Using the results of earlier investigations, a method for determination of the velocity or pressure distribution and the aerodynamic properties of a low-aspect-ratio swept wing with slender body of elliptical cross-section and vertical tail surface, having arbtrary form, is briefly presented. The method can be used for the prediction of the load distribution, aerodynamic forces and moments on inclined slender wing, body and vertical tail combinations travelling at subsonic or supersonic speeds.
Pressure Distribution and Aerodynamic Properties of High-Speed Aircraft
A Method for Determining the Main Aerodynamic Properties of High-Speed Aeroplanes
Aircraft Engineering and Aerospace Technology ; 28 , 8 ; 259-261
1956-08-01
3 pages
Article (Journal)
Electronic Resource
English
THE AERODYNAMIC AND POWER PLANT HEATING PROBLEM IN HIGH SPEED AIRCRAFT
SAE Technical Papers | 1954
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