Chordwise pressure distributions on a 12-foot-span wing of NACA 66-series airfoil sections up to a Mach number of 6.0
1948
147 S
Ill., graph. Darst
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Book
English
Engineering Index Backfile | 1948
|Engineering Index Backfile | 1959
|Engineering Index Backfile | 1947
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