Research Catalog

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  • Investigation of advanced counterrotation blade configuration concepts for high speed turboprop systems. Task 8, Cooling flow/heat transfer analysis [microform] : users manual / E.J. Hall ... [et al.].

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Investigation of advanced counterrotation blade configuration concepts for high speed turboprop systems. Task 8, Cooling flow/heat transfer analysis [microform] : users manual / E.J. Hall ... [et al.].

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • An analysis code for the Rapid Engineering Estimation of Momentum and Energy Losses (REMEL) [microform] / Lawrence J. DeChant.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Documentation and archiving of the Space Shuttle Wind Tunnel Test data base. Volume 2, user's guide to the archived data base [microform] / Paul O. Romere, Steve Wesley Brown.

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

  • Documentation and archiving of the space shuttle wind tunnel test data base. Volume 1, Background and description [microform] / Paul O. Romere, Steve Wesley Brown.

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

  • Simulation of brush insert for leading-edge-passage convective heat transfer [microform] / R.C. Hendricks ... [et al.].

    • Text
    • [Washington, D.C.] : NASA ; [Springfield, Va. : For sale by the National Technical Information Service, 1991?]
    • 1991

  • 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

  • Unsteady transonic heat transfer in a transient facility [microform] : semi-annual progress report / principal investigator, J.E. LaGraff.

    • Text
    • [Syracuse, N.Y.] : Syracuse University, Dept. of Mechanical and Aerospace Engineering ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1985]
    • 1985

  • Aerodynamics of heat exchangers for high-altitude aircraft [microform] / Mark Drela.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Aerodynamic investigation of incidence angle effects in a large scale transonic turbine cascade / Ashlie B. McVetta, Paul W. Giel, Gerard E. Welch.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, August 2013.
    • 2013-8
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo50526

  • Aerodynamic investigation of incidence angle effects in a large scale transonic turbine cascade / Ashlie B. McVetta, Paul W. Giel, Gerard E. Welch.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, June 2014.
    • 2014-6
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo53624

  • Modeling of aerobrake ballute stagnation point temperature and heat transfer to inflation gas / Parviz A. Bahrami.

    • Text
    • Moffett Field, California : National Aeronautics and Space Administration, Ames Research Center, 2012.
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo37271

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