Results of sweptback wing tests compared with triangular wing results for Mach number of 1.43 show same trends of lift and drag as sweep angle is changed.
Preliminary investigation at supersonic speeds of triangular and sweptback wings
Nat Advisory Committee Aeronautics -- Tech Note
1949
37 pages
Illus, Diagrs, Charts
Report
Englisch
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Stability derivatives of triangular wings at supersonic speeds
TIBKAT | 1948
|Stability derivatives of triangular wings at supersonic speeds
Engineering Index Backfile | 1948
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