Effects of cone angle, Mach number, and nose blunting on transition at supersonic speeds
1961
31 S.
Ill., graph. Darst.
Langzeitarchivierung durch Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Buch
Englisch
Effects of cone angle, Mach number, and nose blunting on transition at supersonic speeds
Engineering Index Backfile | 1961
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