Aerodynamic characteristics of a hypersonic research airplane concept having a 70° swept double-data wing at mach numerbes from 0.80 to 1.20, with summary of data from 0.20 to 6.0
NASA technical paper ; 1552
1979
144 S.
graph. Darst.
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
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English