Reference to previous drag studies involving superimposed or " combined" flow field; method for determining mathematically combined disturbances field, and in certain cases minimum drag, of wings at supersonic speeds; example is provided by wing of elliptic plan form, which achieves minimum drag when lift is distributed uniformly over surface.
Theoretical determination of minimum drag of airfoils at supersonic speeds
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 19 , n 12
1952
10 pages
Aufsatz (Zeitschrift)
Englisch
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