Investigation at transonic speeds of loading over a 30° sweptback wing of aspect ratio 3, taper 0.2, and NACA 65A004 airfoil section mounted on a body
1960
79 S
Ill., graph. Darst
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Book
English