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Aerodynamics, Supersonic
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Langley Research Center
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Riebe, Gregory D.
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Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts at Mach numbers of 2.96, 3.96, and 4.63 /
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Pittman, Jimmy L.
Published 1980
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Aerodynamic test and analysis of a turbojet-boosted launch vehicle concept (spacejet) over a Mach number range of 1.50 to 2.86 /
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Riebe, Gregory D.
Published 1981
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Langley Research Center
Riebe, Gregory D.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch
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Morris, Odell A.
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Pittman, Jimmy L.
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Small, William J. (William John), 1939-
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