Pressure-distribution investigation of an N.A.C.A. 0009 airfoil with a 80-percent-chord plain flap and three tabs
1940
11 S
graph. Darst
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Book
English
Engineering Index Backfile | 1940
|Engineering Index Backfile | 1940
|Engineering Index Backfile | 1939
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