Showing 1 - 7 results of 7 for search 'Kacynski, Kenneth J.', query time: 0.04s Refine Results
  1. 1
    A three-dimensional turbulent heat transfer analysis for advanced tubular rocket thrust chambers

    A three-dimensional turbulent heat transfer analysis for advanced tubular rocket thrust chambers by Kacynski, Kenneth J.

    [Washington, DC] : [Springfield, Va. : National Aeronautics and Space Administration ; National Technical Information Service, distributor, 1990
    Format: Government Document Book


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  2. 2
    A dual-cooled hydrogen-oxygen rocket engine heat transfer analysis

    A dual-cooled hydrogen-oxygen rocket engine heat transfer analysis by Kacynski, Kenneth J.

    [Washington, D.C.] : [Springfield, Va.] : National Aeronautics and Space Administration ; [National Technical Information Service, distributor], 1991
    Format: Government Document Book


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  3. 3
    The prediction of nozzle performance and heat transfer in hydrogen/oxygen rocket engines with transpiration cooling, film cooling, and high area ratios

    The prediction of nozzle performance and heat transfer in hydrogen/oxygen rocket engines with transpiration cooling, film cooling, and high area ratios by Kacynski, Kenneth J.

    [Washington, DC] : [Springfield, Va.] :; [Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration ; [National Technical Information Service, distributor], 1994
    Format: Government Document Book


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  4. 4
    Experimental evaluation of heat transfer on a 1030:1 area ratio rocket nozzle

    Experimental evaluation of heat transfer on a 1030:1 area ratio rocket nozzle by Kacynski, Kenneth J.

    [Washington, D.C.] : [Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information Service], 1987
    Format: Government Document Book


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  5. 5
    A dual-cooled hydrogen-oxygen rocket engine heat transfer analysis

    A dual-cooled hydrogen-oxygen rocket engine heat transfer analysis by Kacynski, Kenneth J.

    [Washington, D.C.] : [Springfield, Va. : National Aeronautics and Space Administration ; National Technical Information Service, distributor, 1991
    Format: Government Document Book


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  6. 6
    Experimental thrust performance of a high-area-ratio rocket nozzle

    Experimental thrust performance of a high-area-ratio rocket nozzle by Pavli, Albert J.

    [Washington, DC] : [Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; For sale by the National Technical Information Service], 1987
    Other Authors: “…Kacynski, Kenneth J.…”
    Format: Government Document Book


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  7. 7
    Comparison of theoretical and experimental thrust performance of a 1030:1 area ratio rocket nozzle at a chamber pressure of 2413 kN/m²(350 psia)

    Comparison of theoretical and experimental thrust performance of a 1030:1 area ratio rocket nozzle at a chamber pressure of 2413 kN/m²(350 psia) by Smith, Tamara A.

    [Washington, D.C.] : [Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information Service], 1987
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    Format: Government Document Book


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