Use of camber and twist to produce low drag delta or swept back wings, without leading edge singularities, at supersonic speeds
low-drag swept-back leading-edge
1961
54 S.
Sonstige
Englisch
RVK: | ZO 7000 |
Some Effects of Camber on Swept-Back Wings
SAE Technical Papers | 1973
|Theoretical lift of flat swept-back wings at supersonic speeds
Engineering Index Backfile | 1948
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