Presence of tip reduces lift and performance compared with corresponding values for 2-dimensional wing; it appeared from work by K.STEWARTSON that addition of vane at wing tip might counteract this effect; effect due to presence of vane determined.
Effect of Delta vanes on supersonic wings
Aeronautical Quarterly
Aeronautical Quarterly ; 5 , Part 4
1954
29 pages
Aufsatz (Zeitschrift)
Englisch
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