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Theory of Helicopter Damping in Pitch or Roll and a Comparison With Flight Measurements
Landing Characteristics of Fighter Aircraft with Asymmetric Tip Tank Loading
Aerodynamic Performance and Stability Coefficients for the XSM-65A Missile
Ws-117LSUBSYSTEM a Engineering Analysis Report. Volume I. Program I
Evaluation of the Sikorsky 'Swastika' Dynamic Vibration Absorber in the H-37A
Free-Spinning Characteristics of a 1/30-Scale Model of the Grumman WF-2 Airplane
Free-Flight Investigation of Radio Controlled Models with Parawings
An Approach to the Control of Statically Unstable Manned Flight Vehicles
Rapid-Transition Tests of a 1/4-Scale Model of the VZ-2 Tilt-Wing Aircraft
Lateral Vibrations of an Aircraft, Caused by Effect of Wind Gusts
Spin Tunnel Investigation of a 1/30 Scale Model of the North American A-5A Airplane