Research Catalog

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  • Heat transfer on a film-cooled rotating blade [microform] / Vijay K. Garg.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
    • 1999

  • Performance of an axisymmetric rocket based combined cycle engine during rocket only operation using linear regression analysis [microform] / Timothy D. Smith ... [et al.].

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998

  • Application of the [kappa]-[omega] turbulence model to quasi-three-dimensional turbomachinery flows [microform] / R.V. Chima.

    • Text
    • Reston, VA : American Institute of Aeronautics and Astronautics ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Prediction of heat and mass transfer in a rotating ribbed coolant passage with a 180 degree turn [microform] / David L. Rigby.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
    • 1999

  • Wind-US code contributions to the first AIAA Shock Boundary Layer Interaction Prediction Workshop / Nicholas J. Georgiadis, Manan A. Vyas, and Dennis A. Yoder.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, 2013.
    • 2013
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo51482

  • Summary of EASM turbulence models in CFL3D with validation test cases / Christopher L. Rumsey and Thomas B. Gatski.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, June 2003.
    • 2003-6
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS51551

  • Comparison of predicted and measured turbine vane rough surface heat transfer / R.J. Boyle, C.M. Spuckler, and B.L. Lucci.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, December 2000.
    • 2000-12
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo79758

  • Computational work to support FAP/SRW variable-speed power-turbine development / Ali A. Ameri.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo32902

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