Effects of forebody length on the stability and control characteristics at a mach number of 2.01 of a canard airplane configuration with a trapezoidal aspect-ratio-3 wing
1962
30 S
Ill., graph. Darst
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Book
English