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2000 (2)

1999 (2)

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Static performance of six innovative thrust reverser concepts for subsonic transport applications : summary of the NASA Langley Innovative Thrust Reverser Test Program
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Year: 2000 Publisher: Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center,

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Static performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction control
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Year: 1999 Publisher: Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center,

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Book
Static performance of six innovative thrust reverser concepts for subsonic transport applications : summary of the NASA Langley Innovative Thrust Reverser Test Program
Authors: --- ---
Year: 2000 Publisher: Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center,

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Abstract


Book
Static performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction control
Authors: --- ---
Year: 1999 Publisher: Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center,

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