The effect of canard and vertical tails on the aerodynamic characteristics of a model with a 59 [degrees] sweptback wing at a Mach number of 0.30
1974
33 S
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
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English