Problem of reducing drag due to lift of wing alone to its minimum value for given lift; minimum drag must be obtained by distributing total lift in most appropriate way over surface of wing; how general criterion may be employed to determine both lift distribution for minimum drag and actual shape of lifting surface.
Wings with minimum drag due to lift in supersonic flow
J Aero/Space Sciences
Journal of Aerospace Science ; 27 , n 1
1960
Aufsatz (Zeitschrift)
Englisch
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