STOL characteristics of a propeller-driven, aspect-ratio-10, straight-wing airplane with boundary-layer control flaps, as estimated from large-scale wind-tunnel tests
1961
57 S.
Ill., graph. Darst.
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Book
English
Engineering Index Backfile | 1959
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