Experimental data have shown that decrease in aspect ratio of wing decreases adverse effects of compressibility on wing; approximate method by which quantitative effect of variation of aspect ratio can be predicted.
Aspect ratio influence at high subsonic speeds
J. Aeronautical Sciences
Journal of the Aeronautical Sciences ; 23 , n 9
1956
5 pages
Article (Journal)
English
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Stability derivatives of low-aspect-ratio triangular wings at subsonic and supersonic speeds
Engineering Index Backfile | 1947
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