Results cover extensive range of sweepback angle, Mach number, aspect ratio, and thickness ratio; results for total wave drag are applicable both to sweptback and sweptforward wings.
Theoretical supersonic wave drag of untapered sweptback and rectangular wings at zero lift
Nat Advisory Committee Aeronautics -- Tech Note
1947
43 pages
Report
English
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Supersonic wave drag of sweptback tapered wings at zero lift
Engineering Index Backfile | 1947
|Engineering Index Backfile | 1953
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