Developments in high speed aircraft and missiles have resulted in trend toward using thin airfoils of short span, making it necessary to obtain reasonable predictions for aerodynamic load in tip region and at moderate angle of attack; theoretical investigation on simplified model. Bibliography.
Aerodynamics of rectangular plate with vortex separation in supersonic flow
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 22 , n 4
1955
10 pages
Aufsatz (Zeitschrift)
Englisch
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