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Flugmechanik
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keywords:("Flugmechanik")
Investigations of pressure distribution on fast flying bodies
Free-Spinning-Tunnel Tests of a 1/20-Scale Model of the Northrop N-9M Airplane
A Systematic Approach to Aerodynamic Design of Radial Engine Installations
Correlation Tests of the Ditching Behavior of an Army B-24D Airplane and a 1/16-size Model
Influence of jet of propulsion unit on nearby wings
Wind-Tunnel Investigation of the Stability of the Jettisonable Nose Section of the X-3 Airplane
A Method of Ground Resonance Testing for Helicopters
DESIGN AND TEST EXPERIENCE WITH MONOCOQUE MAGNESIUM WINGS
HEAT RECOVERY - Applied to Heating and Anti-Icing of Aircraft
GERMAN DEVELOPMENTS in the FIELD of GUIDED MISSILES
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
High-Speed Wind-Tunnel Tests of a Twin-Fuselage Pursuit Airplane
Analysis of Effect of Rolling Pull-Outs on Wing and Aileron Loads of a Fighter Airplane
Characteristics of a Configuration with a Large Angle of Sweepback
A Comparison of the Lateral Motion Calculated for Tailless and Conventional Airplanes
Wing pressure-distribution measurements up to 0,866 Mach number in flight on jet-propelled airplane
Flight Tests of Rocket-Powered "Tin-Can" Models of AAF Project MX-800
Tunnel correction for compressible subsonic flow
Wind-Tunnel Tests at Low Speed of Swept and Yawed Wings Having Various Plan Forms
Prediction of the aerodynamic characteristics of wings of arbitrary plan form
Russian Laminar Flow Airfoils 3rd Part: Measurements on the Profile No. 2315 BIS with Ava-Nose Flap