An investigation of wing and aileron loads due to deflected inboard and outboard ailerons on a 4-percent-thick 30° sweptback wing at transonic speeds
1961
282 S
graph. Darst
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Book
English
Engineering Index Backfile | 1961
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