Aerodynamics loads at Mach numbers from 0.70 to 2.22 on an airplane model having a wing and canard of triangular plan form and either single or twin vertical tails
1961
57 S
graph. Darst
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Book
English