Use of camber and twist to produce low-drag delta or swept-back wings, without leading-edge singularities, at supersonic speeds
1961
54 S.
graph. Darst.
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Report
English
DDC: | 629.13432 |
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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