Showing 1 - 8 results of 8 for search 'Vigyan Research Associates, Inc. : National Aeronautics and Space Administration, Langley Research Center,', query time: 7.39s Refine Results
  1. 1
    Method for the prediction of the installation aerodynamics of a propfan at subsonic speeds user manual /
    by Chandrasekaran, B., 1942-
    Published 1986
    “...Vigyan Research Associates, Inc. : National Aeronautics and Space Administration, Langley Research...”

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  2. 2
    An investigation at static conditions of nonaxisymmetric nozzle thrust reverser port geometry including effects of rounding and rotating the port corner /
    “...Vigyan Research Associates, Inc. : National Aeronautics and Space Administration, Langley Research...”

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  3. 3
    An experimental investigation of propfan installations on an unsewpt supercritical wing at transonic Mach numbers /
    “...Vigyan Research Associates, Inc. : National Aeronautics and Space Administration, Langley Research...”

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  4. 4
    Method for the prediction of the installation aerodynamics of a propfan at subsonic speeds : user manual /
    “...Vigyan Research Associates, Inc. : National Aeronautics and Space Administration, Langley Research...”

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
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  5. 5
    Subsonic flow investigations on a cranked wing designed for high maneuverability /
    by Rao, Dhanvada M, Rao, Dhanvada M
    Published 1986
    “...Vigyan Research Associates, Inc. : National Aeronautics and Space Administration, Langley Research...”

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
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  6. 6
    An experimental investigation of propfan installations on an unsewpt supercritical wing at transonic Mach numbers
    by Bartlett, Glynn R
    Published 1985
    “...Vigyan Research Associates, Inc. : National Aeronautics and Space Administration, Langley Research...”

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
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  7. 7
    An investigation at static conditions of nonaxisymmetric nozzle thrust reverser port geometry including effects of rounding and rotating the port corner
    by Arbiter, Dorothy G
    Published 1985
    “...Vigyan Research Associates, Inc. : National Aeronautics and Space Administration, Langley Research...”

    Government Document Book
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  8. 8
    Subsonic flow investigations on a cranked wing designed for high maneuverability
    by Rao, Dhanvada M
    Published 1986
    “...Vigyan Research Associates, Inc. : National Aeronautics and Space Administration, Langley Research...”

    Government Document Book
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