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Impingement of boundary-reflected disturbances originating at the nose of a body of revolution in the Langley Research Center 16-foot transonic tunnel
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Year: 1998 Publisher: Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center,

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A wind tunnel investigation of three NACA 1-series inlets at Mach numbers up to 0.92
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Year: 1996 Publisher: Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center,

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Static internal performance of a thrust vectoring and reversing two-dimensional convergent-divergent nozzle with an aft flap
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Year: 1986 Publisher: Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch,

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Investigation of convergent-divergent nozzles applicable to reduced-power supersonic cruise aircraft
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Year: 1980 Publisher: [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch,

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