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book (7)


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Estimation of supersonic stage separation aerodynamics of winged-body launch vehicles using response surface methods
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Year: 2010 Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center,

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Unified application of vapor screen flow visualization and pressure sensitive paint measurement techniques to vortex- and shock wave-dominated flow fields
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Year: 2010 Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center,

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Wind tunnel investigation of passive porosity applied to the leading-edge extension and leading-edge flaps on a slender wing at subsonic speed
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Year: 2017 Publisher: Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center,

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Wind tunnel investigation of the supersonic stage separation aerodynamics of a generic 0.0175- scale bimese two-stage-to-orbit reusable launch vehicle configuration
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Year: 2020 Publisher: Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center,

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Analysis of a split-plot experimental design applied to a low-speed wind tunnel investigation
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Year: 2013 Publisher: Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center,

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Wind tunnel investigation of passive vortex control and vortex-tail interactions on a slender wing at subsonic and transonic speeds
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Year: 2013 Publisher: Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center,

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Experimental investigation of aeroelastic deformation of slender wings at supersonic speeds using a video model deformation measurement technique
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Year: 2013 Publisher: Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center,

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