Effects of Mach number and Reynolds number on the maximum lift coefficient of a wing of NACA 230-series airfoil sections
1947
14, [29] S.
Ill., graph. Darst.
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Book
English
Engineering Index Backfile | 1947
|Engineering Index Backfile | 1950
|Engineering Index Backfile | 1952
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