Pressure distributions and aerodynamic characteristics of several spoiler controls on a 40° sweptback wing at a Mach number of 1.61
1960
66 S
graph. Darst
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Book
English
Engineering Index Backfile | 1960
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