Analysis of low aspect ratio triangular wings given in Tech Note n 1423 (see Engineering Index 1947 p 55) is extended to apply to triangular wings having large vertex angles. (15¢) (published 1950)
Stability derivatives of triangular wings at supersonic speeds
Nat Advisory Committee Aeronautics -- Reports
1948
9 pages
Report
English
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Stability derivatives of triangular wings at supersonic speeds
Engineering Index Backfile | 1948
|Stability derivatives of low-aspect-ratio triangular wings at subsonic and supersonic speeds
Engineering Index Backfile | 1947
|