AHS International -- The Vertical Flight Society

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Forum 57 - Best Papers Nominees

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Acoustics Helicopter Cabin Noise Reduction Using Active Structural Acoustic Control
James O'Connell, Gopal Mathur, Ram JanakiRam - The Boeing Company; Marty Johnson, Virginia Tech; Dino J. Rossetti, Lord Corporation

Aerodynamics and Aeroacoustics Tiltrotor Descent Aerodynamics: A Small-Scale Experimental Investigation of Vortex Ring State
Mark D. Betzina, NASA Ames Research Center

Aircraft Design Design And Development of A Four-Bladed Tail Rotor System For The USMC H-1 Upgrade Program
Ajay Sehgal, Eric Boyle; Bell Helicopter Textron, Inc.

Avionics and Systems Cockpit and Mission System Modernization
Don Anttila, Kyle DeLong, Mike Skaggs, Sikorsky Aircraft; Scott White, Rockwell Collins

Crash Safety Analysis and Design of Dynamically Loaded Fittings
Rodney H. Jones, J. Donn Hethcock, B. R. Mullins, Bell Helicopter Textron, Inc.

Crew Stations & Human Factors Engineering How Do Helicopter Pilots Know When to Stop, Turn or Pull Up? (Developing guidelines for vision aids)
Gareth D Padfield, The University of Liverpool; David N Lee, University of Edinburgh; Roy Bradley, Glasgow Caledonian University

Dynamics Vibratory Loads Reduction Testing of The Nasa/Army/MIT Active Twist Rotor
Matthew L. Wilbur, Paul H. Mirick, William T. Yeager, Jr., Chester W. Langston, NASA Langley Research Center; Carlos E. S. Cesnik, SangJoon Shin, Massachusetts Institute of Technology

Flight Simulation New Developments In Dynamic Wake Modeling For Dynamics Applications
David A. Peters, Jorge A. Morillo, Adria M. Nelson, Washington University in St. Louis

Handling Qualities Experimental Evaluation of Flight Control System Designs Exploiting Rotor State Feedback
J. Howitt, S.E. Howell, A.T. McCallum, Defence Evaluation Research Agency; P.R. Brinson, Agusta-Westland Helicopters

HUMS Planetary Gear Box Diagnostics Using Adaptive Vibration Signal Representations: A Proposed Methodology
Paul Samuel, Darryll Pines, University f Maryland

IMPACT RWSTD Airframe Technology - Foundation For The 21St Century
Bruce F. Kay, Sikorsky Aircraft Corporation

Lichten Award Presentation Tiltrotor Blade-Vortex Interaction (BVI) Noise Control Through Non-Unique Longitudinal Force Trim
Marc Gervais, University of Maryland

Military Operations Advanced Tactical Combat Model (ATCOM) Team Behavior Modeling of the Apache Longbow
Bill Baker, The Boeing Company

Product Support TBD
Propulsion Analysis Methods to Control Performance Variability and Costs in Aircraft Turbine Engine Manufacturing
K. E. Sheldon, C. M. Anderson-Cook, W.F. O'Brien, Virginia Polytechnic Institute and State University

Structures and Materials Bird Strike Analysis and Test of a Spinning S-92 Tail Rotor
Alan Dobyns, Frank Federici, Robert Young , Sikorsky Aircraft Corporation

STOVL Technology The Vectored Slipstream Propfan has the Potential for Being the Best Approach for Large VSTOL Transports
Kenneth G. Wernicke, Sky Technology Vehicle Design & Development Co.

Test and Evaluation An Analytical Methodology For Category A Performance Prediction And Extrapolation
Eric Bernard Carlson, Bell Helicopter Textron, Inc.

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Acoustics	Helicopter Cabin Noise Reduction Using Active Structural Acoustic Control James O'Connell, Gopal Mathur, Ram JanakiRam - The Boeing Company; Marty Johnson, Virginia Tech; Dino J. Rossetti, Lord Corporation
Aerodynamics and Aeroacoustics	Tiltrotor Descent Aerodynamics: A Small-Scale Experimental Investigation of Vortex Ring State Mark D. Betzina, NASA Ames Research Center
Aircraft Design	Design And Development of A Four-Bladed Tail Rotor System For The USMC H-1 Upgrade Program Ajay Sehgal, Eric Boyle; Bell Helicopter Textron, Inc.
Avionics and Systems	Cockpit and Mission System Modernization Don Anttila, Kyle DeLong, Mike Skaggs, Sikorsky Aircraft; Scott White, Rockwell Collins
Crash Safety	Analysis and Design of Dynamically Loaded Fittings Rodney H. Jones, J. Donn Hethcock, B. R. Mullins, Bell Helicopter Textron, Inc.
Crew Stations & Human Factors Engineering	How Do Helicopter Pilots Know When to Stop, Turn or Pull Up? (Developing guidelines for vision aids) Gareth D Padfield, The University of Liverpool; David N Lee, University of Edinburgh; Roy Bradley, Glasgow Caledonian University
Dynamics	Vibratory Loads Reduction Testing of The Nasa/Army/MIT Active Twist Rotor Matthew L. Wilbur, Paul H. Mirick, William T. Yeager, Jr., Chester W. Langston, NASA Langley Research Center; Carlos E. S. Cesnik, SangJoon Shin, Massachusetts Institute of Technology
Flight Simulation	New Developments In Dynamic Wake Modeling For Dynamics Applications David A. Peters, Jorge A. Morillo, Adria M. Nelson, Washington University in St. Louis
Handling Qualities	Experimental Evaluation of Flight Control System Designs Exploiting Rotor State Feedback J. Howitt, S.E. Howell, A.T. McCallum, Defence Evaluation Research Agency; P.R. Brinson, Agusta-Westland Helicopters
HUMS	Planetary Gear Box Diagnostics Using Adaptive Vibration Signal Representations: A Proposed Methodology Paul Samuel, Darryll Pines, University f Maryland
IMPACT	RWSTD Airframe Technology - Foundation For The 21St Century Bruce F. Kay, Sikorsky Aircraft Corporation
Lichten Award Presentation	Tiltrotor Blade-Vortex Interaction (BVI) Noise Control Through Non-Unique Longitudinal Force Trim Marc Gervais, University of Maryland
Military Operations	Advanced Tactical Combat Model (ATCOM) Team Behavior Modeling of the Apache Longbow Bill Baker, The Boeing Company
Product Support	TBD
Propulsion	Analysis Methods to Control Performance Variability and Costs in Aircraft Turbine Engine Manufacturing K. E. Sheldon, C. M. Anderson-Cook, W.F. O'Brien, Virginia Polytechnic Institute and State University
Structures and Materials	Bird Strike Analysis and Test of a Spinning S-92 Tail Rotor Alan Dobyns, Frank Federici, Robert Young , Sikorsky Aircraft Corporation
STOVL Technology	The Vectored Slipstream Propfan has the Potential for Being the Best Approach for Large VSTOL Transports Kenneth G. Wernicke, Sky Technology Vehicle Design & Development Co.
Test and Evaluation	An Analytical Methodology For Category A Performance Prediction And Extrapolation Eric Bernard Carlson, Bell Helicopter Textron, Inc.