Variations in drag with taper ratio, aspect ratio, sweepback, and Mach number are determined; calculations are presented for families of tapered wings having equal root bending stress.
Supersonic wave drag of sweptback tapered wings at zero lift
Nat Advisory Committee Aeronautics -- Tech Note
1947
49 pages
Report
Englisch
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Theoretical supersonic wave drag of untapered sweptback and rectangular wings at zero lift
Engineering Index Backfile | 1947
|Engineering Index Backfile | 1948
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