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  • Three-dimensional Navier-Stokes heat transfer predictions for turbine blade rows [microform] / Robert J. Boyle and Paul W. Giel.

    • Text
    • [Washington, D.C.] : NASA ; [Springfield, Va. : National Technical Information Service, distributor, 1992]
    • 1992

  • Two-dimensional Navier-Stokes heat transfer analysis for rough turbine blades system [microform] / R.J. Boyle and K.C. Civinskas.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Adelphi, MD?] : U.S. Army Research Laboratory ; [Springfield, Va. : National Technical Information Service, distributor, 1991]
    • 1991

  • Grid orthogonality effects on predicted turbine midspan heat transfer and performance [microform] / R.J. Boyle and A.A. Ameri.

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

  • Heat transfer predictions for two turbine nozzle geometries at high Reynolds and Mach numbers [microform] / R.J. Boyle and R. Jackson.

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

  • Prediction of nonuniform inlet temperature effects on vane and rotor heat transfer [microform] / R.J. Boyle, P.W. Giel.

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

  • Prediction of relaminarization effects on turbine blade heat transfer [microform] / R.J. Boyle, P.W. Giel.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2001]
    • 2001
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS27419

  • Aerodynamic performance and turbulence measurements in a turbine van cascade [microform] / Robert J. Boyle and Barbara L. Lucci, Richard G. Senyitko.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center ; Hanover MD : Available from NASA Center for AeroSpace Information, [2002]
    • 2002
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS43727

  • Engineering analysis using a web-based protocol [microform] / James D. Schoeffler, Russell W. Clauss.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center ; Hanover MD : Available from NASA Center for AeroSpace Information, [2002]
    • 2002
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS43890

  • Navier-Stokes analysis of turbine blade heat transfer [microform] / R.J. Boyle ; prepared for the 35th International Gas Turbine and Aeroengine Congress and Exposition sponsored by the American Society of Mechanical Engineers, Brussels, Belgium, June 11-14, 1990.

    • Text
    • [Washington, D.C.] : NASA ; [Springfield, Va. : For sale by the National Technical Information Service, 1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS66714

  • Heat transfer in serpentine passages with turbulence promoters [microform] / Robert J. Boyle.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration, 1984]
    • 1984

  • Comparison between measured turbine stage performance and the predicted performance using quasi-3D flow and boundary layer analyses [microform] / Robert J. Boyle and Jeffrey E Haas and Theodore Katsanis.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration, 1984]
    • 1984

  • Design concepts for cooled ceramic composite turbine vane / Robert J. Boyle, Ankur H. Parikh, and Vinod K. Nagpal.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, February 2015.
    • 2015-2
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo57223

  • Predicted turbine heat transfer for a range of test conditions / R.J. Boyle and B.L. Lucci.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, November 1996.
    • 1996-11
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo70711

  • Engineering analysis using a web-based protocol / James D. Schoeffler, Russell W. Clauss.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, October 2002.
    • 2002-10
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS43890

  • Mach number effects on turbine blade transition length prediction / R.J. Boyle and F.F. Simon.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, June 1998.
    • 1998-6
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo83126

  • Aerodynamics of a transitioning turbine stator over a range of Reynolds numbers / R.J. Boyle [and four others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, June 1998.
    • 1998-6
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo83134

  • 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

  • Infrared low temperature turbine vane rough surface heat transfer measurements / R.J. Boyle [and three others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, August 2000.
    • 2000-8
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo79813

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