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Flugmechanik
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keywords:("Flugmechanik")
Method of computing subsonic flows around given airfoils
Pressure distribution and some effects of viscosity on slender inclined bodies of revolution
Some studies on flow of gas in region of transition through velocity of Sound
Results of recent hypersonic and unsteady flow research at Langley Aeronautical Laboratory
Results of recent hypersonic and unsteady flow research at Langley Aeronautical Laboratory
Calculation of downwash behind wings of arbitrary plan form at supersonic speeds
Theoretical investigation of transonic similarity for bodies of revolution
Calculation of transonic flows past thin airfoils by integral method
Charts for estimating downwash behind rectangular, trapezoidal, and triangular wings at supersonic
Gas kinetics of very high flight speeds
Calculation of compressible potential flow past slender bodies of revolution by integral method
First-order theory for unsteady motion of thin wings at supersonic speeds
Supersonic flow around circular cones at angles of attack
Analytical study of spheric representation of flight
Application of Mathieu functions in theory of subsonic compressible flow past oscillating airfoils
Similarity laws for transonic flow about wings of finite span
Method for calculating downwash field due to lifting surfaces at subsonic and supersonic speeds
Two-dimensional transonic flow past airfoils
Inviscid flow about airfoils at high supersonic speeds
On calculation of flow about objects traveling at high supersonic speeds
Experiments on transonic flow around wedges
Theoretical study of transonic lift of double-wedge profile with detached bow wave
Theoretical study of transonic lift of double-wedge profile with detached bow wave
On application of transonic similarity rules
Study of second-order supersonic flow theory
Characteristics of Propellers for Turboprop Airplanes
Supersonic flow past oscillating airfoils including nonlinear thickness effects
Elements of propeller and helicopter aerodynamics
On application of transonic similarity rules to wings of finite span
Study of inviscid flow about airfoils at high supersonic speeds
Effect of Aerodynamic Heating on Fuel Systems