Effects of independent variations of mach number and Reynolds number of the maximum lift coefficients of four NACA 6-series airfoil sections
1952
32 S.
graph. Darst.
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Book
English
Engineering Index Backfile | 1952
|Engineering Index Backfile | 1947
|Engineering Index Backfile | 1950
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