Measured base pressures on several twin rocket-nozzle configurations at Mach numbers of 0.6 to 1.4 with effects due to nozzle canting and stabilizing fins
1960
19 S
Ill., graph. Darst
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Book
English
Aeroelastic investigation of three rocket fins at high mach numbers
Engineering Index Backfile | 1965
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