Experimental aerodynamic characteristics of 10 short axisymmetric bodies at Mach numbers of 5 to 15
1965
32 S
graph. Darst.
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Book
English
Shock tunnel study of spiked aerodynamic bodies flying at hypersonic Mach numbers
Tema Archive | 2002
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