Effects of cone angle, Mach number, and nose blunting on transition at supersonic speeds
1961
31 S.
Ill., graph. Darst.
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Book
English
Effects of cone angle, Mach number, and nose blunting on transition at supersonic speeds
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