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Flugmechanik
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Wind-Tunnel Investigation of an NACA 23021 Airfoil with a 0.32-Airfoil- Chord Double Slotted Flap
Effect of Compressibility on Pressure Distribution over an Airfoil with a Slotted Frise Aileron
Profile-Drag Coefficients of Conventional and Low-Drag Airfoils as Obtained in Flight
High-Speed Wind-Tunnel Tests of a 0.3-Scale Model of the P-47D Airplane
Compressibility barrier to supersonic speeds
Computation of compressibility effect on flight envelope
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
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