Effect of wing leading-edge shape on aerodynamic characteristics of a 67° swept wing-body model at Mach 1.50 to 4.63
1966
22 S
Ill., graph. Darst
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Book
English