Aerodynamic characteristics of a hypersonic research airplane concept having a 70° swept double-delta wing at mach numbers from 1.50 to 2.86
1975
81 S
graph. Darst
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Book
English