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  • Cooling apparatus and couplings therefor [microform] / inventors, Curtis Lomax, Bruce Webbon.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1989]
    • 1989

  • Bearing tester data compilation analysis, and reporting and bearing math modeling [microform] : monthly progress report for July, 1986.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986

  • Effects of cooling system parameters on heat transfer in PAFC stack [microform] / Ali A. Abdul-Aziz.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1985]
    • 1985

  • Effects of the cooling system parameters on heat transfer and performance of the PAFC stack during transient operation [microform] / Rabi M. J. Ridha.

    • Text
    • [Cleveland, Ohio] : Cleveland State University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1992]
    • 1992

  • Hydrogen file cooling with incident and swept-shock interactions in a Mach 6.4 nitrogen free stream [microform] / George C. Olsen and Robert J. Nowak.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Heat transfer on a film-cooled blade [microform] : effect of hole physics : prepared under contract NAS3-27571 / Vijay K. Garg, David L. Rigby.

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

  • Effect of velocity and temperature distribution at the hole exit on film cooling of turbine blades [microform] / V.K. Garg, R.E. Gaugler.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Nonintrusive flow rate determination through space shuttle water coolant loop floodlight coldplate [microform] / Rudolph Werlink, Harry Johnson, Ravi Margasahayam.

    • Text
    • Kennedy Space Center, Fla. : National Aeronautics and Space Administration, John F. Kennedy Space Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997
    • 1997

  • Development of a contact heat exchanger for a constructable radiator system [microform] / prepared by H. R. Howell.

    • Text
    • Dallas, Texas : Vought Corporation, [1983]
    • 1983

  • Rocket engine hot-spot detector [microform] : final report.

    • Text
    • Sacramento, Calif. : Aerojet TechSystems Company ; [Houston, Tex.] : National Aeronautics and Space Administration, Lyndon B. Johnson Space Center, [1985]
    • 1985

  • Perormance comparison of axisymmetric and three-dimensional hydrogen film coolant injection in a 110N hydorgen-oxygen rocket [microform] / Lynn A. Arrington and Brian D. Reed.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center, [1992?]
    • 1992

  • Flow boiling with enhancement devices for cold plate coolant channel design : final report / by Ronald D. Boyd, Sr.

    • Text
    • Prairie View, TX : Department of Mechanical Engineering, Prairie View A&M University ; [Houston, Tex.] : National Aeronautics and Space Administration (NASA) Lyndon B. Johnson Space Center, [1989]
    • 1989
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo29929

  • Flow boiling with enhancement devices for cold plate coolant channel design [microform] : final report / by Ronald D. Boyd, Sr.

    • Text
    • Prairie View, TX : Department of Mechanical Engineering, Prairie View A&M University ; [Houston, Tex.] : National Aeronautics and Space Administration (NASA) Lyndon B. Johnson Space Center, [1989]
    • 1989

  • Influence of coolant tube curvature on film cooling effectiveness as detected by infrared imagery / S. Stephen Papell, Robert W. Graham, and Richard P. Cageao.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, November 1979.
    • 1979-11
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo52212

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