Damping in roll of models with 45 [degrees], 60 [degrees] and 70 [degrees] delta wings determined at high subsonic, transonic, and supersonic speeds with rocket-powered models
1952
18 S
Ill., graph. Darst
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Report
English