Experiments on a 70 [degrees] cropped delta wing with 90 [degrees] downward deflected peripheral blowing
1962
13 S., [6] Bl
Ill., graph. Darst
Langzeitarchivierung durch Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Hochschulschrift
Englisch
Low speed wind tunnel tests on a 70 [degrees] cropped delta wing
TIBKAT | 1960
|Aerodynamic characteristics of model wing having split flap deflected downward and moved to rear
Engineering Index Backfile | 1932
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