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Flugmechanik
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Effects of compressibility and large angles of yaw on pressure indicated by total-pressure tube
Summary of Drag Results from Recent Langley Full-Scale-Tunnel Tests of Army and Navy Airplanes
Rolling Moment Due to Sideslip. Part 1. The Effect of Dihedral
Analysis of the effect of rolling pull-outs on the wing and aileron loads of a fighter airplane
Effect of Wing Modifications on the Longitudinal Stability of a Tailless All-Wing Airplane Model
Wind-Tunnel Tests of a Portion of a PV-2 Helicopter Rotor Blade
Effect of compressibility at high subsonic velocities on lifting force acting on elliptic cylinder
Investigations of pressure distribution on fast flying bodies
Influence of jet of propulsion unit on nearby wings
Influence of Large Amounts of Wing Sweep on Stability and Control Problems of Aircraft
Supperssion of Image Movement in Air Photography
Tables for Use in the Investigation of Supersonic Fields of Flow by the Method of Characteristics
Effect of Mach and Reynolds Numbers on Maximum Lift Coefficient
Toward New Horizons. Volume 4. Aerodynamics and Aircraft Design
Use of Rocket-Propelled Flying Models for Experiments at Transonic Speeds