Aerodynamic characteristics of a hypersonic research airplane concept having a 70 ̊swept double-delta wing at Mach numbers from 0.80 to 1.20, with summary of data from 0.20 to 6.0 /
|Main Authors:||, ,|
|Format:||Government Document Online Book|
Washington, District of Columbia :
National Aeronautics and Space Administration, Scientific and Technical Information Branch,
|Series:||NASA technical paper ;
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