On basis of recently developed theory for finite sweptback wings at supersonic speeds, calculations of supersonic wave drag at zero lift were made for series of wings having thin symmetrical biconvex sections with untapered plan forms and various angles of sweepback and aspect ratios.
Calculations of supersonic wave drag of nonlifting wings with arbitrary sweepback and aspect ratio wings swept behind Mach lines
Nat Advisory Committee Aeronautics -- Tech Note
1947
34 pages
6 Supp Plates
Report
English
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