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  • An analysis of supersonic flows with low-Reynolds number compressible two-equation turbulence models using LU finite volume implicit numerical techniques [microform] / J. Lee.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, [1994]
    • 1994

  • Scale disparity and spectral transfer in anisotropic numerical turbulence [microform] / Ye Zhou, P.K. Yeung, James G. Brasseur.

    • Text
    • Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Modification of the two-equation turbulence model in NPARC to a Chien low Reynolds number k-epsilon formulation [microform] / Nicholas J. Georgiadis, Tawit Chitsomboon and Jiang Zhu.

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

  • Methodology for sensitivity analysis, approximate analysis, and design optimization in CFD for multidisciplinary applications [microform] : progress report for the period April 15, 1992 to January 31, 1993 / by Arthur C. Taylor, III, principal investigator ; Gene W. Hou, co-principal investigator.

    • Text
    • Norfolk, Va. : Old Dominion University Research Foundation ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1993]
    • 1993

  • Low Reynolds number two-equation modeling of turbulent flows [microform] / V. Michelassi and T.-H. Shih.

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

  • Low Reynolds number [kappa]-[epsilon] and empirical transition models for oscillatory pipe flow and heat transfer [microform] / Christopher Bauer.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1993]
    • 1993

  • Development of a low-Reynolds number, nonlinear [kappa-epsilon] model for the reduced Navier-Stokes equations [microform] : a final technical report for NASA-LeRC grant NAG-1781 / David A. Boger, T.R. Govindan, and Henry McDonald.

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

  • A k-E [i.e. Kappa-Epsilon] calculation of transitional boundary layers [microform] / Z. Yang and T.H. Shih.

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

  • Investigation of low-Reynolds-number rocket nozzle design using PNS-based optimization procedure [microform] / M. Moin Hussaini and John J. Korte.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • CMOTT turbulence module for NPARC [microform] : under cooperative agreement NCC3-520 / J. Zhu and T.-H. Shih.

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

  • Design and predictions for a high-altitude (low-Reynolds-number) aerodynamic flight experiment [microform] / Donald Greer ... [et al.].

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
    • 1999

  • Efficient parallel algorithm for direct numerical simulation of turbulent flows [microform] / Stuti Moitra and Thomas B. Gatski.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Design and performance calculations of a propeller for very high altitude flight [microform] / L. Danielle Koch.

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

  • Slip-boundary equations for multicomponent nonequilibrium airflow [microform] / Roop N. Gupta, Carl D. Scott, James N. Moss.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1985.
    • 1985

  • Validation of a CFD methodology for variable speed power turbine relevant conditions / Ali A. Ameri, Paul W. Giel, Ashlie B. McVetta.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo45754

  • Dynamic wind-tunnel testing of a sub-scale iced S-3B Viking / Sam Lee, Billy Barnhart, Thomas P. Ratvasky.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo51477

  • A computational study for the utilization of jet pulsations in gas turbine film cooling and flow control / Olga V. Kartuzova.

    • Text
    • Cleveland, Ohio : Cleveland State University : National Aeronautics and Space Administration, Glenn Research Center, September 2012.
    • 2012-9
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo53818

  • Simulation of VSPT experimental cascade under high and low free-stream turbulence conditions / Ali A. Ameri, Paul W. Giel, Ashlie B. Flegel.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo59311

  • Requirements for large eddy simulation computations of variable-speed power turbine flows / Ali A. Ameri.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, March 2016.
    • 2016-3
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo72510

  • Investigation of low-Reynolds-number rocket nozzle design using PNS-based optimization procedure / M. Moin Hussaini and John J. Korte.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, November 1996.
    • 1996-11
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS67205

  • An evaluation of three two-dimensional computational fluid dynamics codes including low Reynolds numbers and transonic Mach numbers / Raymond M. Hicks and Susan E. Cliff.

    • Text
    • [Moffett Field, Calif.] : [Ames Research Center], [1991]
    • 1991
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS60524

  • The screem-J4D : a proposal in response to a low Reynolds number station keeping mission.

    • Text
    • Notre Dame, IN : Dept. of Aerospace and Mechanical Engineering, University of Notre Dame, [1990]
    • 1990
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS60887

  • 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

  • Implementation of a transition model in a NASA code and validation using heat transfer data on a turbine blade / 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/gpo32880

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