Aerodynamic investigation of a parabolic body of revolution at Mach number of 1.92 and some effects of an annular supersonic jet exhausting from the base
1956
62 S
Ill., graph. Darst
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Book
English
Experimental Investigation of Supersonic Wrap-Around Fin Aerodynamic Mach Number Effects
British Library Conference Proceedings | 1999
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