Effect of taper ratio on low-speed static and yawing stability derivates of 45° sweptback wings with aspect ratio of 2.61
1948
20 S
Ill., graph. Darst
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Book
English
Engineering Index Backfile | 1948
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