Effects at Mach numbers of 1.61 and 2.01 of camber and twist on the aerodynamic characteristics of three swept wings having the same planform
1961
48 S
graph. Darst
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Book
English
Engineering Index Backfile | 1961
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