Forum 23 - Washington, D.C. 1967
AHS Forum 23
May 10-12, 1967
Washington, D.C. USA
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Determination of Helicopter Rotor Blade Compressibility Effects-Prediction Vs. Flight Test Regular Price: $30.00 Member price: $15.00
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Aerodynamic Considerations of Stopping a Rotor in Flight Regular Price: $30.00 Member price: $15.00
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Avionics for the Light Observation Helicopter Regular Price: $30.00 Member price: $15.00
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Evaluation of Two Instrument-Landing Displays in Simulated IFR Approaches with a Helicopter Regular Price: $30.00 Member price: $15.00
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Electrostatic Discharging Systems for Helicopters - A Review of the State of the Art Regular Price: $30.00 Member price: $15.00
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The Effects of Flight Dynamics on Rotor Blade Antenna Performance Regular Price: $30.00 Member price: $15.00
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Emergency Lift and Autorotational Boost Systems for Single Engine Helicopters Regular Price: $30.00 Member price: $15.00
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Bending Strength of Spur Gear Teeth Regular Price: $30.00 Member price: $15.00
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Increased Helicopter Capability Through Advanced Powerplant Technology Regular Price: $30.00 Member price: $15.00
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Structural Development the of XV-9A Hot Cycle Research Aircraft Regular Price: $30.00 Member price: $15.00
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A Comparison of Fatigue Life and Reliability from Constant and Variable Amplitude Loading Test Regular Price: $30.00 Member price: $15.00
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Helicopter Cargo Restraint Regular Price: $30.00 Member price: $15.00
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The Army CH-54A in RVN, HLH on the Move Regular Price: $30.00 Member price: $15.00
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Optimum Use of Contingency Power Rating for Increasing Permissible Operating Gross Weight in Twin-Turbine Helicopters Regular Price: $30.00 Member price: $15.00
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Suppression of Transmitted Harmonic Rotor Loads by Blade Pitch Control Regular Price: $30.00 Member price: $15.00
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An Analysis of the Stall Flutter Instability of Helicopter Rotor Blades Regular Price: $30.00 Member price: $15.00
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The Influence of Blade Flapping Restraint on the Dynamic Stability of Low Disk Loading Propeller-Rotor Regular Price: $30.00 Member price: $15.00
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Control Loads and Their Effects on Fuselage Vibrations Regular Price: $30.00 Member price: $15.00
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Response Characteristics of the Gyro-Controlled Lockheed Rotor System Regular Price: $30.00 Member price: $15.00
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AAFSS (AH-56A) Application Of A Fully Integrated Avionics Aircrafts Weapons System Regular Price: $30.00 Member price: $15.00
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Stall Flutter of Helicopter Rotor Blades : A Special Case of the Dynamic Stall Phenomenon Regular Price: $30.00 Member price: $15.00
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Comments on "Effects of Control Loads on Fuselage Vibration by D. Kidd, R. Spivey, K. Lawrence" Regular Price: $30.00 Member price: $15.00
