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Aerodynamics, Supersonic
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Blair, A. B.
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1
Effect of Reynolds number on the aerodynamic stability and control characteristics of a 55 degree clipped-delta-wing orbiter configuration at supersonic Mach numbers /
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Blair, A. B.
Published 1976
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2
Wind-tunnel investigation at supersonic speeds of a canard-controlled missile with fixed and free-rolling tail fins /
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Blair, A. B.
Published 1978
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3
Effect on tail-fin span on stability and control characteristics of a canard-controlled missile at supersonic Mach numbers /
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Blair, A. B.
Published 1983
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Wind-tunnel investigation at supersonic speeds of a remote-controlled canard missile with a free-rolling-tail brake torque system /
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Blair, A. B.
Published 1985
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5
Supersonic axial-force characteristics of a rectangular-box cavity with various length-to-depth ratios in a flat plate /
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Blair, A. B.
Published 1986
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Blair, A. B.
Langley Research Center
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United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch
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Allen, Jerry M.
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Hernandez, Gloria
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Stallings, Robert L.
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United States. National Aeronautics and Space Administration
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United States. National Aeronautics and Space Administration. Scientific and Technical Information Office
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