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  • Textbook multigrid efficiency for the incompressible Navier-Stokes equations [microform] : high Reynolds number wakes and boundary layers / James L. Thomas, Boris Diskin, Achi Brandt.

    • Text
    • Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [1999]
    • 1999

  • A new k-[epsilon] eddy viscosity model for high Reynolds number turbulent flows [microform] : model development and validation / T.-H. Shih ... [et al.].

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

  • Aerodynamics and heat transfer investigations on a high Reynolds number turbine cascade [microform] / T. Schobeiri, E. McFarland, and F. Yeh.

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

  • Numerical simulation of the flow about the F-18 HARV at high angle of attack [microform] / Scott M. Murman.

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

  • Effects of artificial viscosity on the accuracy of high-Reynolds-number [kappa-epsilon] turbulence model [microform] / Tawit Chitsomboon.

    • Text
    • Cleveland, Ohio : NASA, Lewis Research Center, Institute for Computational Mechanics in Propulsion ; [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

  • On the Lighthill relationship and sound generation from isotropic turbulence [microform] / Ye Zhou, Alexander Prashnowsky, Steven Oncley.

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

  • Acoustic properties and durability of liner materials at non-standard atmospheric conditions [microform] / K.K. Ahuja, R.J. Gaeta, Jr., and J.S. Hsu.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Numerical simulation of the flow about the F-18 HARV at high angle of attack [microform] / Scott M. Murman.

    • Text
    • San Jose, CA : MCAT Institute ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • 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

  • Sweeping and straining effects in sound generation by high Reynolds number isotropic turbulence [microform] / Ye Zhou, Robert Rubinstein.

    • Text
    • Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • A longitudinal aerodynamic data repeatability study for a commercial transport model test in the National Transonic Facility [microform] / R.A. Wahls ... [et al.].

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

  • An experimental and numerical investigation of turbulent vortex breakdown and aircraft wakes [microform] : final report, contract NAG 1-1775 / by Robert E. Spall.

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

  • A near-wall Reynolds-stress closure without wall normals [microform] : final report ... under grant number NAG-1-1772 / S.P. Yuan and R.M.C. So.

    • Text
    • Tempe, Ariz. : College of Engineering and Applied Sciences, Arizona State University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Fully nonlinear Görtler vortices in constricted channel flows and their effect on the onset of separation [microform] / James P. Denler, Philip Hall.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1992]
    • 1992

  • Cryogenic tunnel pressure measurements on a supercritical airfoil for several shock buffet conditions [microform] / Robert E. Bartels and John W. Edwards.

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

  • High Reynolds number effects on multi-hole probes and hot wire anemometers [microform] / N. Ramachandran ... [et al.].

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

  • A note on kinetic energy, dissipation and enstrophy [microform] / Jie-Zhi Wu, Ye Zhou, Meng Fan.

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

  • Multigrid strategies for viscous flow solvers on anisotropic unstructured meshes [microform] / Dimitri J. Mavriplis.

    • Text
    • Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [1998]
    • 1998

  • Directional agglomeration multigrid techniques for high-Reynolds number viscous flows [microform] / Dimitri J. Mavriplis.

    • Text
    • Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [1998]
    • 1998

  • Computation of separated and unsteady flows with one- and two-equation turbulence models [microform] : 32nd Aerospace Sciences meeting & exhibit, January 10-13, 1994/Reno, NV / J.A. Ekaterinaris and F.R. Menter.

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

  • Aeroacoustic data for a high Reynolds number axisymmetric subsonic jet [microform] / Michael K. Ponton, Lawrence S. Ukeiley, Sang W. Lee.

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

  • High Reynolds number hybrid laminar flow control (HLFC) flight experiment. IV, Suction system design and manufacture [microform] / Boeing Commercial Airplane Group.

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

  • High Reynolds number hybrid laminar flow control (HLFC) flight experiment. II, Aerodynamic design [microform] / Boeing Commercial Airplane Group.

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

  • Directional agglomeration multigrid techniques for high Reynolds number viscous flow solvers [microform] / D.J. Mavriplis.

    • Text
    • Reston, Va. : American Institute of Aeronautics and Astronautics ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998

  • Assessment of an Euler-interacting boundary layer method using high Reynolds number transonic transport flight data [microform] / Daryl L. Bonhaus and Dal V. Maddalon.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [1998]
    • 1998

  • Effects of yaw angle and Reynolds number on rectangular-box cavities at subsonic and transonic speeds [microform] / E.B. Plentovich, Julio Chu, and M.B. Tracy.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : For sale by the National Technical Information Service], 1991.
    • 1991
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS67795

  • Algebraic turbulence modeling for unstructured and adaptive meshes [microform] / Dimitri J. Mavriplis.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS69038

  • The stability of two-dimensional wakes and shear-layers at high Mach numbers [microform] / D.T. Papageorgiou.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS69039

  • Pressure distributions from high Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel [microform] / William G. Johnson, Jr., and Acquilla S. Hill.

    • 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
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS85654

  • Aeroacoustic data for high Reynolds number supersonic axisymmetric jets [microform] / John M. Seiner, Michael K. Ponton.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.
    • 1985

  • A realizable Reynolds stress algebraic equation model [microform] / Tsan-Hsing Shih, Jiang Zhu, and John L. Lumley.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, Institute for Computational Mechanics in Propulsion, [1993]
    • 1993
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS97991

  • Optimization of an advanced design three-element airfoil at high Reynolds numbers / J.C. Lin, C.J. Dominik.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, [1995]
    • 1995
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo77769

  • Optimization of an advanced design three-element airfoil at high reynolds numbers / J.C. Lin, C.J. Dominik.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, [1995]
    • 1995

  • Cause and cure : deterioration in accuracy of CFD simulations with use of high-aspect-ratio triangular/tetrahedral grids / Sin-Chung Chang, Chau-Lyan Chang, Balaji Shankar Venkatachari.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, July 2017.
    • 2017-7
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo84059

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