Effects of simulated retrorockets on the aerodynamic characteristics of a body of revolution at Mach numbers from 0.25 to 1.90
1962
45 S.
Ill., graph. Darst.
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Book
English
Experimental determination of flat plate recovery factors for Mach numbers between 1.90 and 3.14
Engineering Index Backfile | 1954
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