Six-component low-speed tunnel tests of jet-flap complete models with variation of aspect ratio, dihedral, and sweepback, including the influence of ground proximity
1967
66 S.
Ill., graph. Darst.
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Book
English
DDC: | 629.134/33 |
Wind tunnel tests of tapered wings with various amounts of dihedral and sweepback
Engineering Index Backfile | 1948
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