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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
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Authors:
Penland, Jim A.
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Hallissy, James B.
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Dillon, James L.
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United States.
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Langley Research Center
Year: 1979 Publisher: Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch,
Year: 1979 Publisher: Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch,
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