Analysis of derivatives of low-aspect-ratio wings at subsonic and supersonic speeds, given in NACA TN n 1423 (see Engineering Index1947 p 55), is extended to apply to triangular wings having large vertex angles and traveling at supersonic speeds.
Stability derivatives of triangular wings at supersonic speeds
Nat Advisory Committee Aeronautics -- Tech Note
1948
20 pages
Report
English
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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
|Stability derivatives of low-aspect-ratio triangular wings at subsonic and supersonic speeds
Engineering Index Backfile | 1947
|