and Fixed-Wing Configurations J.B. Malone and J.C. Narramore, Bell Helicopter Textron May 22, 1989 2012-04-03
Forum 45 Optimization of Rotor Performance in Hover and Axial Flight Using a Free Wake Analysis T.R. Quackenbush, A.E. Kaufman, and D.A. Wachspress, Continuum Dynamics, Inc. and D.B. Bliss, Duke University May 22, 1989 2012-04-03
Forum 45 Prediction and Measurement of the Aerodynamic Interactions Between a Rotor and an Airframe in Forward Flight N.M. Komerath, H.M. McMahon, A.G. Brand, S.G. Liou, and D.N. Mavris, Georgia Institute of Technology May 22, 1989 2012-04-03
Forum 45 The LHTEC T800-LHT-800 Engine Integration Into the Agusta A129 Helicopter R.D. Toms Jr., LHTEC and G. Godio, Agusta May 22, 1989 2012-04-03
Forum 45 Flight Testing of the Chandler Evans Adaptive Fuel Control On The S-76A Helicopter D.H. Sweet, Sikorsky Aircraft Division, UTC May 22, 1989 2012-04-03
Forum 45 Icing Research Tunnel Test of a Model Helicopter Rotor T.L. Miller, Sverdrup Technology Inc. and T.H. Bond, NASA Lewis Research Center May 22, 1989 2012-04-03
Forum 45 Initial Results From the Joint NASA-Lewis/U.S. Army Icing Flight Research Tests D. Belte, U.S. Army Aviation Engineering Flight Activity and R.J. Ranaudo, NASA Lewis Research Center May 22, 1989 2012-04-03
Forum 45 A Comprehensive Diagnostic System for the T800-APW-800 Engine K.S. Collinge and A.R. Bilodeau, Textron Lycoming May 22, 1989 2012-04-03
Forum 45 Development of the Improved Helicopter Icing Spray System (IHISS) A.A. Peterson and M.D. Jenks, Boeing Helicopters, and W. Gaitskill, U.S. Army Aviation Systems Command May 22, 1989 2012-04-03
Forum 45 Flight Tests of Adaptive Fuel Control and Decoupled Rotor Speed Control System S.W. Killion, Bell Helicopter Textron May 22, 1989 2012-04-03
Forum 45 Designers as Users: Design Support Based Upon Crew Systems Design Practices W.J. Cody, Search Technology Inc. May 22, 1989 2012-04-03
Forum 45 Human Factors in EMS Helicopter Operations J.K. Lauber and P.J. Kayten, National Transportation Safety Board May 22, 1989 2012-04-03
Forum 45 Overview of NASA Rotorcraft Human Factors Research Program S.G. Hart, NASA Ames Research Center May 22, 1989 2012-04-03
Forum 45 Damage Tolerance Analysis and Testing of a Welded Cluster Gear for the Main Transmission of the Advanced Attack Helicopter T. Shen and W.D. Harris, McDonnell Douglas Helicopter Co. May 22, 1989 2012-04-03
Forum 45 New Concept for Nonmetallic Erosion Protection Systems D.A. Haynie, Bell Helicopter Textron, K.M. Kalumuck, Tracor Hydronautics, Inc., and G.L. Chahine, DYNAFLOW, Inc. May 22, 1989 2012-04-03
Forum 45 Improvement in Structural Integrity and Long Term Durability of Aerospace Composite Components A.K. Munjal, Kaman Aerospace Corp. May 22, 1989 2012-04-03
Forum 45 Structural Tailoring Techniques to Prevent Delamination in Composite Laminates W.R. Pogue, III and A.J. Vizzini, University of Maryland May 22, 1989 2012-04-03
Forum 45 The Use of Fibre Reinforced Thermoplastics for Helicopter Primary Structures and Their Engineering Substantiation S.P. Spurway, Westland Helicopters Ltd and A.C. Duthie, Westland Inc. May 22, 1989 2012-04-03
Forum 45 Evaluation of 3-D Reinforcements in Commingled, Thermoplastic Structural Elements G.T. Rossi, Boeing Helicopters May 22, 1989 2012-04-03
Forum 45 Analysis and Testing of Fiber-Reinforced Thermoplastoc Composite Vertical Stabilizer Skins for an Advanced Attack Helicopter A. Kaizoji, McDonnell Douglas Helicopter Co. May 22, 1989 2012-04-03
Forum 45 A Numerical Analysis of the British Experimental Rotor Program Blade E.P.N. Duque, U.S. Army Aeroflightdynamics Dir. May 22, 1989 2012-04-03
Forum 45 Comparison of Measured Induced Velocities with Results from a Closed-Form Finite State Wake Model in Forward Flight D.A. Peters and C.J. He, Georgia Institute of Technology May 22, 1989 2012-04-03
Forum 45 Tip Vortex Geometry of a Hovering Helicopter Rotor in Ground Effect J.S. Light, NASA Ames Research Center May 22, 1989 2012-04-03
Forum 45 Advanced Rotor Computations with a Corrected Potential Method J.O. Bridgeman, Woodside Summit Group, R.C. Strawn and F.X. Caradonna, U.S. Army Aeroflightdynamics Dir., and C.S. Chen, National Research Council May 22, 1989 2012-04-03
Forum 45 An Investigation of Aerodynamic Interactions between a Rotor and a Fuselage in Forward Flight J.G. Leishman, N. Bi, D.K. Samek and M. Green, University of Maryland May 22, 1989 2012-04-03
Forum 45 Mission Effectiveness Testing of an Adaptive Electronic Fuel Control on an S-76A D.M. Walsh, Sikorsky Aircraft Division, UTC May 22, 1989 2012-04-03
Forum 45 Theoretical and Experimental Correlation of Helicopter Aeromechanics in Hover S.S. Houston and P.C. Tarttelin, Royal Aerospace Establishment May 22, 1989 2012-04-03
Forum 45 Active Control of Gust- and Interference-Induced Vibration of Tilt-Rotor Aircraft N.D. Ham, N.M. Wereley, and K.D. von Ellenrieder, Massachusetts Institute of Technology May 22, 1989 2012-04-03
Forum 45 Identification of Mathematical Derivative Models for the Design of a Model Following Control System J. Kaletka and W. von Grunhagen, DLR May 22, 1989 2012-04-03
Forum 45 Helicopter Flight Control System Design and Evaluation for NOE Operations Using Controller Inversion Techniques R.M. McKillip Jr. and T.A. Perri, Princeton University May 22, 1989 2012-04-03
Forum 45 Helicopter Simulation Development By Correlation With Frequency Sweep Flight Test Data T.T. Kaplita, J.T. Driscoll, M.A. Diftler, and S.W. Hong, Sikorsky Aircraft Division, UTC May 22, 1989 2012-04-03
Forum 45 Control Sensitivity, Bandwidth and Disturbance Rejection Concerns to Advanced Aircraft S.W. Baillie and J.M. Morgan, National Research Council - Canada May 22, 1989 2012-04-03
Forum 45 A Management Process for CALS Compliant Automation G.B. Webster and R.A.M. White, McDonnell Douglas Helicopter Co. May 22, 1989 2012-04-03
Forum 45 New Technologies and Cost Management Issues E.P. Laughlin, U.S. Army Aviation Systems Command May 22, 1989 2012-04-03
Forum 45 A Synergistic Approach to Logistics Planning and Engine Design M.A. Hall and K.C. Ross, Light Helicopter Turbine Engine Co. May 22, 1989 2012-04-03
Forum 45 State-of-the-Art Dehumidification: Cost Effective Corrosion Prevention O.R. Thompson, Logis-Tech, and C.S. Laurent, Munters Cargocaire May 22, 1989 2012-04-03
Forum 45 Human Factors in Helicopter Maintenance and Inspection K.A. Pierce and J.T. Moran, Aerospatiale May 22, 1989 2012-04-03
Forum 45 A Review of the V-22 Health Monitoring System M.J. Augustin and G.D. Middleton, Bell Helicopter Textron May 22, 1989 2012-04-03
Forum 45 Creating a Commercial Tiltrotor (CRT) System (Product Support Perspectives) T.K. Fleming, G.M. Powell, and R.R. Reber, Bell Helicopter Textron with S. Mayer, Boeing Helicopters May 22, 1989 2012-04-03
Forum 45 The Future of Field Service Representatives L.T. Huntley, Aerospatiale May 22, 1989 2012-04-03
Forum 45 EH101 Design and Development Status R.I. Case, Westland Helicopters Ltd and F. Reina, Agusta May 22, 1989 2012-04-03
Forum 45 Helicopter Design Optimization For Maneuverability and Agility J. Olson and M. Scott, Sikorsky Aircraft Division, UTC May 22, 1989 2012-04-03
Forum 45 Preliminary Comparisons of Tilt Rotor and Compound Helicopter for Civil Applications J. Esculier, STPA/HE, B. Gmelin and U. Schmidt, DLR, D. Humpherson, Westland Helicopters Ltd, A. Jones, RAE, A. LePretre, Aerospatiale, J-J. Philippe, ONERA, A. Rauen, MBB, and J. Stevens, NLR May 22, 1989 2012-04-03
Forum 45 The New Spheriflex Tail Rotor For The Super Puma Mark II B. Guimbal and J-L. Leman, Aerospatiale May 22, 1989 2012-04-03
Forum 45 The Four-Bladed Main Rotor System For The AH-1W Helicopter J.H. Harse, Bell Helicopter Textron May 22, 1989 2012-04-03
Forum 45 A Comparison of Four vs. Five Blades For The Main Rotor of a Light Helicopter K.B. Amer, Consultant, RAND Corporation May 22, 1989 2012-04-03
Forum 45 RSRA/X-Wing Flight Control System Development: Lessons Learned L.D. Corliss, NASA Ames Research Center, W.R. Dunn, University of Southern Colorado, M.A. Morrison, Morrison Consultants, Inc. May 22, 1989 2012-04-03
Forum 45 Avionics and Electromagnetic Compatibility (EMC) Considerations on an Advanced Composite Airframe G.W. Osborne, Bell Helicopter Textron May 22, 1989 2012-04-03
Forum 45 Helicopter Obstacle Avoidance System: The Use of Manned Simulation To Evaluate The Contribution of Key Design Parameters P. Cerchie and A.C. Flackbert, McDonnell Douglas Helicopter Co. and D. Reago, U.S. Army CECOM Center for Night Vision and Electro-Optics May 22, 1989 2012-04-03
Forum 45 Fully Automatic Guidance for Rotorcraft Nap-of-the-Earth Flight Following Planned Profiles P.J. Gorder, W.F. Clement, and W.F. Jewell, Systems Technology, Inc. May 22, 1989 2012-04-03
Forum 45 OPST 1 - An Optical Yaw Control System for High Performance Helicopters M. Stock, H. Koning, and S. Zeller, MBB Helicopter Division May 22, 1989 2012-04-03
Forum 45 Design Criteria for Helicopter Night Pilotage Sensors R.H. Vollmerhausen and C.J. Nash, U.S. Army CECOM Center for Night Vision and Electro-Optics May 22, 1989 2012-04-03
Forum 45 Adapting Air to Ground Acquisition Systems to the Air to Air Task E. Wilson, McDonnell Douglas Helicopter Co. May 22, 1989 2012-04-03
Forum 45 V-22 Ballistic Vulnerability Hardening Program D. Liardon and J. Johnson, Bell Helicopter Textron and J. Holtrop, Naval Weapons Center May 22, 1989 2012-04-03
Forum 45 Preliminary Design of Advanced Counter-Air System B. Fry and B. Driggs, IBM Federal Systems Div. and K.A. Stanzione and R.F. Smith, Praxis Technologies Corp. May 22, 1989 2012-04-03
Forum 45 Unique Methodology Used in the Bell-Boeing V-22 Main Landing Gear Landing Loads Analysis and Drop Tests Barbara McCown-McClintick, Boeing Helicopters; Ralph Darlington, Dowty Canada Limited May 22, 1989 2020-13-01
Forum 45 Linear Control Issues in the Higher Harmonic Control of Helicopter Vibrations S.R. Hall and N.M. Wereley, Massachusetts Institute of Technology May 22, 1989 2012-04-03
Forum 45 Rotor Loads Validation Utilizing a Coupled Aeroelastic Analysis with Refined Aerodynamic Modeling M.S. Torok and I. Chopra, University of Maryland May 22, 1989 2012-04-03
Forum 45 Stability of Hingeless Rotors in Hover Using Three Dimensional Unsteady Aerodynamics D.H. Hodges, O.J. Kwon, and L.N. Sankar, Georgia Institute of Technology May 22, 1989 2012-04-03
Forum 45 The Effect of An Unsteady Three-Dimensional Wake on Elastic Blade-Flapping Eigenvalues in Hover D.A. Peters and A. Su, Georgia Institute of Technology May 22, 1989 2012-04-03
Forum 45 Periodic Response of Thin-Walled Composite Blades O. Rand, Israel Institute of Technology May 22, 1989 2012-04-03
Forum 45 Relative Aeromechanical Stability Characteristics for Hingeless and Bearingless Rotors W. Weller, United Technologies Research Center May 22, 1989 2012-04-03
Forum 45 UCAR(R) 2040, A Novel Wear Resistant Coating for Aircraft Structural Components J.M. Quets, Union Carbide Coatings Service Corp. May 22, 1989 2012-04-03
Forum 45 Strike Tolerant Main Rotor Blade Tip P.F. Maloney and D. Daly, Kaman Aerospace Corp., and L.T. Burrows, U.S. Army Aviation Applied Technology Dir. May 22, 1989 2012-04-03
Forum 45 Modeling Strategies for Crashworthiness Analysis of Landing Gears A. Bolukbasi and J. Sen, McDonnell Douglas Helicopter Co. May 22, 1989 2012-04-03
Forum 45 Design and Analysis of Composite Structures with Manufacturing Flaws C. Kassapoglou and J. Hammer, Sikorsky Aircraft Division, UTC May 22, 1989 2012-04-03
Forum 45 Effects of Damage on Post Buckled Skin Stiffener Composite Skin Panels N.D. Phan and W.J. Kesack, Boeing Helicopters May 22, 1989 2012-04-03
Forum 45 Torsional Buckling Analysis and Damage Tolerance of Graphite/Epoxy Shafts O.A. Bauchau, P.S. Bryan and A.W. Peck, Rensselaer Polytechnic Institute May 22, 1989 2012-04-03
Forum 45 Aerodynamic Design of the V-22 Osprey Proprotor Farrell, M. K, Bell Helicopter Textron, Inc. May 22, 1989 2014-10-04
Forum 46 Bell's Design Approach for Future Rotorcraft Mainenance/Diagnostics H. Franks, R. Samson, R. Patten, J. Emery, Bell Helicopter Textron Inc. May 21, 1990 2020-24-08
Forum 46 An Experimental Investigation of Rotor Blade Airloads and Wake Structure at High Advance Ratio T. L. Wood, A. G. Brand, Bell Helicopter Textron Inc.; J. W. Elliot, USAARTA-AVSCOM May 21, 1990 2020-24-08
Forum 46 Validation of the Dynamic Response of a Blade-Element UH-60 Simulation Model in Hovering Flight Mark G. Ballin, NASA Ames Research Center; Marie-Alix Dalang-Secretan, Sterling Software, Inc. May 21, 1990 2020-24-08
Forum 46 Estimation of UH-60 Blade Aerodynamic Loads And Rotor Impedance Using Generalized Strain Pattern / Kalman Filter Approach Ofer Bruhis, Ronald W. DuVal, Advanced Rotorcraft Technology, Inc.; Moshe Idan, Stanford University, CA May 21, 1990 2020-24-08
Forum 46 Physical Aspects of Rotor Body Coupling In Stability And Control H. C. Curtiss, Jr., Princeton University May 21, 1990 2020-24-08
Forum 46 V-22 Government Test Pilot Trainer Program Overview John D. McCrillis, W. Rusty Lowry, Naval Air Test Center May 21, 1990 2020-24-08
Forum 46 Noise Mechanisms of Trnsonic Blade-Vortex Interactions A. S. Lyrintzis, Y. Xue, University of Minnesota May 21, 1990 2020-24-08
Forum 46 Automated Threat Assessment and Response Ira Glickstein, IBM - Federal Sector Division May 21, 1990 2020-24-08
Forum 46 Helicopter Design Support Testing in the McDonnell Douglas Research Laboratories Hover Research Facility James H. Ekins, Kondala R. Saripalli, Roger L. Smith, McDonnell Douglas Helicopter Company May 21, 1990 2020-24-08
Forum 46 XV-15 Tiltrotor Aircraft Noise Characteristics Bryan D. Edwards, Bell Helicopter Textron Inc. May 21, 1990 2020-24-08
Forum 46 Can Your Turbine Survive A Half Century George J. Pond, Textron Lycoming Stratford Division May 21, 1990 2020-24-08
Forum 46 Program And Operational Highlights Of The Armed OH-58D Kiowa Warrior Myron Michael Kawa, Bell Helicopter Textron, Inc.; Jack M. Van Kirk, US Army Program Executive Office - Aviation May 21, 1990 2018-03-10
Forum 46 Analysis and Prediction of Tilt Rotor Hover Noise Charles D. Coffen, Albert R. George, Cornell University May 21, 1990 2020-20-02
Forum 46 An Evaluation of Active Control of Structural Response as a Means of Reducing Helicopter Vibration A.E. Staple, Westland Helicopters Ltd. May 21, 1990 2012-04-03
Forum 46 Test and Evaluation of Fuselage Vibration Utilizing Active Control of Structural Response (ACSR) Optimized to ADS-27 W.A. Welsh, and P.C. Von Hardenberg, P.W. Von Hardenberg, Sikorsky Aircraft Div., UTC, and A.E. Staple, Westland Helicopters Ltd. May 21, 1990 2012-04-03
Forum 46 Test and Evaluation of Fuselage Vibration Utilizing Active Control of Structural Response (ACSR) Optimized to ADS-27 W.A. Welsh, and P.C. Von Hardenberg, P.W. Von Hardenberg, Sikorsky Aircraft Div., UTC, and A.E. Staple, Westland Helicopters Ltd. May 21, 1990 2012-04-03
Forum 46 An Experimental and Analytical Investigation of Dynamic Stall Effects on Isolated Rotor Flap-Lag Stability D. Barwey, G.H. Gaonkar, Florida Atlantic University and R.A. Ormiston, Aeroflightdynamics Directorate, U.S. Army AVSCOM May 21, 1990 2012-04-03
Forum 46 An Experimental and Analytical Investigation of Dynamic Stall Effects on Isolated Rotor Flap-Lag Stability D. Barwey, G.H. Gaonkar, Florida Atlantic University and R.A. Ormiston, Aeroflightdynamics Directorate, U.S. Army AVSCOM May 21, 1990 2012-04-03
Forum 46 Development of UMARC (University of Maryland Advanced Rotorcraft Code) G.S. Bir, I. Chopra, The University of Maryland and K. Nguyen, NASA Ames Research Center May 21, 1990 2012-04-03
Forum 46 Development of UMARC (University of Maryland Advanced Rotorcraft Code) G.S. Bir, I. Chopra, The University of Maryland and K. Nguyen, NASA Ames Research Center May 21, 1990 2012-04-03
Forum 46 On Chaos Methods Applied to Higher Harmonic Control M.M. Sarigul-Klijn, U.S. Navy, R. Kolar, E.R. Wood, Naval Postgraduate School, F.K. Straub, McDonnell Douglas Helicopter Co. May 21, 1990 2012-04-03
Forum 46 On Chaos Methods Applied to Higher Harmonic Control M.M. Sarigul-Klijn, U.S. Navy, R. Kolar, E.R. Wood, Naval Postgraduate School, F.K. Straub, McDonnell Douglas Helicopter Co. May 21, 1990 2012-04-03
Forum 46 Frequency-Response Method for Rotorcraft System Identification with Applications to the BO-105 Helicopter M.B. Tischler, Aeroflightdynamics Directorate, U.S. Army AVSCOM and M.G. Cauffman, Sterling Federal Systems, Inc. May 21, 1990 2012-04-03
Forum 46 Frequency-Response Method for Rotorcraft System Identification with Applications to the BO-105 Helicopter M.B. Tischler, Aeroflightdynamics Directorate, U.S. Army AVSCOM and M.G. Cauffman, Sterling Federal Systems, Inc. May 21, 1990 2012-04-03
Forum 46 Finite Element Model Reduction Application to Parametric Studies and Optimization of Rotorcraft Structures M. Hashemi-kia and M. Toossi, McDonnell Douglas Helicopter Co. May 21, 1990 2012-04-03
Forum 46 Finite Element Model Reduction Application to Parametric Studies and Optimization of Rotorcraft Structures M. Hashemi-kia and M. Toossi, McDonnell Douglas Helicopter Co. May 21, 1990 2012-04-03
Forum 46 Preliminary Assessment of a Supersonic STVOL Flight Research and Demonstration Aircraft J.J. Samuels and G.A. Payne, NASA Ames Research Center May 21, 1990 2012-04-03
Forum 46 Numerical Simulation of Powered-Lift Flows W.R. VanDalsem, K. Chawla, M.H. Smith, NASA Ames Research Center and P. Abeloff, University of Colorado May 21, 1990 2012-04-03
Forum 46 V/STOL Concepts for Special Operations A.D. Disselkoen, U.S. Air Force May 21, 1990 2012-04-03
Forum 46 Trail Rotor V/STOL Aircraft, Features and Applications K.W. Sambell, D.S. JanakiRam, and L.J. Silverthorn, McDonnell Douglas Helicopter Co. May 21, 1990 2012-04-03
Forum 46 Advanced Methods of Helicopter Propulsion System Integration/Air Management System Design K.E. Boyd and E. Murgia, McDonnell Douglas Helicopter Co. May 21, 1990 2012-04-03
Forum 46 Advanced Rotorcraft Transmission Program R.C. Bill, Propulsion Directorate, U.S. Army AVSCOM May 21, 1990 2012-04-03
Forum 46 Diagnostic Systems Research Applicable to Helicopter Transmissions H.J. Rose, Boeing Helicopters May 21, 1990 2012-04-03
Forum 46 Modeling of Helicopter Transmissions for Vibration and Noise Prediction M. Meyyappa, M. Toossi, and M. Hashemi-kia, McDonnell Douglas Helicopter Co. May 21, 1990 2012-04-03
Forum 46 Passive Infrared Ice Detection for Helicopter Applications A.L. Dershowitz and R.J. Hansman Jr., Massachusetts Institute of Technology May 21, 1990 2012-04-03
Forum 46 Icing Tests of a Model Main Rotor T.H. Bond, NASA Lewis Research Center, R.J. Flemming, Sikorsky Aircraft Div., UTC, and R.K. Britton, Sverdrup Technology, Inc. May 21, 1990 2012-04-03
Forum 46 Advanced Helicopter Avionics A. Raz, Elbit Computers Ltd. May 21, 1990 2012-04-03
Forum 46 Increasing Helicopter Survivability Through Information Fusion J. Dasaro, Aviation Research and Development Activity, U.S. Army AVSCOM May 21, 1990 2012-04-03
Forum 46 Manned Simulation Study Results Concerning Design Parameters for an Effective Helicopter Obstacle Avoidance System (OASYS) P.H. Cerchie, B. Shipley, R.B. Aust, and J.W. Wasson, McDonnell Douglas Helicopter Co., and D. Reago, U.S. Army CNVEO May 21, 1990 2018-27-06
Forum 46 Manned Simulation Study Results Concerning Design Parameters for an Effective Helicopter Obstacle Avoidance System (OASYS) P.H. Cerchie, B. Shipley, R.B. Aust, and J.W. Wasson, McDonnell Douglas Helicopter Co., and D. Reago, U.S. Army CNVEO May 21, 1990 2012-04-03
Forum 46 CGAD Technical Data System D.R. Nelson, Rockwell International May 21, 1990 2012-04-03
Forum 46 Flight Data Acquisition Methodology for Validation of Passive Ranging Algorithms for Obstacle Avoidance P.N. Smith, NASA Ames Research Center May 21, 1990 2012-04-03
Forum 46 Can Shock Waves on Helicopter Rotors Generate Noise? A Study of Quadrupole Source F. Farassat, NASA Langley Research Center, and H. Tadghighi, McDonnell Douglas Helicopter Co. May 21, 1990 2012-04-03
Forum 46 The Acoustic Results of a United Technologies Scale Model Helicopter Rotor Tested at DNW S.R. Liu, Aeroflightdynamics Directorate, U.S. Army AVSCOM, and M.A. Marcolini, NASA Langley Research Center May 21, 1990 2012-04-03
Forum 46 Prediction of Blade-Vortex Interaction Noise Using Airloads Generated by a Finite-Difference Technique H. Tadghighi, A.A. Hassan, and B. Charles, McDonnell Douglas Helicopter Co. May 21, 1990 2012-04-03
Forum 46 Three-Dimensional Shock Fitting for Transonic Rotor Acoustics V.L. Wells, T.E. Vincent, Arizona State University, and J.W. Rutherford, McDonnell Douglas Helicopter Co. May 21, 1990 2012-04-03
Forum 46 Validation of a New General Aerospatiale Aeroelastic Rotor Model Through the Wind Tunnel and Flight Tests Data M. Allongue and T. Krysinski, Aerospatiale Helicopter Division May 21, 1990 2012-04-03
Forum 46 Validation of a New General Aerospatiale Aeroelastic Rotor Model Through the Wind Tunnel and Flight Tests Data M. Allongue and T. Krysinski, Aerospatiale Helicopter Division May 21, 1990 2012-04-03
Forum 46 A Modal-Based Procedure for Efficiently Predicting Low Vibration Rotor Designs W.H. Weller and M.W. Davis, United Technologies Research Center May 21, 1990 2012-04-03
Forum 46 A Modal-Based Procedure for Efficiently Predicting Low Vibration Rotor Designs W.H. Weller and M.W. Davis, United Technologies Research Center May 21, 1990 2012-04-03
Forum 46 Application of Nonlinear Programming Techniques to Dynamic Correlation and Design of Helicopter Structures T.L.C. Chen, W.J. Twomey, and S. Pizzolato, Sikorsky Aircraft Div., UTC May 21, 1990 2012-04-03
Forum 46 Application of Nonlinear Programming Techniques to Dynamic Correlation and Design of Helicopter Structures T.L.C. Chen, W.J. Twomey, and S. Pizzolato, Sikorsky Aircraft Div., UTC May 21, 1990 2012-04-03
Forum 46 Nonlinear Coupled Rotor-Fuselage Helicopter Vibration Studies with Higher Harmonic Control P.P. Friedmann, C. Venkatesan, and I. Papavassiliou, University of California, Los Angeles May 21, 1990 2012-04-03
Forum 46 Nonlinear Coupled Rotor-Fuselage Helicopter Vibration Studies with Higher Harmonic Control P.P. Friedmann, C. Venkatesan, and I. Papavassiliou, University of California, Los Angeles May 21, 1990 2012-04-03
Forum 46 Hingeless Rotor Blade Stability Using a Coupled Aeroelastic Analysis with Refined Aerodynamic Modeling M.S. Torok and I. Chopra, University of Maryland May 21, 1990 2012-04-03
Forum 46 Hingeless Rotor Blade Stability Using a Coupled Aeroelastic Analysis with Refined Aerodynamic Modeling M.S. Torok and I. Chopra, University of Maryland May 21, 1990 2012-04-03
Forum 46 An Enhanced Integrated Aerodynamic Load/Dynamic Approach to Optimum Rotor Blade Design A. Chattopadhyay, Analytical Services & Materials Inc. and Y.D. Chiu, Lockheed Engineering & Sciences Co. May 21, 1990 2012-04-03
Forum 46 An Enhanced Integrated Aerodynamic Load/Dynamic Approach to Optimum Rotor Blade Design A. Chattopadhyay, Analytical Services & Materials Inc. and Y.D. Chiu, Lockheed Engineering & Sciences Co. May 21, 1990 2012-04-03
Forum 46 Status of Integrated Multidisciplinary Rotorcraft Optimization Research at the Langley Research Center W.R. Mantay, Aerostructures Directorate, U.S. Army AVSCOM, and H.M. Adelman, NASA Langley Research Center May 21, 1990 2012-04-03
Forum 46 MBB's BO 108 Design and Development H.B. Huber and C. Schick, MBB May 21, 1990 2012-04-03
Forum 46 The Franco-German Tiger Program, A Development Status K. Schymanietz, MBB and M. Torres, Aerospatiale Helicopter Division May 21, 1990 2012-04-03
Forum 46 Integrated Design Environment-Aircraft (IDEA) S.A. Meyer, McDonnell Douglas Helicopter Co. May 21, 1990 2012-04-03
Forum 46 Advanced Cargo Aircraft Size Optimization C.P. Van Buiten, Sikorsky Aircraft Div., UTC May 21, 1990 2012-04-03
Forum 46 Advanced Rotorcraft V/STOL-Rotary Wing with Airplane Qualities J.J. Schneider and J.B. Wilkerson, Boeing Helicopters May 21, 1990 2012-04-03
Forum 46 Tailboom Design of the 520N NOTAR Helicopter C.S. Rao, McDonnell Douglas Helicopter Co. May 21, 1990 2012-04-03
Forum 46 Tiltrotor Aerodynamic Blade Design by Numerical Optimization Method J. Liu, D.J. Paisley, Boeing Helicopters, and J. Hirsh, Boeing Computer Services May 21, 1990 2012-04-03
Forum 46 The Role of Mission/Task Analysis in Reducing Weapon System Costs and Risks T.B. Aldrich and B.E. Hamilton, Sikorsky Aircraft Div., UTC, and S.M. Szabo, CAE-Link Corporation May 21, 1990 2012-04-03
Forum 46 Structural Evaluation of Composite Fuselage Structure Fabricated Using a THERM-X (sm) Process C. Kassapoglou, A.J. DiNicola, and J.C. Chou, Sikorsky Aircraft Div., UTC May 21, 1990 2012-04-03
Forum 46 Damage Resistance of Graphite/Epoxy Sandwich Panels Under Low Speed Impacts P.H. Wilson Tsang and J. Dugundji, Massachusetts Institute of Technology May 21, 1990 2012-04-03
Forum 46 Static Testing of V-22 Airframe Structure W.J. Kesack and G.N. Bachman, Boeing Helicopters May 21, 1990 2012-04-03
Forum 46 The Effect of the Fracture Process of the Strength of Composite Laminates C.W. Rogers, E.W. Lee, and D.A. Crane, Bell Helicopter Textron Inc. May 21, 1990 2012-04-03
Forum 46 Evaluation of a Simplified Approach to In-Plane Shear Testing for Damage Tolerance Evaluation D. Weems and S. Llorente, Boeing Helicopters May 21, 1990 2012-04-03
Forum 46 Tension Fatigue of Glass/Epoxy and Graphite/Epoxy Tapered Laminates G.B. Murri, T.K. O'Brien, Aerostructures Directorate, U.S. Army AVSCOM, and S.A. Salpekar, Analytical Services and Materials Inc. May 21, 1990 2012-04-03
Forum 46 Composite Actuators/Components for Airborne Systems F. Ching, HR Textron Inc. May 21, 1990 2012-04-03
Forum 46 Composite Actuators/Components for Airborne Systems F. Ching, HR Textron Inc. May 21, 1990 2020-25-11
Forum 46 Aerodynamic Results of a Pressure-Instrumented Nodal Rotor Test at the DNW Lorber, Peter F., United Technologies
May 21, 1990 2012-04-03
Forum 46 Aerodynamic Results of a Pressure-Instrumented Model Rotor Test at the DNW P.F. Lorber, United Technologies Research Center May 21, 1990 2012-04-03
Forum 46 Direct Periodic Solutions of Rotor Free Wake Calculations by Inversion of a Linear Periodic System Miller, Wayne O. and Bliss, Donald B., Duke University
May 21, 1990 2012-04-03
Forum 46 Direct Periodic Solutions of Rotor Free Wake Calculations by Inversion of a Linear Periodic System W.O. Miller and D.B. Bliss, Duke University May 21, 1990 2012-04-03
Forum 46 An Assessment of Full Potential and Euler Solutions for Self-Generated Rotor Blade-Vortex Interactions Hassan, A.A., McDonnell Douglas Helicopter Company; Tung, C., AVSCOM; Sankar, L.N., Georgia Institute of Technology
May 21, 1990 2012-04-03
Forum 46 An Assessment of Full Potential and Euler Solutions for Self-Generated Rotor Blade-Vortex Interactions A.A. Hassan, McDonnell Douglas Helicopter Co., C. Tung, Aeroflightdynamics Directorate, U.S. Army AVSCOM, and L.N. Sankar, Georgia Institute of Technology May 21, 1990 2012-04-03
Forum 46 Model Tilt-Rotor Hover Performance and Surface Pressure Measurement Tung, Chee and Branum, Lonnie, NASA Ames
May 21, 1990 2012-04-03
Forum 46 Model Tilt-Rotor Hover Performance and Surface Pressure Measurement C. Tung and L. Branum, Aeroflightdynamics Directorate, U.S. Army AVSCOM May 21, 1990 2012-04-03
Forum 46 Computation and Measurement of the Flowfield Near a Swept Rotor Blade Tip in Hover Tsung, Fu-Lin, Liou, Shiuh-Guang, Komerath, Narayanan, M., Sankar, Lakshmi N., Georgia Institute of Technology May 21, 1990 2012-04-03
Forum 46 Computation and Measurement of the Flowfield Near a Swept Rotor Blade Tip in Hover F.L. Tsung, S.G. Liou, N.M. Komerath, and L.N. Sankar, Georgia Institute of Technology May 21, 1990 2012-04-03
Forum 46 Results of Wake Surveys on Advanced Rotor Planforms Carlin, G., Farrance, K., Boeing Helicopter
May 21, 1990 2012-04-03
Forum 46 Results of Wake Surveys on Advanced Rotor Planforms G.J. Carlin and K.E. Farrance, Boeing Helicopters May 21, 1990 2012-04-03
Forum 46 Finding the Needle in the Haystack: Results of the Army Flight Safety Parts Surveillance Program Arden, Robert W. and Ross, Cynthia A., U.S. Army Aviation Systems Command
May 21, 1990 2012-04-03
Forum 46 Finding the Needle in the Haystack: Results of the Army Flight Safety Parts Surveillance Program Robert W. Arden and Cynthia A. Ross, U.S. Army Aviation Systems Command May 21, 1990 2012-04-03
Forum 46 Evaluation of Advanced Sandwich Structure Designed For Improved Durability and Damage Tolerance Llorente, Steven, Weems, Douglas, Fay, Russell, Boeing Helicopters
May 21, 1990 2012-04-03
Forum 46 Evaluation of Advanced Sandwich Structure Designed for Improved Durability and Damage Tolerance Steven Llorente, Douglas Weems, and Russel Fay, Boeing Helicopters May 21, 1990 2012-04-03
Forum 46 Damage Tolerance Testing of SH-2 Seasprite Composite Main Rotor Blade K. Drake Klotzman and Frank B. Clark, Kaman Aerospace Corporation May 21, 1990 2012-04-03
Forum 46 Damage Tolerance Testing of SH-2 Seasprite Composite Main Rotor Blade K. Drake Klotzman and Frank B. Clark, Kaman Aerospace Corporation May 21, 1990 2012-04-03
Forum 46 Damage Tolerance Assessment of the HH-53 Helicopter

Douglas R Tritsch and George J. Schneider, Sikorsky Aircraft Division of UTC; Gary Chamberlain, Robins Air Force Base; John W. Lincoln, Wright-Patterson Air Force Base

May 21, 1990 2012-04-03
Forum 46 Damage Tolerance Assessment of the HH-53 Helicopter Douglas E. Tritsch, George J. Schneider, Sikorsky Aircraft Div., UTC; Gary Chamberlain, Warner Robins Air Logistics Center; and John W. Lincoln, Wright-Patterson Air Force Base May 21, 1990 2012-04-03
Forum 46 Safe Strength/Damage Tolerance Assessment vs. a Fail-Safe Approach in the Design of the SH-2G Engine Mount Structure

Charles D. Van Etten and Paul E. Keary, Kaman Aerospace Corporation

May 21, 1990 2012-04-03
Forum 46 Safe Strength/Damage Tolerance Assessment V. a Fail-Safe Approach in the Design of the SH-2G Engine Mount Structure Charles D. Van Etten and Paul E. Keary, Kaman Aerospace Corporation May 21, 1990 2012-04-03
Forum 46 A Computational Method for the Determination of Structural Reliability of Helicopter Dynamic Components Audbur E. Thompson and David O. Adams, United Technologies Corporation May 21, 1990 2012-04-03
Forum 46 A Computational Method for the Determination of Structural Reliability of Helicopter Dynamic Components Audbur .E. Thompson and David O. Adams, Sikorsky Aircraft Div. UTC May 21, 1990 2012-04-03
Forum 46 Interactive Curve for Fatigue Life Prediction of a Comflex ? Rotor Flexure

John E. Fale, Duncan J. Lawrie, and Bhagwati P. Gupta, Lord Corporation

May 21, 1990 2012-04-03
Forum 46 Interactive Curve for Fatigue Life Prediction of a Comflex(tm) Rotor Flexure John E. Fale, Duncan J. Lawrie, and Bhagwati P. Gupta, Lord Corporation May 21, 1990 2012-04-03
Forum 46 Interactive Curve for Fatigue Life Prediction of a Comflex(tm) Rotor Flexure John E. Fale, Duncan J. Lawrie, and Bhagwati P. Gupta, Lord Corporation May 21, 1990 2015-22-12
Forum 46 A New Methodology to Predict and Optimize Rotorcraft Structural Loads/Weights Using Finite Element Method

Sohan Singh and David R. Lindsay, Bell Helicopter Textron

May 21, 1990 2012-04-03
Forum 46 A New Methodology to Predict and Optimize Rotorcraft Structural Loads/Weights Using Finite Element Method Sohan Singh and David R. Lindsay, Bell Helicopter Textron Inc. May 21, 1990 2012-04-03
Forum 46 Champ: A Helicopter/VTOL Flight Model for Integrated Operational Analysis Sally La Forge, James Jennings, and Albert Zobrist, The RAND Corporation May 21, 1990 2012-04-03
Forum 46 CHAMP: A Helicopter/VTOL Flight Model for Integrated Operational Analysis S. LaForge, J. Jennings, and A.L. Zobrist, The Rand Corporation May 21, 1990 2012-04-03
Forum 46 Sustained Combat Availability - A Design Assessment Technique

George Daugherty, Martin Marietta Electronic Systems

May 21, 1990 2012-04-03
Forum 46 Sustained Combat Availability, A Design Assessment Technique G. Daugherty, Martin Marietta Electronic Systems May 21, 1990 2012-04-03
Forum 46 TACTS ? Helicopter Air Combat Training System of the Future

Bernard A. Wunder, Naval Air Test Center

May 21, 1990 2012-04-03
Forum 46 TACTS - Helicopter Air Combat Training System of the Future B.A. Wunder, Naval Air Test Center May 21, 1990 2012-04-03
Forum 46 Design Considerations for a Counterair Situation Awareness Display For Army Aviation Christopher C. Smyth, Frank J. Malkin, and William B. DeBellis, U.S. Army Laboratory Command May 21, 1990 2012-04-03
Forum 46 Design Considerations for a Counterair Situation Awareness Display for Army Aviation C.C. Smyth, F.J. Malkin, and W.B. DeBellis, U.S. Army Human Engineering Laboratory May 21, 1990 2012-04-03
Forum 46 Cargo Rotorcraft in Future Army Operations Gene R. Marner, Marner Systems Corporation; Thomas O. Potthoff, U.S. Army Aviation Systems Command; Daniel P. Schrage, Georgia Institute of Technology May 21, 1990 2012-04-03
Forum 46 Cargo Rotorcraft in Future Army Operations G.R. Marner, Marner System Corporation; T.O. Potthoff, Army Aviation Systems Command; D.P. Schrage, Georgia Institute of Technology May 21, 1990 2012-04-03
Forum 46 An In-Flight Investigation of Symbology Drive Law Improvements to an Operational Attack Helicopter Jeffery A. Schroeder, NASA Ames; Michelle M. Eshow, U.S. Army ASC; William S. Hindson, NASA Ames May 21, 1990 2012-04-03
Forum 46 An In-Flight Investigation of Symbology Drive Law Improvements to an Operational Attack Helicopter J.A. Schroeder, W.S. Hindson, NASA Ames Research Center, and M.M. Eshow, Aeroflightdynamics Directorate, U.S. Army AVSCOM May 21, 1990 2012-04-03
Forum 46 An Evaluation of the Proposed Specification for Handling Qualities of Military Rotorcraft, MIL-H-8501B, Utilizing Predicted and Actual SH-60B Handling Qualities A.N. Cappetta and J.B. Johns, Naval Air Development Center May 21, 1990 2012-04-03
Forum 46 Initial Flight Test Assessment of V-22 Flying Qualities C. Dabundo, Boeing Helicopters and D. Kimball, Bell Helicopter Textron Inc. May 21, 1990 2012-04-03
Forum 46 Formulation and Validation of High-Order Linearized Models of Helicopter Flight Mechanics F.D. Kim, R. Celi, University of Maryland and M.B. Tischler, Aeroflightdynamics Directorate, U.S. Army AVSCOM May 21, 1990 2012-04-03
Forum 46 A Theory for the Analysis of Rotorcraft Operating in Atmospheric Turbulence M.F. Costello, Boeing Helicopters May 21, 1990 2012-04-03
Forum 46 Helicopter Parameter Identification Using a Trained Multi-Perceptron Neural Network Q.M. Lam, L.P. Pelosi, R.H. Clapp, Synetics Corporation and M. Kam, Drexel University May 21, 1990 2012-04-03
Forum 46 International Aspects of Civil Helicopter Operators F.A. Moore, Canadian Helicopters May 21, 1990 2021-27-09
Forum 46 International Aspects of Civil Helicopter Operators F.A. Moore, Canadian Helicopters May 21, 1990 2012-04-03
Forum 46 Marketing Helicopter Services B.S. Bilmes, Aero Marketing Consultants May 21, 1990 2012-04-03
Forum 46 The Economic Impact of Maintenance on the Helicopter Operator R.B. McNab, Edwards and Associates May 21, 1990 2012-04-03
Forum 46 Direct Operating Costs and the Cost of Misunderstanding Them B.M. Battles, Bell Helicopter Textron Inc. May 21, 1990 2012-04-03
Forum 46 Helicopter Insurance-An Overview L. Mattiello, Alpha Aviation Insurance Agency May 21, 1990 2012-04-03
Forum 46 Heliport/Vertiport Development F.L. Jensen Jr., Helicopter Association International May 21, 1990 2012-04-03
Forum 46 V-22 Flight Test - A Promise Fulfilled M.A. McVeigh and H. Rosenstein, Boeing Helicopters May 21, 1990 2012-04-03
Forum 46 Theoretical and Experimental Study of Unsteady Rotor/Body Aerodynamic Interactions G.L. Crouse, J.G. Leishman, and N. Bi, University of Maryland May 21, 1990 2012-04-03
Forum 46 Application of a New Navier-Stokes Inverse Method to the Design of Advanced Airfoils J.C. Narramore, Bell Helicopter Textron Inc., J.B. Malone, NASA Langley Research Center and R. Vermeland, CRAY Research, Inc. May 21, 1990 2012-04-03
Forum 46 New Vortex/Surface Interaction Methods for the Prediction of Wake-Induced Airframe Loads T.R. Quackenbush, C.M. Lam, Continum Dynamics, D.B. Bliss and A. Katz, Duke University May 21, 1990 2012-04-03
Forum 46 Inflow Velocity Perturbations Due to Fuselage Effects in the Presence of a Fully Interactive Wake J.D. Berry and S.L. Althoff, Aerostructures Directorate, U.S. Army AVSCOM May 21, 1990 2012-04-03
Forum 46 Systematic Correlation and Evaluation of the EHPIC Hover Analysis J.P. Shanley, R.C. Moffitt, and S.J. Davis, Sikorsky Aircraft Div., UTC May 21, 1990 2012-04-03
Forum 46 Correlations of Rotor/Wake-Airframe Interaction Measurements with Flow Vizualization Data A.G. Brand, Bell Helicopter Textron Inc., H.M. McMahon, and N.M. Komerath, Georgia Institute of Technology May 21, 1990 2012-04-03
Forum 46 Testing of the V-22 Flight Control System W.L. Ballauer, J.R. Leet, J. Mitchell, and D.R. Eck, Boeing Helicopters May 21, 1990 2012-04-03
Forum 46 Flight Investigation of the Effect of Tail Boom Strakes on Helicopter Directional Control H.L. Kelley, C.A. Crowell, Aerostructures Directorate, U.S. Army AVSCOM, K.R. Yenni, NASA Langley Research Center, and M.B Lance, Lockheed Engineering & Sciences Company May 21, 1990 2012-04-03
Forum 46 Design and Test of an Advanced Technology Landing Gear J.K. Sen, McDonnell Douglas Helicopter Co. and N.A. Chase, U.S. Army Aviation Applied Technology Directorate May 21, 1990 2012-04-03
Forum 46 Endurance Testing of Damaged Main Rotor Upper Thrust Bearings M.C. Frengley and J.D. Eakin, McDonnell Douglas Helicopter Co. May 21, 1990 2015-12-08
Forum 46 Endurance Testing of Damaged Main Rotor Upper Thrust Bearings M.C. Frengley and J.D. Eakin, McDonnell Douglas Helicopter Co. May 21, 1990 2012-04-03
Forum 46 Application of the Wide-Field Shadowgraph Technique to Helicopters in Forward Flight Jeffrey S. Light, NASA Ames Research Center; Alexandra A. Frerking, Sterling Federal Systems; Thomas R. Norman, NASA Ames Research Center May 21, 1990 2012-04-03
Forum 46 Obtaining Consistent Models of Helicopter Flight-Data Measurement Errors using Kinematic-Compatibility and State-Reconstruction Methods J.W. Fletcher, Aeroflightdynamics Directorate, U.S. Army AVSCOM May 21, 1990 2012-04-03
Forum 46 Aerodynamic and Acoustic Test of a United Technologies Model Scale Rotor at DNW Yung H. Yu, Sandy R. Liu, Aeroflightdynamics Directorate, US Army AVSCOM; Anton J. Landgrebe, Peter F. Lorber, United Technologies Research Center; Michael J. Pollack, Sikorsky Aircraft Div., UTC; Ruth M. Martin, NASA Langley Research Center; and Dave E. Jordan, NASA Ames Research Center May 21, 1990 2012-04-03
Forum 46 Advanced Surface Hardening Technologies M.S. Chatterjee, Allison Gas Turbine Division, GM Corporation May 21, 1990 2012-04-03
Forum 46 Composite Group Technology Development K.S. Dehoff, Boeing Helicopters May 21, 1990 2012-04-03
Forum 46 Main Rotor Blade Bonding Automation G.H. Burdorf, F.C. Edman, and R.W. Gobeil, McDonnell Douglas Helicopter Co. May 21, 1990 2012-04-03
Forum 46 Optimizing Wire Crimps Using Taguchi Designed Experiments T.A. Zerby, A. Dragun, and L.A. Grau, McDonnell Douglas Helicopter Co. May 21, 1990 2012-04-03
Forum 46 Case Study of Contoured Tape Laying for Production B.J. Benda and J.P. Fleischman, Bell Helicopter Textron Inc. May 21, 1990 2012-04-03
Forum 46 Robotic Welding of Sheet Metal Parts Using the GTAW Process Mike Harlow and Frank J. Marzano, Allied-Signal Aerospace Co., Garrett Engine Div.; Dale Palmgren, Arizona State University May 21, 1990 2012-04-03
Forum 46 Validation of a Flight Simulation Model of the AH-64 Apache Attack Helicopter Against Flight Test Data J.W. Harding and S.M. Bass, McDonnell Douglas Helicopter Co. May 21, 1990 2012-04-03
Forum 46 A Comparison of Real-Time Blade-Element and Rotor-Map Helicopter Simulations Using Parallel Processing L.D. Corliss, NASA Ames Research Center, R.W. Du Val, H. Gillman, and L.C. Huynh, Advanced Rotorcraft Technology, Inc. May 21, 1990 2012-04-03
Forum 46 NATC Manned Flight Simulator VTOL Ship Motion Simulation and Application B. Ferrier, Canadair Division of Bombardier Inc. and J. Semenza, Rotary Wing Directorate, Naval Air Test Center May 21, 1990 2012-04-03
Forum 47 Frequency Domain Identification of BO 105 Derivative Models with Rotor Degrees of Freedom K.H. Fu and J. Kaletka, DLR, Institut fur Flugmechanik May 6, 1991 2012-04-03
Forum 47 An Integrated Airloads-Inflow Model for Use in Rotor Aeroelasticity and Control Analysis D.A. Peters and A. Su, Georgia Institute of Technology May 6, 1991 2012-04-03
Forum 47 Three Dimensional Analysis of a Rotor in Forward Flight R.G. Rajagopalan and S.R. Mathur, Iowa State University May 6, 1991 2012-04-03
Forum 47 Wing Tip Vortex Calculations with an Unstructured Adaptive-Grid Euler Solver R.C. Strawn, NASA Ames Research Center May 6, 1991 2012-04-03
Forum 47 LH Wind Tunnel Testing: Key to Advanced Aerodynamic Design C. Keys, R. Heminway and M. Sheffler, Boeing Defense and Space Group and S. Weiner, Sikorsky Aircraft May 6, 1991 2012-04-03
Forum 47 Results from a Test of a 2/3 Scale V-22 Rotor and Wing in the 40-by-80-Foot Wind Tunnel F.F. Felker, NASA Ames Research Center May 6, 1991 2012-04-03
Forum 47 V22 Flight Test Aerodynamics W.K. Grauer, Boeing Helicopters and M.K. Farrell, Bell Helicopter Textron, Inc. May 6, 1991 2012-04-03
Forum 47 Flying Qualities Evaluation of the V22 Tiltrotor C. Dabundo and J. White, Boeing Helicopters; M. Joglekar, Bell Helicopter Textron May 6, 1991 2012-04-03
Forum 47 Handling Qualities of the H76 FANTAIL Demonstrator G.P. Wright and J.T. Driscoll, Sikorsky Aircraft and J.D. Nickerson, Boeing Helicopters May 6, 1991 2012-04-03
Forum 47 Identification of Higher-Order Helicopter Dynamics Using Linear Modeling Methods B.L. Aponso, D.E. Johnston, W.A. Johnson and R.E. Magdaleno, Systems Technolgy, Inc. May 6, 1991 2012-04-03
Forum 47 Forward Flight Trim Calculation and Frequency Response Validation of Using a High-Order Helicopter Simulation Model F.D. Kim and R. Celi, University of Maryland; M.B. Tischler, U.S. Army Aeroflightdynamics Directorate May 6, 1991 2012-04-03
Forum 47 Helicopter Control Response Types for Hover and Low Speed Near-Earth Tasks in Degrade Visual Conditions C.L. Blanken and D.C. Hart, Army Aeroflightdynamics Directorate; R. Hoh, Hoh Aeronautics, Inc. May 6, 1991 2012-04-03
Forum 47 Flight Testing the Handling Qualities Requirements of ADS-33C - Lessons Learned at ATTC J.A. Ham and C.P. Butler, U.S. Army Aviation Technical Test Center May 6, 1991 2012-04-03
Forum 47 Practical Robustness Testing for Helicopter Flight Control Systems S.S. Osder and D.G. Caldwell, McDonnell Douglas Helicopter Co. May 6, 1991 2012-04-03
Forum 47 Continuation of the AHS Round Robin on Fatigue Reliability and Damage Tolerance G. Schneider, Sikorsky Aircraft and C. Gunsallus, Kaman Aerospace Corp. (Invited) May 6, 1991 2012-04-03
Forum 47 Probabilistic Fatigue Methodology for Six Nines Reliability R.A. Everett Jr., F. D. Bartlett Jr., W. Elber, U.S. Army Aerostructures Directorate (Invited) May 6, 1991 2012-04-03
Forum 47 Safe Life Reliability: Evaluation of New Statistical Methods H.L. Zion, Boeing Helicopters May 6, 1991 2012-04-03
Forum 47 Reliability of Helicopter Composite Dynamic Components B.R. Krasnowski and S.P. Viswanathan, Bell Helicopter Textron, Inc. May 6, 1991 2012-04-03
Forum 47 A Full Scale Airframe High Cycle Fatigue Test Methodology and its Application to the SH-2G Helicopter P.E. Keary, T. Vothanh, and C.A. Tomashofski, Kaman Aerospace Corp. May 6, 1991 2012-04-03
Forum 47 Mechanics of Curved Fiber Composite H.G. Rai, C.W. Rogers and D.A. Crane, Bell Helicopter Textron, Inc. May 6, 1991 2012-04-03
Forum 47 Expanding USMC Roles for the AH-1W SuperCobra Col. T. Crews, USMC and K.A. Stanzione, Praxis Technologies Corp. May 6, 1991 2012-04-03
Forum 47 Requirements and Possible Technical Solutions Derived from the New Airmobility Concept of the German Army R.D. Von Reth and H. Kohler, MBB May 6, 1991 2012-04-03
Forum 47 Value of Survivability Enhancement Techniques M.D. Homiller, LTV Aircraft Products Group May 6, 1991 2012-04-03
Forum 47 Radar Detection Analysis of Rotor Systems (RADARS) T.L. Gibson, Bell Helicopter Textron, Inc. May 6, 1991 2012-04-03
Forum 47 Rotorcraft Maneuverability and Agility Survivability Sensitivity Analysis (RMSASSA) S.R. Swinsick and S.L. Drummond, McDonnell Douglas Helicopter Co. May 6, 1991 2012-04-03
Forum 47 Tactical Mission Analysis Methodology B.C. Wolven, Bell Helicopter Textron, Inc. May 6, 1991 2012-04-03
Forum 47 The Helicopter Air-to-Air Value-Driven Engagement Model (HAVDEM): Prototype Development N.E. Bent, Decision-Science Applications May 6, 1991 2012-04-03
Forum 47 Effectiveness of V-22 Tiltrotors in Support of Land Combat Operations A.S. Warshawksy, Lawrence Livermore National Laboratory May 6, 1991 2012-04-03
Forum 47 The Design Manufacture of an Advanced Thermoplastic Horizontal Stabilator for the AH-64A M.L. Vitlip, A.D. Stemple and T.R. Lee, McDonnell Douglas Helicopter Co. May 6, 1991 2012-04-03
Forum 47 Automated Combustor Hole Drilling and Inspection System F.R. Moskal III, Garrett Engine Division, Allied Signal Aerospace May 6, 1991 2012-04-03
Forum 47 H-76B FANTAIL Demonstrator Composite Fan Blade Fabrication T. Falasco, E. Zachar and A. Lallo, Boeing Helicopters May 6, 1991 2012-04-03
Forum 47 Intelligent Electrical Harness Connector Assembly Using Bell Helicopter Textron's Wire Harness Automated Manufacturing System D.W. Springer, Bell Helicopter Textron, Inc. May 6, 1991 2012-04-03
Forum 47 Fundamental Research in Helicopter Rotor Blade - Vortex Interaction Modeling D.R. Poling, Boeing Helicopters and M.C. Wilder and D.P. Telionis, Virginia Polytechnic Institute May 6, 1991 2012-04-03
Forum 47 An Analysis of Pitch and Plunge Effects on Unsteady Airfoil Behavior J.C. Tyler and J.G. Leishman, University of Maryland May 6, 1991 2012-04-03
Forum 47 A 3-D Separation Model for Arbitrary Planforms T.S. Beddoes, Westland Helicopters Limited May 6, 1991 2012-04-03
Forum 47 Full-Scale Investigation of Aerodynamic Interactions Between a Rotor and Fuselage T.R. Norman and G.K. Yamauchi, NASA Ames Research Center May 6, 1991 2012-04-03
Forum 47 Helicopter Local Blade Circulation Calculations for a Model Rotor in Forward Flight Using Laser Velocimeter Measurements D.R. Hoad, NASA-Langley Research Center May 6, 1991 2012-04-03
Forum 47 Development of an Advanced Piloted Helicopter Simulation M.E. Dreier, C.M. Kirkpatrick and F.M. Schramm, Bell Helicopter Textron, Inc. May 6, 1991 2012-04-03
Forum 47 Helicopter Modeling Requirements for Full Mission Simulation and Handling Qualities Assessment J. Mayo, J. Occhiato and S.W. Hong, Sikorsky Aircraft May 6, 1991 2012-04-03
Forum 47 Performance and Handling Qualities Criteria for Low Cost Real Time Rotorcraft Simulators - A Methodology Development J.V.R. Prasad, D.P. Schrage, W.D. Lewis and D.G. Wolfe, Georgia Institute of Technology May 6, 1991 2012-04-03
Forum 47 Real-Time Simulation of Helicopter Air-to-Air Combat F. Austin and D. George, Grumman, and C. Bivens, Aeroflightdynamics Directorate, Ames Research Center May 6, 1991 2012-04-03
Forum 47 A Full Mission Simulation Data System J.A. Edwards, Sikorsky Aircraft May 6, 1991 2012-04-03
Forum 47 New Method for Simulating Atmospheric Turbulence for Rotorcraft Applications J. Riaz, J.V.R. Prasad and D.P. Schrage, Georgia Institute of Technology and G.H. Gaonkar, Florida Atlantic University May 6, 1991 2012-04-03
Forum 47 Analysis of Crash Resistant Fuel Systems and Airframe Structure Interaction in a Crash Environment A.O. Bolukbasi, McDonnell Douglas Helicopter Co. May 6, 1991 2012-04-03
Forum 47 Development of a Reclined Crashworthy Crewseat for Rotorcraft G. Yaniv and K.A. Lou, Simula, Inc. and F. Smith, U.S. Army AATD May 6, 1991 2012-04-03
Forum 47 Stress Analysis of Composite Rotor Systems J.C. Fish, McDonnell Douglas Helicopter Co. May 6, 1991 2012-04-03
Forum 47 Flight Service Evaluation of Composite Helicopter Components G.H. Mardoian and M.B. Ezzo, Sikorsky Aircraft May 6, 1991 2012-04-03
Forum 47 Impact Detection in Composite Skin Panels Using Piezoelectric Sensors D.B. Weems, Boeing Helicopters and H.T. Hahn, E. Granlund and I.G. Kim, Penn State University May 6, 1991 2012-04-03
Forum 47 Evaluation of Thermoplastic Matrix Composites for Use in Energy-Absorbing Helicopter Sub-floors S.M. Arndt, Simula, Inc. May 6, 1991 2012-04-03
Forum 47 Vibration Characteristics of Composite I-Beams with Elastic Couplings under Rotation R. Chandra and I. Chopra, University of Maryland May 6, 1991 2012-04-03
Forum 47 Results of Flight Tests of the Boeing/Sikorsky FANTAIL Demonstrator N.D. Lappos and K.D. Phelps, Sikorsky Aircraft May 6, 1991 2012-04-03
Forum 47 Recent Rotorcraft Aeroelastic Testing in the Langley Transonic Dynamics Tunnel W.T. Yeager Jr., P.H. Mirick, M.L. Wilbur, J.D. Singleton, and W.K. Wilkie, U.S. Army Aerostructures and M.N.H. Hamouda, Lockheed Engineering & Sciences Co. May 6, 1991 2012-04-03
Forum 47 Flight Testing the Avionics System of the V22 Osprey K.P. Katz, Boeing Helicopters and R.G. Poulin, Bell Helicopter Textron, Inc. May 6, 1991 2012-04-03
Forum 47 A Computer Programme for the Certification of Helicopter Vertical Take-Off and Landing Operations and an Application to the S-76B Helicopter H.J.G.C. Vodegel and J.M.G.F. Stevens, National Aerospace Laboratory May 6, 1991 2012-04-03
Forum 47 Development Testing of the EH101 Flight Control System R. Muryn, Westland Helicopters Limited May 6, 1991 2012-04-03
Forum 47 Enhanced Diagnostic System for Autoclaves and Bonding Presses J. Bates, Bell Helicopter Textron, Inc. May 6, 1991 2012-04-03
Forum 47 Taguchi Design of Experiments for Problem Solving B. Keith, Bell Helicopter Textron, Inc. May 6, 1991 2012-04-03
Forum 47 An NDT Assessment of the V-22 Osprey T.G. Marshall, Bell Helicopter Textron, Inc. May 6, 1991 2012-04-03
Forum 47 Development of a Shock Noise Prediction Code for High Speed Helicopters - The Subsonically Moving Shock H. Tadghighi and R. Holz, McDonnell Douglas Helicopter Co., and F. Farassat and Y. Lee, NASA Langley Research Center May 6, 1991 2022-26-05
Forum 47 Development of a Shock Noise Prediction Code for High Speed Helicopters - The Subsonically Moving Shock H. Tadghighi and R. Holz, McDonnell Douglas Helicopter Co., and F. Farassat and Y. Lee, NASA Langley Research Center May 6, 1991 2012-04-03
Forum 47 Acoustic Predictions Using Measured Pressures From a Model Rotor in the DNW J.A. Visintainer, Sikorsky Aircraft and C.L. Burley and M.A. Marcolini, NASA Langley Research Center and S.R. Liu, U.S. Army AFDD May 6, 1991 2012-04-03
Forum 47 Computation of the BVI Noise for the BO 105 Model Rotor in Forward Flight and Comparison with Wind-Tunnel Tests M. Schaffar, J. Haertig and P. Gnemmi, Institut Franco-Allemand de Recherches de Saint-Louis May 6, 1991 2012-04-03
Forum 47 A Neural Network for the Identification of Measured Helicopter Noise R.H. Cabell, C.R. Fuller and W.F. O'Brien, Virginia Polytechnic Institute May 6, 1991 2012-04-03
Forum 47 Stage 2 Noise Certification of the Sikorsky S-76A and S-76C Helicopters E.W. Jacobs, R.D. Prillwitz, J.R. Johnson and C.A. Yoerkie Jr., Sikorsky Aircraft May 6, 1991 2012-04-03
Forum 47 A Ray Acoustics Approach to Fuselage Scattering of Rotor Noise N. Attalla and S.A.L. Glegg, Florida Atlantic University (AIAA Exchange Paper) May 6, 1991 2012-04-03
Forum 47 Design Optimization of Rotor Blades for Improved Performance and Vibration C.B. Callahan and F.K. Straub, McDonnell Douglas Helicopter Co. May 6, 1991 2012-04-03
Forum 47 Rotorcraft Airframe Structural Optimization for Combined Vibration and Fatigue Constraints D. Schrage and A. Sareen, Georgia Institute of Technology and T.S. Murthy, Lockheed May 6, 1991 2012-04-03
Forum 47 Hub and Pylon Fairing Integration for Helicopter Drag Reduction D.M. Martin, Sterling Software, R.W. Mort and P.R. Squires, Bell Helicopter Textron, Inc. and L.A. Young, NASA Ames Research Center May 6, 1991 2012-04-03
Forum 47 Closing the Loop on Helicopter Crashworthiness Design Requirements K.B. Amer, RAND Corp. May 6, 1991 2012-04-03
Forum 47 Concurrent Engineering at Boeing Helicopters B. Chiesi, T. Parasida and E. Walliser, Boeing Helicopters May 6, 1991 2012-04-03
Forum 47 Analysis of Rotor Blade Dynamics Using Experimental UH-60A Airloads Obtained at the DNW M.S. Torok and R.K. Goodman, Sikorsky Aircraft May 6, 1991 2012-04-03
Forum 47 Structural Optimization and Mach Scale Test Validation of a Low Vibration Rotor D.K. Young and F.J. Tarzanin Jr., Boeing Helicopters May 6, 1991 2012-04-03
Forum 47 Experimental Investigation of Helicopter Vibration Reduction Using Rotor Blade Aeroelastic Tailoring M.L. Wilbur, U.S. Army Aerostructures Directorate May 6, 1991 2012-04-03
Forum 47 Experimental Investigation of Helicopter Vibration Reduction Using Rotor Blade Aeroelastic Tailoring M.L. Wilbur, U.S. Army Aerostructures Directorate May 6, 1991 2018-29-08
Forum 47 Flight Vibration Testing of the V-22 Tiltrotor Aircraft M.A. Rangacharyulu, Bell Helicopter Textron, Inc. and M.J. Moore, Boeing Helicopters May 6, 1991 2012-04-03
Forum 47 Studying Dynamic Behavior of X380 Helicopter Equipped with a New 5-Blade Composite Rotor C. Serr and M. Trouve, Aerospatiale - Helicopter Division May 6, 1991 2012-04-03
Forum 47 Finite Element Correlation of the U.S. Army/BHTI ACAP Composite Airframe Helicopter R.V. Dompka, Bell Helicopter Textron, Inc. and N.J. Calapodas, U.S. Army Aviation Applied Technology Directorate May 6, 1991 2012-04-03
Forum 47 Dynamic Response of a Variable-Speed Rotor During Rapid Shaft Tilt A.S. Elliot, Mechanical Dynamics, Inc. May 6, 1991 2012-04-03
Forum 47 Design Considerations for a Helicopter Helmet-Mounted Display J. Elia, Sikorsky Aircraft May 6, 1991 2012-04-03
Forum 47 Functionally Integrated Aircraft Instrumentation for the Next Generation Commercial Helicopter D. Geist, McDonnell Douglas Helicopter Co. and Z. Fried, Canadian Marconi Co. May 6, 1991 2012-04-03
Forum 47 Automatic Link Establishment - The Key to Reliable Helicopter NOE Communications G.A. Bradley, Bendix / King May 6, 1991 2012-04-03
Forum 47 GPS-INS Integration Requirements for Robust NOE Helicopter Navigation J.R. Coffee, McDonnell Douglas Helicopter Co. May 6, 1991 2012-04-03
Forum 47 Automatic Flight Control System (AFCS) Honeywell SPZ-7600 for Search and Rescue Helicopters B. Eddy, Honeywell, Inc. May 6, 1991 2012-04-03
Forum 47 V-22 Thrust Power Management Control Law Development J.M. Schaeffer and R. Alwang, Boeing Helicopters and M. Joglekar, Bell Helicopter Textron, Inc. May 6, 1991 2012-04-03
Forum 47 LHTEC T800 Integration in the Agusta A129: A Progress Report D. Risser, LHTEC and G. Godio, Gruppo Agusta S.P.A. May 6, 1991 2012-04-03
Forum 47 Advanced Ice Protection Systems Test in the NASA Lewis Icing Research Tunnel Thomas H. Bond and Jaiwan Shin, NASA Lewis Research Center and Geert A. Mesander, USAF May 6, 1991 2012-04-03
Forum 47 Ongoing Development of a Computer Jobstream to Predict Helicopter Main Rotor Performance in Icing Conditions R.K. Britton, Sverdrup Technology, Inc. May 6, 1991 2012-04-03
Forum 47 Optimization of a Light Helicopter With Arrius Power Plants J.L. Thouvenot, Turbomeca May 6, 1991 2012-04-03
Forum 47 Distortion Tolerance of the T800-LHT-800 Turboshaft Engine W.T. Cousins, R.E. Miller and K.K. Dalton, Garrett Engine Division, Allied Signal Aerospace May 6, 1991 2012-04-03
Forum 47 The Practical Application of New Technology to the Civil Rotorcraft Need J.F. Ward, Ward Associates May 6, 1991 2012-04-03
Forum 47 Committees, Their Importance to the Structures of the Helicopter Association International R.D. Fox, Hillcrest Aviation May 6, 1991 2012-04-03
Forum 47 Rotor Blade Maintenance R.B. McNab, Edwards & Associates May 6, 1991 2012-04-03
Forum 47 A Holistic Approach to Support R.M. Devin, McDonnell Douglas Helicopter Co. May 6, 1991 2012-04-03
Forum 47 Maintenance, Malfunction Information Report (MMIR) System F.L. Jensen Jr., Helicopter Association International May 6, 1991 2012-04-03
Forum 47 High Speed Rotorcraft: Comparison of Leading Concepts and Technology Needs P.D. Talbot, NASA Ames Research Center May 6, 1991 2012-04-03
Forum 47 The Eurofar Vehicle Overview V. Caramaschi, Agusta S.P.A.; W. Muggli, MBB; A. Lepretre and C. Thibaudat, Aerospatiale, and G. Venn, Westland May 6, 1991 2012-04-03
Forum 47 Crash-Resistant Rotorcraft Preliminary Design Optimization A.O. Bolukbasi, McDonnell Douglas Helicopter Co. May 6, 1991 2012-04-03
Forum 47 Tiger Main Gear Box - High Reliability, Low Weight M. Vialle, Aerospatiale, Helicopter Division May 6, 1991 2012-04-03
Forum 47 Aerodynamic Design of a Coanda Induced Force and Thruster Antitorque System H. Velkoff, Sterling Federal Systems and C. Tung, U.S. Army Aeroflightdynamics Directorate May 6, 1991 2012-04-03
Forum 47 V-22 Osprey Tiltrotor Blade Fold/Wing Stow System Design and Testing R.L. Olson, Bell Helicopter Textron, Inc. and W.E. Rumberger, Boeing Helicopters May 6, 1991 2012-04-03
Forum 47 Enhanced Energy Maneuverability for Attack Helicopters Using Continuous Variable (CV) Rotor Speed Control C.G. Schaefer, Naval Air Systems Command and F.H. Lutze, Virginia Polytechnic Institute May 6, 1991 2012-04-03
Forum 47 V22 Pilot-in-the-Loop Aeroelastic Stability Analysis T. Parham Jr. and D. Popelka, Bell Helicopter Textron, Inc. and D.G. Miller and A.T. Froebel, Boeing Defense & Space Group May 6, 1991 2012-04-03
Forum 47 Alleviation of Whirl-Flutter on Tilt-Rotor Aircraft Using Active Controls J.M. Van Aken, Sterling Software May 6, 1991 2012-04-03
Forum 47 Lifting Line Predictions for a Swept Tip Rotor Blade C. Young, Royal Aerospace Establishment Farnborough and W.G. Bousman and T.H. Maier, U.S. Army Aeroflightdynamics Directorate and F. Toulmay, Aerospatiale SNI and N. Gilbert, Aeronautical Research Laboratory Australia May 6, 1991 2012-04-03
Forum 47 Variation in Hover Aeromechanical Stability Trends with Bearingless Main Rotor Design W.H. Weller, United Technologies Research Center May 6, 1991 2012-04-03
Forum 47 Evaluation of an Advanced Finite Element Analysis for Rotor Blades S.Y. Chen and R. Sopher, Sikorsky Aircraft and O. Bauchau, Rensselaer Polytechnic Institute May 6, 1991 2012-04-03
Forum 47 Dynamics of Helicopters with Dissimilar Blades J.M. Wang and I. Chopra, University of Maryland May 6, 1991 2012-04-03
Forum 47 Comparison of Theory and Experiment for Nonlinear Flutter and Stall Response of Helicopter Blade D.M. Tang and E.H. Dowell, Duke University May 6, 1991 2012-04-03
Forum 47 Day/Night Adverse Weather Pilotage System (D/NAPS) R.T. Schwab and R.C. Hood, AATD, AVSCOM May 6, 1991 2012-04-03
Forum 47 Architectural Impact of Blending Machine Intelligence Technology with Full Spectrum Rotorcraft Operations F.E. Huber, IBM Federal Systems Division and K. Wroblewski, McDonnell Douglas Helicopter Co. May 6, 1991 2012-04-03
Forum 47 Increasing Mission Effectiveness with an Intelligent Pilot-Vehicle Interface P.A. Casper and S.R. Smith, Sikorksy Aircraft Sikorsky Aircraft; H.R. Smith, United Technologies Research Center; B. Hubanks, Texas Instruments May 6, 1991 2012-04-03
Forum 47 Advanced Workload Assessment Techniques for Engineering Flight Simulation J.F. Grenell, Boeing Defense & Space Group and A.F. Kramer, E.J. Sirevaag and C.D. Wickens, University of Illinois May 6, 1991 2012-04-03
Forum 47 Comparison of SOMLA and ATB Programs for Prediction of Occupant Motions in Energy-Absorbing Seating Systems L.W. Bark and K. Lou, Simula, Inc. May 6, 1991 2012-04-03
Forum 47 Enhanced Training to Reduce Pilot Error Accidents R.J. Adams, Advanced Aviation Concepts, Inc. and R.W. Weiss, FAA May 6, 1991 2012-04-03
Forum 47 Spares Support of Your Rotary Wing 'Jenny' R.R. Walker, Boeing Helicopters May 6, 1991 2012-04-03
Forum 47 Corrosion Prevention Field Test Utilizing Water Displacement Compounds H.F. Jacobs, McDonnell Douglas Helicopter Co. May 6, 1991 2012-04-03
Forum 47 How to Support the 'Little Guy' R.R. Long, Textron Lycoming May 6, 1991 2012-04-03
Forum 47 Malfunction/Discrepancy Reporting J.B. Swift, Aerospatiale Helicopter Corporation May 6, 1991 2012-04-03
Forum 47 Life Cycle Aviation System Safety Program E.J. Hollman, U.S. Army Aviation Systems Command May 6, 1991 2012-04-03
Forum 47 Combat Maintenance and Gas Turbine Engines D.L. Wensits, Allison Gas Turbine Div., GMC and R. Scardina, Garrett Engine Div., Allied Signal Corp. May 6, 1991 2012-04-03
Forum 47 Life Cycle Hazard Tracking System R.D. Brock, U.S. Army Aviation Systems Command May 6, 1991 2012-04-03
Forum 47 LH-Embedded Training: The First Team's Approach W.E. Hackett Jr. and G.M. Stulb Jr., Boeing Defense & Space Group and R.J. Coleman Jr., Kollsman Co. May 6, 1991 2012-04-03
Forum 48 Influence of Cross Section Variations on the Structural Behaviour of Composite Rotor Blades H. Rapp and R. Worndle, Eurocopter Deutschland GmbH June 3, 1992 2012-04-03
Forum 48 Effects of Dynamics Stall and Structural Modeling on Aeroelastic Stability of Elastic Bending and Torsion of Hingeless Rotor Blades with Experimental Correlation D. Barwey and G.H. Gaonkar, Florida Atlantic University June 3, 1992 2012-04-03
Forum 48 The Development of the Coupled Rotor-Fuselage Model (CRFM) R.E. Hansford, Westland Helicopters Ltd. June 3, 1992 2012-04-03
Forum 48 Aeromechanical Stability of Helicopters with Composite Rotors in Forward Flight E.C. Smith and I. Chopra, University of Maryland June 3, 1992 2012-04-03
Forum 48 Component Vibration Qualification Requirements for the RAH-66 Comanche Helicopter R. Vlaminck, Boeing Defense & Space Group, Helicopters Div. and K. Frederickson, Sikorsky Aircraft Div., UTC June 3, 1992 2012-04-03
Forum 48 On the Effect of Pitch/Mast-Bending Coupling on Whirl-Mode Stability D.L. Kunz, McDonnell Douglas Helicopter Co. June 3, 1992 2012-04-03
Forum 48 Overview of Tiger Dynamics Validation Program T. Krysinski, Eurocopter France and G. Seitz, Eurocopter Deutschland June 3, 1992 2012-04-03
Forum 48 Design of the Variable Pitch Fan for the McDonnell Douglas MD 520N Helicopter Equipped with the NOTAR System D.A. Nyhus and C. Rao, McDonnell Douglas Helicopter Co. June 3, 1992 2012-04-03
Forum 48 Product Development Team Approach for Developing RAH-66 Comanche Airframe Systems B.F Kay, Sikorsky Aircraft Div., UTC June 3, 1992 2012-04-03
Forum 48 McDonnell Douglas? New Light Twin Helicopter: MD EXPLORER R.E. Head and C.W. Hughes, McDonnell Douglas Helicopter Co. June 3, 1992 2012-04-03
Forum 48 Maximum Operational Effectiveness on RAH-66 Comanche W.H. Harper and J.J. Morris, Boeing Sikorsky, RAH-66 Comanche Program Office June 3, 1992 2012-04-03
Forum 48 Antitorque Safety and the RAH-66 Fantail M.G. Clemmons, Boeing Defense and Space Group, Helicopters Div. June 3, 1992 2012-04-03
Forum 48 Lessons Learned During the Development of the AH-64A Apache Attack Helicopter K.B. Amer, R.W. Prouty. G. Korkosz, and D. Fouse, formerly McDoknnell Douglas Helicopter Co. June 3, 1992 2012-04-03
Forum 48 Helmet Mounted Display Symbology Integration Research (HMDSIR) L.A. Haworth and RE. Seery, NASA Ames Research Center June 3, 1992 2012-04-03
Forum 48 Development of an Expert System for Cockpit Emergency Procedures M. Carter, C.D. Holley, and J.H. Emery, Bell Helicopter Textron, Inc. June 3, 1992 2012-04-03
Forum 48 Concept Feasibility Demonstration for the Army Cockpit Delethalization Program R.L. Greth, W.B. Shope, and M.S. Pfaff, LME, Inc. and K.F. Smith, Aviation Applied Technology Directorate June 3, 1992 2012-04-03
Forum 48 Advanced Helicopter Pilotage Visual Requirements J.S. Seeman, J. DeMaio, S. Justice, and J. Wasson, McDonnell Douglas Helicopter Co.; P. Derenski, M. Hunter, and L. Walrath, McDonnell Aircraft Co. June 3, 1992 2012-04-03
Forum 48 Visual Cues in Low-Level Flight: Implications for Pilotage, Training, Simulation, & Enhanced/ Synthetic Vision Systems D.C. Foyle, M.K. Kaiser, and W.W. Johnson, NASA Ames Research Center June 3, 1992 2012-04-03
Forum 48 Digital Terrain Systems for Helicopters B. Darlington and T. Henley, GEC Avionics Limited June 3, 1992 2012-04-03
Forum 48 MIDAS Technology Transfer R.M. Beggs, Boeing Defense & Space Group, Helicopters Div. June 3, 1992 2012-04-03
Forum 48 Visual Augmentation for Night Flight Over Featureless Terrain M.K. Kaiser, W.W. Johnson, and L. Mowafy, NASA Ames Research Center and R.T. Hennessy and J.A. Matsumoto, Monterey Technology, Inc. June 3, 1992 2012-04-03
Forum 48 Configuration Management Impacts on Customer Support and Satisfaction R. Jones Jr. and W.W. Shivers, McDonnell Douglas Helicopter Co. June 3, 1992 2012-04-03
Forum 48 The Criticalness of Spares Effectivity Checks for Aircraft Configuration Control R.F. Gouck, Boeing Defense & Space Group, Helicopters Div. June 3, 1992 2012-04-03
Forum 48 Logistics Support Analysis: An Integrated Approach to Configuration Management R.S. Bodzek, Boeing Defense & Space Group, Helicopters Div. June 3, 1992 2012-04-03
Forum 48 Navy Success in Modification Installation Management M.G. Montilla, Naval Air Systems Command June 3, 1992 2012-04-03
Forum 48 The Importance of Configuration Management: An Overview with Test Program Sets C. Merlenbach, McDonnell Douglas Helicopter Co. June 3, 1992 2012-04-03
Forum 48 Why Wait for CALS/CE? J.R. Tilton, GE Aircraft Engines June 3, 1992 2012-04-03
Forum 48 Controlling Hazardous Configurations in Helicopter Systems E.J. Hollman and B.J. Meyer, U.S. Army Aviation Systems Command June 3, 1992 2012-04-03
Forum 48 Improved Static and Dynamic Performance of Helicopter Powerplant G.N. Leonov, Mil Moscow Helicopter Plant June 3, 1992 2012-04-03
Forum 48 T55 Engine: The Challenge of Torque Measurement A. Dubrow. J. Mathews, and J. Hewitt. Textron Lycoming June 3, 1992 2012-04-03
Forum 48 A Vibration Monitoring Acquisition & Diagnostic System for Helicopter Drive Train Bench Tests D.A. Dousis. Bell Helicopter Textron Inc. June 3, 1992 2012-04-03
Forum 48 A High Deflection Diaphragm Concept (HDD) for Power Transmission Shafting J.A. Stocco, Lucas Aerospace Power Transmission Corp. June 3, 1992 2012-04-03
Forum 48 Results of a Low Power Ice Protection System Test and a New Method of Imaging Data Analysis J. Shin and T.H. Bond, NASA Lewis Research Center and G.A. Mesander, USAF/Oklahoma Air Logistics Center June 3, 1992 2012-04-03
Forum 48 An Advanced Method for Predicting the Performance of Helicopter Propulsion System Ejectors C.C. Folkman, McDonnell Douglas Helicopter Co. June 3, 1992 2012-04-03
Forum 48 Identification of the Open Loop Dynamics of the T700 Turboshaft Engine A. Duyar and Z. Gu, Florida Atlantic Univ., and J.S. Litt, U.S. Army Aviation Systems Command June 3, 1992 2012-04-03
Forum 48 A Finite-Volume Euler Solver for Computing Rotary-Wing Aerodynamics on Unstructured Meshes R.C. Strawn, U.S. Army Aeroflightdynamics Directorate, and T.J. Barth, NASA Ames Research Center June 3, 1992 2012-04-03
Forum 48 Numerical Simulation of a Hovering Rotor Using Embedded Grids E.P.N. Duque. U.S. Army Aeroflightdynamics Directorate, and G.R. Srinivasan, JAI Assoc., Inc. June 3, 1992 2012-04-03
Forum 48 Navier-Stokes Correlations to Fuselage Wind Tunnel Test Data J.C. Narramore and A.G. Brand, Bell Helicopter Textron, Inc. June 3, 1992 2012-04-03
Forum 48 Helicopter Aerodynamic Research Techniques and Rotor-Fuselage Interaction Analysis V.B. Letnikov, Mil Moscow Helicopter Plant June 3, 1992 2012-04-03
Forum 48 Vortex Methods for the Computational Analysis of Rotor/Body Interaction T.R. Quackenbush and C.M.G. Lam, Continuum Dynamics. Inc., and D.B. Bliss and A.L Katz, Duke Univ. June 3, 1992 2012-04-03
Forum 48 Three-Dimensional Calculations of a Rotor-Airframe Interaction in Forward Flight L.A.J. Zori, S.R. Mathur, and R.G. Rajagopalan, Iowa State University June 3, 1992 2012-04-03
Forum 48 Interactional Aerodynamics Effects on Rotor Performance in Hover and Forward Flight G.L. Crouse Jr. and J.G. Leishman, University of Maryland June 3, 1992 2012-04-03
Forum 48 Eyes for the Fleet: Tiltrotor UAVs in an Integrated Combat System R.J. Scholes, Bell Helicopter Textron, Inc. and T.D. Lowe, Paramax Systems June 3, 1992 2012-04-03
Forum 48 Assessing the Impact of Reduced Airspeed on Tiltrotor Support to Ground Combat A.S. Warshawsky, D.U. Olness, and M.J. Uzelac, Lawrence Livermore National Laboratory June 3, 1992 2012-04-03
Forum 48 A Taguchi Analysis of Helicopter Maneuverability and Agility S.R. Swinsick, McDonnell Douglas Helicopter Co. June 3, 1992 2012-04-03
Forum 48 Analytical Simulation of a Helicopter Mounted Turreted Gun System with Active Control J. Peters, M. Hashemi-Kia, and M. Toossi, McDonnell Douglas Helicopter Co. June 3, 1992 2012-04-03
Forum 48 A Portable Mission Performance and Planning Computer System for Military Helicopter Operations K.A. Stanzione and R.F. Smith, Praxis Technologies Corp. June 3, 1992 2012-04-03
Forum 48 JTVX - Joint Service Requirements for Tactical Missions J.P. Donnelly and D. Newman. Boeing Defense & Space Group, Helicopters Div. June 3, 1992 2012-04-03
Forum 48 Crack Growth/Damage Tolerance Analysis Methods as Applied to V-22 Fuselage and Empennage R.W. Askin, Boeing Defense & Space Group, Helicopters Div. June 3, 1992 2012-04-03
Forum 48 Application of Generalized Force Determination to a Full Scale Low Cycle Fatigue Test of the SH-2G Helicopter C.A. Tomashofski, E.J. Nagy, and P.E. Keary, Kaman Aerospace Corp.` June 3, 1992 2012-04-03
Forum 48 Development of a Failure Prediction Methodology for Adhesive-Bonded Composites E.W.Y. Lee, Bell Helicopter Textron, Inc. June 3, 1992 2012-04-03
Forum 48 Effects on Load Distribution in a Helicopter Rotor Support Structure Associated with Various Boundary Configurations M. H. Morton and A. Kaizoji, McDonnell Douglas Helicopter Co. June 3, 1992 2012-04-03
Forum 48 Thermoplastic Applications In Helicopter Components J.G. Hutchins, Bell Helicopter Textron, Inc. June 3, 1992 2012-04-03
Forum 48 On Design and Optimization of Curved Composite Beams A.W. Peck and O.A. Bauchau, Rensselaer Polytechnic Institute June 3, 1992 2012-04-03
Forum 48 EH 101 Ship Interface Trials R. Longobardi, G. Vismara, and B. Paggi, Gruppo Agusta June 3, 1992 2012-04-03
Forum 48 Mi-26 Autorotational Landings G.R. Karapetyan, Mil Moscow Helicopter Plant June 3, 1992 2012-04-03
Forum 48 Side-by-Side Hover Performance Comparison of MDHC 500 NOTAR and Tail Rotor Anti-Torque Systems R.E. Bregger and S. Dawson, McDonnell Douglas Helicopter Co. June 3, 1992 2012-04-03
Forum 48 A Study of the Rotor Wake of a Small-Scale Rotor Model in Forward Flight Using Laser Light Sheet Flow Visualization with Comparisons to Analytical Models T.A. Ghee, Analytical Services & Materials, Inc., and J.W. Elliott, U.S. Army Aerostructures Directorate June 3, 1992 2012-04-03
Forum 48 A Piloted Simulation Investigation of Pitch and Roll Handling Qualities Requirements for Air-to-Air Combat M.S. Whalley, U.S. Army Aeroflightdynamics Directorate, and W.R. Carpenter, Sterling Federal Systems, Inc. June 3, 1992 2012-04-03
Forum 48 Effects of Higher Order Dynamics on Helicopter Flight Control Law Design S.J. Ingle, Boeing Defense & Space Group, Helicopters Div., and R. Celi, University of Maryland June 3, 1992 2012-04-03
Forum 48 Frequency-Domain Identification of Coupled Rotor/Body Models of an Advanced Attack Helicopter J.W. Harding, McDonnell Douglas Helicopter Co. June 3, 1992 2012-04-03
Forum 48 Handling Qualities Testing Using the Mission Orients Requirements of ADS-33C J.A. Ham and M. Metzger, U.S. Army Aviation Technical Test Center, R.H. Hoh, Hoh Aeronautics, Inc. June 3, 1992 2012-04-03
Forum 48 Improvements in Hover Display Dynamics for a Combat Helicopter M.M. Eshow, U.S. Army Aerotlightdynamics Directorate, and J. Schroeder, NASA Ames Research Center June 3, 1992 2012-04-03
Forum 48 A Simulation Assessment of the Westland Lynx Stability and Command Augmentation System for Air-to-Air Tracking Tasks J. Howitt, Defense Research Agency June 3, 1992 2012-04-03
Forum 48 A Closed Loop Controller for BVI Impulsive Noise Reduction by Higher Harmonic Control Dr. R. Kube and W.R. Splettstoesser, DLR Institute fur Flugmechanik, M. Achache, Eurocopter France and G. Niesl, Eurocopter Deutschland June 3, 1992 2012-04-03
Forum 48 Effects of Ingested Atmospheric Turbulence on Measured Tail Rotor Acoustics D.B. Signor, G.K. Yamauchi, M. Mosher, NASA Ames Research Center, M.J. Hagen, California Polytechnic State Univ., and A.R. George, Cornell Univ. June 3, 1992 2012-04-03
Forum 48 An Analysis on High Speed Impulsive Noise of Transonic Helicopter Rotor O. Rho and Y.S. Kim, Seoul National University June 3, 1992 2012-04-03
Forum 48 Prediction of BVI Noise Patterns and Correlation with Wake Interaction Locations M.A. Marcolini and R.M. Martin, NASA Langley Research Center and P.F. Lorber and T.A. Egolf, United Technologies Research Center June 3, 1992 2012-04-03
Forum 48 Civil Tiltrotor Noise Impact Prediction Methodology R.G. Riley Jr., Bell Helicopter Textron, Inc. June 3, 1992 2012-04-03
Forum 48 Predicting Rotorcraft Transmission Noise J. O'Connell, McDonnell Douglas Helicopter Co. June 3, 1992 2012-04-03
Forum 48 Large Cocured Composite Structure Development for Comanche Airframe A. Dublinski, Sikorsky Aircraft Div., UTC June 3, 1992 2012-04-03
Forum 48 Optimal Composite Curing System P. Handel and D. Guerin, Boeing Defense & Space Group, Helicopters Div. June 3, 1992 2012-04-03
Forum 48 Improved Airframe Manufacturing Technology Demonstration Program P.B. Leoni, Sikorsky Aircraft Div., UTC June 3, 1992 2012-04-03
Forum 48 Spiral Bevel Gear Improved Manufacturing and Control System W.D. Glasow, Sikorksy Aircraft Div., UTC June 3, 1992 2012-04-03
Forum 48 New Developments in Organized Wire Systems J. Hollis, Sikorsky Aircraft Div., UTC June 3, 1992 2012-04-03
Forum 48 An Adaptation of Model Analysis to the Computation of Steady Bending Loads on a Rotating Beam J. Corrigan, G. Sadler and M. Yuce, Bell Helicopter Textron, Inc. June 3, 1992 2012-04-03
Forum 48 An Investigation of Helicopter Rotor Blade Flap Vibratory Loads W.G. Bousman and T.H. Maier, NASA Ames Research Center June 3, 1992 2012-04-03
Forum 48 Application of Component Mode Synthesis to Modeling the Dynamic Response of Bearingless Main Rotors R. Sopher and S. Chen, Sikorsky Aircraft Div., UTC June 3, 1992 2012-04-03
Forum 48 Coupled Rotor Fuselage Mode Shapes - A Tool in Understanding Helicopter Response P.T.W. Juggins, Westland Helicopters, Ltd. June 3, 1992 2012-04-03
Forum 48 Aeroelastic Behavior of Composite Rotor Blades with Swept Tips K. Yuan, P.P. Friedmann, and C. Venkatesan, University of California, L.A. June 3, 1992 2012-04-03
Forum 48 Flap-Lag Damping in Hover and Forward Flight with a Three-Dimensional Wake A.R. Manjunath, Indian Institute of Science, G.H. Gaonkar and J. Nagabhushanam, Florida Atlantic University, D.A. Peters, Washington Univ., and A. Su, Yuan-Ze Institute of Technology June 3, 1992 2012-04-03
Forum 48 Introduction of the M-85 High Speed Rotorcraft Concept R.H. Stroub, NASA Ames Research Center June 3, 1992 2012-04-03
Forum 48 Cost/Weight Savings for the V-22 Wing Stow T.G. Baroth and W.E. Rumberger, Boeing Defense & Space Group, Helicopters Div. June 3, 1992 2012-04-03
Forum 48 Advancing Tiltrotor State-of-the-Art With Variable Diameter Rotors E.A. Fradenburgh and D.G. Matuska, Sikorksy Aircraft Div., UTC June 3, 1992 2012-04-03
Forum 48 Design & Manufacturing Concepts of EUROFAR Model #2 Blades V. Caramaschi and G. Maffioli, Agusta S.p.A. June 3, 1992 2012-04-03
Forum 48 Fail Safety Aspects of the V-22 Pylon Conversion Actuator D.L. Hicks and A.G. Short, Bell Helicopter Textron, Inc. June 3, 1992 2012-04-03
Forum 48 Optimum Design of High Speed Prop-Rotors Using A Multidisciplinary Approach A. Chattapadhyay, Arizona State University and J.R. Narayan, MCAT Institute June 3, 1992 2012-04-03
Forum 48 A Parametric Study of Real Time Mathematical Modeling Incorporating Dynamic Wake and Elastic Blades C. He and W.D. Lewis, Georgia Institute of Technology June 3, 1992 2012-04-03
Forum 48 Helicopter Response to Atmospheric Turbulence J. Riaz, J.V.R. Prasad, and D.P. Schrage, Georgia Institute of Technology and G.H. Gaonkar, Florida Atlantic University June 3, 1992 2019-29-07
Forum 48 Helicopter Response to Atmospheric Turbulence J. Riaz, J.V.R. Prasad, and D.P. Schrage, Georgia Institute of Technology and G.H. Gaonkar, Florida Atlantic University June 3, 1992 2012-04-03
Forum 48 ATTHeS - A Helicopter In-Flight Simulator with High Bandwidth Capability G. Bouwer, H. Pausder, and W. von Guernhagen, DLR June 3, 1992 2012-04-03
Forum 48 Evaluation of Tilt Rotor Aircraft Design Utilizing a Realtime Interactive Simulation F.W. Warburton, Sikorsky Aircraft Div., UTC and H.C. Curtiss, Princeton University June 3, 1992 2012-04-03
Forum 48 Investigation of the Flight Mechanics Simulation of a Hovering Helicopter M. Chaimovich, A. Rosen, and O. Rand, Israel Institute of Technology and M.H. Mansur and M.B. Tischler, USAVSCOM Aeroflightdynamics Directorate June 3, 1992 2012-04-03
Forum 48 Helicopter Rotor Disk and Blade Element Comparison H. Rafati, R.W. Du Val, and O. Bruhis, Advanced Rotorcraft Technology, Inc. June 3, 1992 2012-04-03
Forum 48 Development and Validation of a Comprehensive Real Time AH-64 Apache Simulation Model S.H. Sturisky, W.D. Lewis, D.P. Schrage, and J.V.R. Prasad, Georgia Institute of Technology June 3, 1992 2012-04-03
Forum 48 Rotor Blade Airfoil Design by Numerical Optimization and Unsteady Calculations H. Bezard, ONERA June 3, 1992 2012-04-03
Forum 48 A 2-D Numerical Model for Predicting the Aerodynamic Performance of the NOTAR? System Tailboom R.G. Holz and A.A. Hassan, McDonnell Douglas Helicopter Co., and H.L. Reed, Arizona State University June 3, 1992 2012-04-03
Forum 48 Dynamic Stall of a Sinusoidally Oscillating Three-Dimensional Swept and Unswept Wing in Compressible Flow P.F. Lorber, United Technologies Research Center June 3, 1992 2012-04-03
Forum 48 Shadowgraph Flow Visualization of Isolated Tiltrotor and Rotor/Wing Wakes A.A. Swanson, Sterling Software, and J.S. Light, NASA Ames Research Center June 3, 1992 2012-04-03
Forum 48 Aerodynamic and Wake Methodology Evaluation Using Model UH-60A Experimental Data M.S. Torok and C.R. Berezin, Sikorsky Aircraft Div., UTC June 3, 1992 2012-04-03
Forum 48 Hover Performance Analysis of Advanced Rotor Blades C. Tung, U.S. Army Aeroflightdynamics Directorate and K. Ramachandran, Flow Analysis, Inc. June 3, 1992 2012-04-03
Forum 48 Influence of Coupling Incidence and Velocity Variations on the Airfoil Dynamic Stall D. Favier, J. Belleudy and C. Maresca, l?Universite d' Aix-Marseille II June 3, 1992 2012-04-03
Forum 48 Evaluation of Thermoplastic Stiffened Panels for Applications to Rotorcraft Airframes D.B. Weems and S.G. Llorente, Boeing Defense & Space Group, Helicopters Div. June 3, 1992 2012-04-03
Forum 48 The Development of a Crashworthy Composite Fuselage and Landing Gear H. Barquet and P. Sarlin, Eurocopter France June 3, 1992 2012-04-03
Forum 48 Scaling of Energy Absorbing Composite Plates K.E. Jackson & R. Boitnott, U.S. Army Aerostructures Directorate and J. Morton and C.M. Traffanstedi, V.P.I. June 3, 1992 2012-04-03
Forum 48 Environmental Conditions for Certification Testing of Helicopter Advanced Composite Main Rotor Components A.S. Llanos, L.A. Lucchetto, D. Stafford and C. Coulliette, McDonnell Douglas Helicopter Co. June 3, 1992 2012-04-03
Forum 48 A Nonlinear Analysis Methodology for the Design of Skid Landing Gear L.C. Williams and A.O. Bolukbasi, McDonnell Douglas Helicopter Co. June 3, 1992 2012-04-03
Forum 48 Evaluation of Fatigue Behavior of Discontinuous and Continuous Fibert Thermoplastic Composite Laminates H.A. Whitworth, Howard University, S.G. Llorente, Boeing Defense & Space Group, Helicopters Div. and R. Croman, E.I. DuPont De Nemours Co. June 3, 1992 2012-04-03
Forum 48 Nonlinear Analysis of Composite Thin-Walled Helicopter Blades J.P. Kalfon and O. Rand, TECHNION - Israel Institute of Technology June 3, 1992 2012-04-03
Forum 48 Valisys - A New Quality Assurance Tool J.J. Mazur Jr., Boeing Defense & Space Group, Helicopters Div. June 3, 1992 2012-04-03
Forum 48 Avionics Troubleshooting System M. Mastrianni, Sikorsky Aircraft Div., UTC June 3, 1992 2012-04-03
Forum 48 Knowledge-Based Design for Composite Bond Tools R.A. Moore, Bell Helicopter Textron, Inc. June 3, 1992 2012-04-03
Forum 48 An Application of Knowledge-Based Engineering to Composite Tooling Design S.L. Lewis and P.H. Jouin, McDonnell Douglas Helicopter Co. June 3, 1992 2012-04-03
Forum 48 Unified Process Planning, The Allison Approach C.W. Simmons, Allison Gas Turbine Co., Div. GMC June 3, 1992 2012-04-03
Forum 48 Maximizing the Utilization of Computer-Aided Technology for Fabrication of Composite Structures G.T. Pyle and C.S. Rao, McDonnell Douglas Helicopter Co. June 3, 1992 2012-04-03
Forum 48 Technologies for Automating Rotorcraft Nap-of-the-Earth Flight V.H.L. Cheng and B. Sridhar, NASA Ames Research Center June 3, 1992 2012-04-03
Forum 48 Modular Electronics for Tilt Rotor UAV Payloads J.C. McDade and D.J. Spencer, TRW Military Electronics & Avionics June 3, 1992 2012-04-03
Forum 48 Appraisal of Digital Terrain Elevation Data for Low-Altitude Flight R.E. Zelenka and H.N. Swenson, NASA Ames Research Center June 3, 1992 2012-04-03
Forum 48 Integrated Navigation System for Tactical Helicopters T.M. Pham. D.C. Mossman, and J.R. Coffee, McDonnell Douglas Helicopter Co. June 3, 1992 2012-04-03
Forum 48 A System Solution for Helicopter Nap-of-the-Earth (NOE) Communications K. Wroblewski, McDonnell Douglas Helicopter Co., and R. Rudow, formerly with McDonnell Douglas Helicopter Co. June 3, 1992 2012-04-03
Forum 48 Some Considerations on Indication Means for Helicopter Pilot Vision Systems E.V. Yablonsky, Mil Moscow Helicopter Plant June 3, 1992 2012-04-03
Forum 48 Future Military Operations for the AH-1W: A Desert Storm Perspective Colonel Curtis T. Crews, USMC, NAVAIR; Kaydon A. Stanzione, Praxis Technologies Corporation; David J. Simkins, IBM Federal System Company

This paper was not submitted in time to be included in the printed Proceedings.
June 3, 1992 2012-05-12
Forum 48 Advanced Technology Blade Testing on the XV-15 Tilt Rotor Research Aircraft Brent Wellman, NASA Ames Research Center

This paper was not submitted in time to be included in the printed Proceedings.
June 3, 1992 2012-05-12
Forum 48 Piloted Simulator Investigations Of A Civil Tilt-Rotor Aircraft On Steep Instrument Approaches William A. Decker, NASA Ames Research Center

This paper was not submitted in time to be included in the printed Proceedings.
June 3, 1992 2012-05-12
Forum 48 RAH - 66 Comanche Integrated Fire and Flight Control Development and Tests Donald W. Fowler and Nicholas D. Lappos, Sikorsky Aircraft Division United Technologies Corporation; James B. Dryfoos and James F. Keller, Boeing Defense and Space Group

This paper was not submitted in time to be included in the printed Proceedings.
June 3, 1992 2012-05-12
Forum 48 The Cabri Two Seat Helicopter - Design And First Flights Bruno Guimbal, EUROCOPTER

This paper was not submitted in time to be included in the printed Proceedings.
June 3, 1992 2012-05-12
Forum 48 Blade Twist - Design of Experiment P. Nick Fletcher, Bell Helicopter Textron, Inc.

This paper was not submitted in time to be included in the printed Proceedings.
June 3, 1992 2012-05-12
Forum 48 The V-22 for SOF Lt. Col. Thomas A. Swertfager, USAF; Stanley Martin Jr. and Ross D. Clark, Bell-Boeing

This paper was not submitted in time to be included in the printed Proceedings.
June 3, 1992 2012-05-12
Forum 48 V-22 Tiltrotor Flight Test Development Philip J. Dunford and Ken Lunn, Boeing Defense & Space Group; Ronald A. Magnuson and Roger L. Marr, Bell Helicopter Textron, Inc.

This paper was not submitted in time to be included in the printed Proceedings.
June 3, 1992 2012-05-12
Forum 49 Noise Certification of Bell Models 412, 230, and 206L-4 Helicopters Charles R. Cox; Suzanna S. Shank; Richard G. Riley Jr.; John T. Brieger; T. Ben Settle; Bell Helicopter Textron, Inc. May 19, 1993 2012-04-03
Forum 49 Noise Certification of Bell Models 412, 230, and 206L-4 Helicopters Charles R. Cox; Suzanna S. Shank; Richard G. Riley Jr.; John T. Brieger; T. Ben Settle; Bell Helicopter Textron, Inc. May 19, 1993 2019-29-10
Forum 49 Flight Measurements of Blade-Vortex Interaction Noise, Including Comparisons with Full Scale Wind Tunnel Data Gloria K. Yamauchi, David B. Signor, Michael E. Watts, Francisco J. Hernandez, NASA Ames Research Center; Philip LeMasurier, Sikorsky Aircraft Div, UTC May 19, 1993 2012-04-03
Forum 49 A Computational Study of the Aeroacoustics of Rotors in Hover James D. Baeder, Judith H. Gallman, Yung H. Yu, U.S. Army Aeroflightdynamics Directorate May 19, 1993 2012-04-03
Forum 49 The Importance of Tail Rotor Interaction as an Acoustic Source John W. Leverton, Westland Helicopters Inc. & Tony C. Pike, Westland Helicopters, Ltd. May 19, 1993 2012-04-03
Forum 49 Helicopter Main Rotor/Tail Rotor Noise Radiation Characteristics from Scaled Model Rotor Experiments in the DNW K-J Schultz and W.R. Splettstoesser, DLR Germany May 19, 1993 2012-04-03
Forum 49 Structural Integrity of Composite Flexbeams Anthony J. Vizzini, and Sung W. Lee, University of Maryland May 19, 1993 2012-04-03
Forum 49 Strength and Damage Tolerance Evaluation of Sandwich Structure Manufactured Utilizing the Automated Tow-Placement Process Steven G. Llorente; Russell Fay; Lee E. Kitson, Boeing Def & Space Group, Helicopter Division May 19, 1993 2012-04-03
Forum 49 Performance of Composite Joints Utilizing Thermoplastic Fasteners Adam J. Sawicki, Boeing Def & Space Group, Helicopter Division May 19, 1993 2012-04-03
Forum 49 Advanced Composite Main Rotor Flexbeam from Optimization to Full Scale Multicomponent and Whirl Tower Testing B.K. Hamilton; N.W. Bell; R.J. Murrill; S.E. Flores; L.A. Lucchetto, McDonnell Douglas Helicopter Company May 19, 1993 2012-04-03
Forum 49 Injection Molded NOTAR (R) Fan Blade for Helicopter Dynamic Application Steve Chen and Ramesh Patel, McDonnell Douglas Helicopter Company May 19, 1993 2012-04-03
Forum 49 Injection Molded NOTAR (R) Fan Blade for Helicopter Dynamic Application Steve Chen and Ramesh Patel, McDonnell Douglas Helicopter Company May 19, 1993 2021-01-01
Forum 49 Bearing Fatigue and Hole Elongation in Composite Bolted Joints Peter Grant, Nhien K. Nguyen & Adam J. Sawicki, Boeing Def & Space Group, Helicopters Division May 19, 1993 2012-04-03
Forum 49 Low Temperature Curing Adhesives for Repair Daniel Ruffner and Ramesh Patel, McDonnell Douglas Helicopter Company May 19, 1993 2022-29-04
Forum 49 Low Temperature Curing Adhesives for Repair Daniel Ruffner and Ramesh Patel, McDonnell Douglas Helicopter Company May 19, 1993 2012-04-03
Forum 49 Identification of UH-60 Stability Derivative Models in Hover from Flight Test Data Jay W. Fletcher, U.S. Army May 19, 1993 2012-04-03
Forum 49 V-22 Load Limiting Control Law Development David W. King and Charles Dabundo, Boeing Def & Space Group, Helicopter Division; Ronald L. Kisor and Ashok Agnihotri, Bell Helicopter Textron, Inc. May 19, 1993 2012-04-03
Forum 49 The European ACT Programme: A Collaborative Approach to Handling Qualities Evaluation and Control Law Design Malcolm Charlton, Defence Research Agency (U.K.); Catherine Guyomard, Eurocopter France; Robert Lane, Westland Helicopters; Heiner Modden, DLR Germany; Dieter Schimke, Eurocopter Deutschland; Armin Taghizad, ONERA France May 19, 1993 2012-04-03
Forum 49 Flight Evaluation of the New Handling Qualities Criteria Using the BO 105 Carl J. Ockier, Institute for Flight Mechanics, DLR May 19, 1993 2012-04-03
Forum 49 Flight Simulation Model Application for AH-64A Apache Engine Integration P. Shanthakumaran, J. Harding, T. Thompson, M. Kuehn and D. Monroe, McDonnell Douglas Helicopter Company May 19, 1993 2012-04-03
Forum 49 Helicopter Robust Nonlinear Controller Synthesis Using Approximate Linearization J. Leitner & J.V.R. Prasad, Georgia Institute of Technology May 19, 1993 2012-04-03
Forum 49 Active Man-Machine Interface for Advanced Rotorcraft Allen L. Zaklad, Monica Z. Weiland, Wayne W. Zachary, Clarence A. Fry, CHI Systems Inc.; James W. Voorhees, Advanced Simulation Engineering May 19, 1993 2012-04-03
Forum 49 Inadvertent Helicopter Air Bag Deployment--Evaluation of the Effects in a Flight Simulator Lindley W. Bark, Richard E. Zimmerman, Simula, Inc.; Kent F. Smith, U.S. Army ATCOM May 19, 1993 2016-16-12
Forum 49 Inadvertent Helicopter Air Bag Deployment--Evaluation of the Effects in a Flight Simulator Lindley W. Bark, Richard E. Zimmerman, Simula, Inc.; Kent F. Smith, U.S. Army ATCOM May 19, 1993 2012-04-03
Forum 49 Human Engineering Maintenance Analyses for the RAH-66 Comanche James F. Grenell & Elliot L. Wunsh, Boeing Def & Space Group, Helicopter Division May 19, 1993 2012-04-03
Forum 49 Human Engineering Maintenance Analyses for the RAH-66 Comanche James F. Grenell & Elliot L. Wunsh, Boeing Def & Space Group, Helicopter Division May 19, 1993 2020-26-06
Forum 49 Fluidic Backup Flight Control and Integrated Pump-Actuator for Advanced FBW Rotorcraft David Muggeridge, Allied-Signal Fluid Systems; John Day and John Berger, McDonnell Douglas Helicopter Company May 19, 1993 2012-04-03
Forum 49 Integrated Fire, Flight and Propulsion Controls (IFFC) for a Rotorcraft Weapon System Joan Edwards, Sikorsky Aircraft Div, UTC May 19, 1993 2012-04-03
Forum 49 Development of a Large AEW/Ground Target Radar for a Shipboard Compatible Tiltrotor Aircraft Richard R. Pruyn, Boeing Def & Space Group, Helicopter Division; Carl-Gilbert Lonroth, Ericsson Radar Electronics May 19, 1993 2012-04-03
Forum 49 An Aeroelastic Model Structure Investigation for a Manned Real-Time Rotorcraft Simulation William D. Lewis, LTC., U.S. Army AATD May 19, 1993 2012-04-03
Forum 49 Evaluation of Simulation Motion Fidelity Criteria in the Vertical and Directional Axes Jeffery A. Schroeder, NASA Ames Research Center May 19, 1993 2012-04-03
Forum 49 Application of Real-Time Flight Simulation for Design of a Helicopter Obstacle Avoidance System CPT Christopher C. Sullivan, U.S. Army; E. Roberts Wood, U.S. Naval Postgraduate School; Joe DeMaio, U.S. Army AFDD May 19, 1993 2012-04-03
Forum 49 Real-Time Implementation Aspects of a Rotorcraft Turbulence Simulation Method J.V.R. Prasad and Jamshed Riaz, Georgia Institute of Technology; Gopal H. Gaonkar and Dang Yingyi, Florida Atlantic University May 19, 1993 2012-04-03
Forum 49 Civil Tiltrotor: Flight Simulation Development of Instrument Procedures Peter D. Klein, Bell Helicopter Textron, Inc.; Paul R. Wilkinson and Leon A. Zmroczek, Boeing Def & Space Group, Helicopter Division May 19, 1993 2012-04-03
Forum 49 System Identification Validation of an AH-64 Aeroelastic Simulation Model Selwyn H. Sturisky and Daniel P. Schrage, Georgia Institute of Technology May 19, 1993 2012-04-03
Forum 49 Fabrication of the NOTAR ? Tailboom for the MD Explorer Pierre H. Jouin, Richard L. Kulesha & Guy R. Schindler, McDonnell Douglas Helicopter Company May 19, 1993 2012-04-03
Forum 49 Cost-Effective Production of Helicopter Energy-Absorbing Subfloor Structures with Advanced Thermoplastic Composites Lindley W. Bark & Gershon Yaniv, Simula, Inc.; Drew G. Orlino, U.S. Army Aviation Applied Technology Directorate May 19, 1993 2012-04-03
Forum 49 Experiments and Modeling of Residual Deformations in the Manufacturing of Sandwich and Laminated Composite Structures Paul Handel & Pierre J.A. Minguet, Boeing Def & Space Group, Helicopter Division May 19, 1993 2012-04-03
Forum 49 Laser Based Alignment, Advanced Manufacturing Techniques Gary Confalone, Sikorsky Aircraft Div., UTC (INSERT) May 19, 1993 2012-04-03
Forum 49 Understanding Heat Treat Distortion Mary L. Parke, AlliedSignal Aerospace Propulsion Engines; Peter D. Hilton and Richard Stringfellow, Arthur D. Little, Inc. May 19, 1993 2012-04-03
Forum 49 Experimental Design Application: Udimet 720 Broaching Optimization Diane Nowatney, AlliedSignal Aerospace Propulsion Engines May 19, 1993 2012-04-03
Forum 49 The Application of Computational Vorticity Confinement to Helicopter Rotor and Body Flows Clin M. Wang and John O. Bridgeman, Flow Analysis, Inc.; John S. Steinhoff and Yonghu Wenren, University of Tennessee Space Institute & Flow Analysis, Inc. May 19, 1993 2012-04-03
Forum 49 The Application of Vorticity Embedding to the Computation of Advancing Rotor Flows K. Ramachandran, Flow Analysis Inc.; S. Schlechtriem, RWTH University of Aaachen; F.X. Caradonna, U.S. Army ATCOM; John S. Steinhoff, University of Tennessee Space Institute and Flow Analysis, Inc. May 19, 1993 2012-04-03
Forum 49 Vorticity Concentration at the Edge of the Inboard Vortex Sheet Jaimoo Kim, Narayanan M. Komerath and Shiuh-Guang Liou, Georgia Institute of Technology May 19, 1993 2012-04-03
Forum 49 A Consistent Approach for Modeling the Aerodynamics of Self-Generated Rotor Blade-Vortex Interactions Ahmad A. Hassan, Bruce D. Charles, Hormoz Tadghighi, McDonnell Douglas Helicopter Company; Casey Burley, NASA Langley Research Center May 19, 1993 2012-04-03
Forum 49 A Fast Adaptive Resolution Method for Efficient Free Wake Calculations Wayne O. Miller, National Research Council May 19, 1993 2012-04-03
Forum 49 Unsteady Compressible Rotor Airfoil Aerodynamics Using an Automated Adaptive Finite Element Method Bruce E. Webster, Mark S. Shephard, Zvi Rusak, Rensselaer Polytechnic Institute May 19, 1993 2012-04-03
Forum 49 Dynamic Stall Correlation of a Rotor/Wing Navier-Stokes Solver on a Massively-Parallel Computer Brian E. Wake, Peter F. Lorber, United Technologies Research Center May 19, 1993 2012-04-03
Forum 49 Scenario Analysis of VTOL Vehicles Using an Interactive Environment (SAVVIE) LTC Terry S. Turpin, U.S. Army ATCOM; Russell Ure, CAE Electronics Ltd. May 19, 1993 2016-29-01
Forum 49 Scenario Analysis of VTOL Vehicles Using an Interactive Environment (SAVVIE) LTC Terry S. Turpin, U.S. Army ATCOM; Russell Ure, CAE Electronics Ltd. May 19, 1993 2012-04-03
Forum 49 Apache Modernization - The User's Perspective COL Dave Sale and CPT Gregory J. Lund, U.S. Army TRADOC May 19, 1993 2012-04-03
Forum 49 Shipboard Suitability and the UAV Bob Scholes, Bell Helicopter Textron, Inc. May 19, 1993 2012-04-03
Forum 49 Development of a Realistic Combat Environment for Operational Testing CW4 Larry E. Weidell, U.S. Army May 19, 1993 2012-04-03
Forum 49 The OH-58D Kiowa Warrior: The Spirit of the Cavalry and The Enemy's Worst Nightmare COL Ted D. Cordrey and CPT Robert M. (Mike) Cumbie, U.S. Army May 19, 1993 2017-21-11
Forum 49 The OH-58D Kiowa Warrior: The Spirit of the Cavalry and The Enemy's Worst Nightmare COL Ted D. Cordrey and CPT Robert M. (Mike) Cumbie, U.S. Army May 19, 1993 2012-04-03
Forum 49 V-22 Osprey Survivability Tradeoff Studies Barbara T. Hegdahl, Bell Helicopter Textron, Inc. May 19, 1993 2012-04-03
Forum 49 Naval Rotorcraft Water Impact Crash Simulation Using Program KRASH Gil Wittlin, Dynamic Response, Inc.; Martin B. Rapaport, Naval Air Warfare Center May 19, 1993 2012-04-03
Forum 49 Procedures Used to Ensure Strength, Endurance and Damage Tolerance of Mil Helicopter Fuselages (Mi-26, Mi-28, etc.) Z. E. Shnurov, Mil Moscow Helicopter Plant May 19, 1993 2012-04-03
Forum 49 Advanced Aluminum Alloys for Improved Rotorcraft Reliability Gerard J. Nanni, Bell Helicopter Textron, Inc. May 19, 1993 2012-04-03
Forum 49 Flight Service Evaluation of Composite Components on the Bell Model 206L Helicopter Scott Smith, ICAD; Henry Wilson, Bell Helicopter Textron, Inc. May 19, 1993 2012-04-03
Forum 49 Systematic Application of Holometric Synthesis for Cost-Effective Helicopter Flight Load Monitoring Bruce Gustavson and W. Lee Pellum, Kaman Aerospace Corp.; Eric Robeson, U.S. Army AATD May 19, 1993 2012-04-03
Forum 49 Development of a Crashworthy Crewseat for the Kaman K-1200 Helicopter Marvin K. Richards, Simula, Inc. May 19, 1993 2012-04-03
Forum 49 Flow Reduction Efforts Benefit from Computer Simulation Sybil Jane Cooper, Sikorsky Aircraft Div, UTC May 19, 1993 2012-04-03
Forum 49 Rapid Prototyping for the Development of Gas Turbine Engines Michael Hyduke and Rey Chu, AlliedSignal Propulsion Engines May 19, 1993 2012-04-03
Forum 49 Automated Harness Design and Process Planning George P. Geanuracos and Jeanette Hollis, Sikorsky Aircraft Div, UTC May 19, 1993 2012-04-03
Forum 49 Small Diameter Wire Marking for Light Weight Electrical Interconnections Systems Lou Marchitto, Mark Rowland, Sikorsky Aircraft Div, UTC May 19, 1993 2018-23-04
Forum 49 Small Diameter Wire Marking for Light Weight Electrical Interconnections Systems Lou Marchitto, Mark Rowland, Sikorsky Aircraft Div, UTC May 19, 1993 2012-04-03
Forum 49 Integration of Avionics Troubleshooting System with Interactive Electronic Technical Manuals Joseph G. Gulick and Edward T. Kelt, Sikorsky Aircraft Div, UTC May 19, 1993 2012-04-03
Forum 49 The Design Evolution of the Canard Rotor-Wing John W. Rutherford and Steven M. Bass, McDonnell Douglas Helicopter Co. May 19, 1993 2012-04-03
Forum 49 Advanced Civil Tiltrotor Design Optimization and Issues David R. Schleicher, NASA Ames Research Center May 19, 1993 2012-04-03
Forum 49 Some European Considerations on Civil Tilt-rotor Efficiency and Viability J. Renaud and J.C. Weisse, Eurocopter France; B. AIlard, Eurocopter International; W. Muggli, Eurocopter Deutschland; D. Ingram, Westland Helicopters, Ltd. May 19, 1993 2012-04-03
Forum 49 Analysis of Helicopter Air-to-Air Combat Tests, Design Implications Kenneth B. Amer, RAND Corporation May 19, 1993 2012-04-03
Forum 49 Variable Design Criteria for Rotary Wing Aircraft Crash Resistance LeRoy T. Burrows, U.S. Army AATD May 19, 1993 2012-04-03
Forum 49 The EH101 Helicopter: A Review of its Capabilities and Technology Christopher J. Battison, Westland Helicopters, Ltd May 19, 1993 2012-04-03
Forum 49 The Tilt Wing Design for a Family of High Speed V/STOL Aircraft William F. Chana and T.M. Sullivan, William F. Chana Associates, Inc. May 19, 1993 2012-04-03
Forum 49 Stability of the Sikorsky S-76 Bearingless Main Rotor James M. Wang, James Duh, Jon-Shen Fuh, Sikorsky Aircraft Div, UTC; Sesi Kottapalli, NASA Ames Research Center May 19, 1993 2012-04-03
Forum 49 Correlation of Experimental Flap-Lag-Torsion Damping - A Case Study Donizeti de Andrade, Instituto Tecnologico de Aeronautica (Brazil); David A. Peters, Washington University May 19, 1993 2012-04-03
Forum 49 Experimental Investigation of Main Rotor Wake Induced Empennage Vibratory Airloads for the RAH-66 Comanche Helicopter Kirk C. Frederickson and J. Richard Lamb, Sikorsky Aircraft Div, UTC May 19, 1993 2012-04-03
Forum 49 Ground Vibrations Tests for the High Speed Dolphin Helicopter Laurent Girard, Eurocopter France; Pascal Lubrina, ONERA May 19, 1993 2012-04-03
Forum 49 Full-Scale Higher Harmonic Control Research to Reduce Hub Loads and Noise Sesi Kottapalli, NASA Ames Research Center; Stephen Swanson, Sterling Federal Systems; Philip LeMasurier and James Wang, Sikorsky Aircraft Div, UTC May 19, 1993 2012-04-03
Forum 49 Dynamics of a Rotor with Nonharmonic Control Friedrich K. Straub and Lawson H. Robinson, McDonnell Douglas Helicopter Company May 19, 1993 2012-04-03
Forum 49 The Practical Implementation of an Actively Controlled Flap to Reduce Vibrations in Helicopter Rotors Thomas A. Millott and Peretz P. Friedmann, University of California at Los Angeles May 19, 1993 2012-04-03
Forum 49 Laser Velocimetry and Blade Pressure Measurements of a Blade-Vortex Interaction Susan Althoff Gorton, U.S. Army ATCOM; David R. Poling and Leo Dadone, Boeing Defense & Space Group, Helicopter Division May 19, 1993 2012-04-03
Forum 49 Investigation of Empennage Airloads Induced by a Helicopter Main Rotor Wake Michael S. Torok and Donald T. Ream, Sikorsky Aircraft Div, UTC May 19, 1993 2012-04-03
Forum 49 High Lift Concepts for Rotorcraft Applications Yung H. Yu, Soogab Lee, Kenneth W. McAlister and Chee Tung U.S. Army Aeroflightdynamics Directorate; Clin M. Wang, Georgia Institute of Technology May 19, 1993 2012-04-03
Forum 49 V-22 Flight Test Aerodynamic Refinements Michael C. Savage, Boeing Def & Space Group, Helicopter Div; Michael K. Farrell, Bell Helicopter Textron, Inc.; William K. Grauer & Michael A. McVeigh, Boeing Def & Space Group, Helicopter Division May 19, 1993 2012-04-03
Forum 49 Reduction of Tiltrotor Download T.L. Wood and M.A.. Peryea, Bell Helicopter Textron, Inc. May 19, 1993 2012-04-03
Forum 49 Detailed Aerodynamic Design of the RAH-66 FANTAIL Using CFD R. Ganesh Rajagopalan, Iowa State University; Charles N. Keys, Boeing Def & Space Group, Helicopter Div May 19, 1993 2012-04-03
Forum 49 Integration of Publications, Training, and LSA to Support a Mature Fleet Martin F. Anderson, III Boeing Def & Space Group, Helicopter Division May 19, 1993 2012-04-03
Forum 49 Changing Role of the Contractor Field Technical Representatives Vincent A. Parziale, GE Aircraft Engines May 19, 1993 2012-04-03
Forum 49 Supporting Mature Aircraft in a Decreasing Budget Environment Anthony M. Conti, Richard J. Crann and David M. Gearhart, Sikorsky Aircraft Div, UTC May 19, 1993 2012-04-03
Forum 49 Smoothing the CH-47D with the OBSERVE, an On Board Vibration Analyzer, Tracker, and Balancer Sam T. Crews and Valentin C. Berger, U.S. Army ATCOM May 19, 1993 2012-04-03
Forum 49 Correlation of the Lynx-XZ170 Flight-Test Results Up to and Beyond the Stall Boundary Benton H. Lau, NASA Ames Research Center; Alexander W. Louie, Sterling Software; Costantinos P. Sotiriou and Nicholas Griffiths, Westland Helicopters, Ltd. May 19, 1993 2012-04-03
Forum 49 High-Speed Tiltrotors: Dynamics Methodology Michael J. Moore, Michael J. Yablonski, Bobby Mathew and John Liu, Boeing Defense & Space Group, Helicopter Division May 19, 1993 2012-04-03
Forum 49 Bearingless Main Rotor Whirl Test: Design, Analysis and Test Results R.J. Murrill, B. Hamilton, V. Anand, D. Lauzon & B. Tuttle, McDonnell Douglas Helicopter Company May 19, 1993 2012-04-03
Forum 49 Aeroelastic Stability of the McDonnell Douglas Advanced Bearingless Rotor Khanh Nguyen, NASA Ames Research Center; Michael McNulty, Vaidyanathan Anand and Dan Lauzon, McDonnell Douglas Helicopter Company May 19, 1993 2012-04-03
Forum 49 Measurements of Unsteady Pressure on a Pitching Rotor Blade Mihir Kumar Lal, S.G. Liou, G Alvin Pierce & N.M. Komerath, Georgia Institute of Technology May 19, 1993 2012-04-03
Forum 49 Wind Tunnel Modeling of High Order Rotor Vibration James A. Staley, M. Bobby Mathew & Frank J. Tarzanin Jr., Boeing Defense & Space Group, Helicopter Division May 19, 1993 2012-04-03
Forum 49 A Feasibility Study of Using Smart Materials for Rotor Control Friedrich K. Straub, McDonnell Douglas Helicopter Co. May 19, 1993 2012-04-03
Forum 49 Aeroelastic Optimization of a Helicopter Rotor with Composite Tailoring Ranjan Ganguli and Inderjit Chopra, University of Maryland May 19, 1993 2012-04-03
Forum 49 The Combat Suitability Filter for the VECTR Project (The Culmination of the Concept Analysis Process) John M. Davis, US Army Aviation & Troop Command May 19, 1993 2012-04-03
Forum 49 Material Applications to a Light Helicopter Rodney Taylor, Ken Nunn and Charles Rogers, Bell Helicopter Textron, Inc. May 19, 1993 2012-04-03
Forum 49 Downwash Design Criteria for VTOL Aircraft