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  • A generalized wall function [microform] / Tsan-Hsing Shih ... [et al.].

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

  • 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

  • Estimations of ABL fluxes and other turbulence parameters from Doppler lidar data [microform] / by Tzvi Gal-Chen and Mei Xu, and Wynn Eberhard.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1991]
    • 1991

  • A phase equation approach to boundary layer instability theory [microform] : Tollmien Schlichting waves / Philip Hall.

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

  • On the nonlinear stability of viscous modes within the Rayleigh problem on an infinite flat plate [microform] / J.C. Webb, S.R. Otto, G.M. Lilley.

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

  • Effect of nonzero surface admittance on receptivity and stability of compressible boundary layer [microform] / Meelan Choudhari.

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

  • Computation of turbulent boundary layers employing the defect wall-function method [microform] / Douglas L. Brown.

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

  • Laser transit anemometer measurements on a slender cone in the Langley unitary plan wind tunnel [microform] / William M. Humphreys, Jr. ... [et al.].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1990]
    • 1990

  • User's manual for the Langley boundary layer noise propagation program (MRS-BLP) [microform] / Peter L. Spence.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1991]
    • 1991

  • Shear flow control of cold and heated rectangular jets by mechanical tabs [microform] / W.H. Brown and K.K. Ahuja.

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

  • Turbulence modeling for sharp-fin-induced shock wave/turbulent boundary-layer interactions [microform] / G.C. Horstman.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1990]
    • 1990

  • A laser Doppler velocimeter approach for near-wall three-dimensional turbulence measurements [microform] / D.A. Johnson and J.D. Brown.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1990]
    • 1990

  • Determination of the pressure drag of airfoils by integration of surface pressures [microform] / Williams H. Phillips.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1990]
    • 1990

  • The inviscid axisymmetric stability of the supersonic flow along a circular cylinder [microform] / Peter W. Duck.

    • Text
    • Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1989]
    • 1989

  • Computational analysis in support of the SSTO flowpath test [microform] / Beverly S. Duncan and Charles J. Trefny.

    • Text
    • [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

  • On the evolution of centrifugal instabilities within curved incompressible mixing layers [microform] / S.R. Otto, T.L. Jackson, F.Q. Hu.

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

  • On supersonic-inlet boundary-layer bleed flow [microform] / Gary J. Harloff and Gregory E. Smith.

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

  • Stability of separating subsonic boundary layers [microform] / Jamal A. Masad, Ali H. Nayfeh.

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

  • Active control of instabilities in laminar boundary-layer flow [microform] / Ronald D. Joslin, Gordon Erlebacher, M. Yousuff Hussaini.

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

  • Effect of crossflow on Görtler instability in incompressible boundary layers [microform] / Y.H. Zurigat, M.R. Malik.

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

  • The stability of two-phase flow over a swept-wing [microform] / Adrian V. Coward, Philip Hall.

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

  • Experiments on the flow field physics of confluent boundary layers for high-lift systems [microform] / by R.C. Nelson, F.O. Thomas, and H. C. Chu.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1994

  • Third-moment closure of turbulence for predictions of separating and reattaching shear flows [microform] : final report on "A study of Reynolds-Stress Closure Model" / by R.S. Amano, principal investigator and Pankaj Goel, research assistant.

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

  • Active control of panel vibrations induced by a boundary layer flow [microform] / Pao-Liu Chow.

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

  • Development of a new instrument for direct skin friction measurements [microform] : final report for NASA grant NAG 1-303 / by A.D. Vakili, J.M. Wu.

    • Text
    • Tullahoma, TN : Gas Dynamics Division, The University of Tennessee Space Institute ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986

  • Response of multi-panel assembly to noise from a jet in forward motion [microform] / A. Bayliss ... [et al.].

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

  • Wavenumber selection for small-wavelength Görtler vortices in curved channel flows [microform] / Andrew Dando, Philip Hall.

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

  • Computation of turbulent boundary layers flows with an algbraic stress turbulence model [microform] / by Sang-Wook Kim and Yen-Sen Chen.

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

  • Direct numerical simulation of transitional and turbulent flow over a heated flat plate using finite-difference schemes [microform] / Nateri K. Madavan.

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

  • Large-eddy simulation of laminar-turbulent breakdown at high speeds with dynamic subgrid-scale modeling [microform] / Nabil M. El-Hady.

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

  • The velocity field created by a shallow bump in a boundary layer [microform] / Michael Gaster, Chester E. Grosch, Thomas L. Jackson.

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

  • Numerical simulations of the flow in the HYPULSE expansion tube [microform] / Gregory J. Wilson, Myles A. Sussman, and Robert J. Bakos.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Numerical calculations of shock-wave/boundary-layer flow interactions [microform] / P.G. Huang and W.W. Liou.

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

  • Computer program BL2D for solving two-dimensional and axisymmetric boundary layers / Venkit Iyer.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, VA : National Technical Information Service, distributor, 1995]
    • 1995

  • Numerical studies of boundary-layer receptivity [microform] : a progress report / submitted by Helen L. Reed.

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

  • An experimental study of a turbulent boundary layer in the trailing edge region of a circulation-control airfoil [microform] / Jeff Brown.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1995]
    • 1995

  • Non-linear boundary-layer receptivity due to distributed surface roughness [microform] : final report / by principal investigator, Gregory V. Selby, Tahani R. Amer, graduate research assistant.

    • Text
    • Norfolk, Va. : Old Dominion University Research Foundation, Dept. of Mechanical Engineering, College of Engineering & Technology ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Multiple scales approach to weakly nonparallel and curvature effects [microform] : details for the novice / Bart A. Singer and Meelan Choudhari.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Weakly nonparallel and curvature effects on stationary crossflow instability [microform] : comparison of results from multiple-scales analysis and parabolized stability equations / Bart A. Singer, Meelan Choudhari, and Fei Li.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • A self-contained, automated methodology for optimal flow control validated for transition delay [microform] / Ronald D. Joslin ... [et al.].

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

  • Flow characteristics in boundary layer bleed slots with plenum [microform] / A. Hamed, J.J. Yeuan and J.D. Jun.

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

  • The effect of crossflow on Görtler vortices [microform] / S.R. Otto, James P. Denier.

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

  • On the nonlinear evolution of a stationary cross-flow vortex in a fully three-dimensional boundary layer flow [microform] / J.S.B. Gajjar.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, Institute for Computational Mechanics in Propulsion ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Implementation of a two-equation K-[omega] turbulence model in NPARC [microform] / Dennis A. Yoder and Nicholas J. Georgiadis, Paul D. Orkwis.

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

  • Annual progress report ... entitled "an experimental investigation of the flow physics of high-lift systems" for the period March-December 1995 [microform] / by Flint O. Thomas and R.C. Nelson.

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

  • Annual progress report ... entitled An experimental investigation of the flow physics of high-lift systems, for the period March-December 1995 [microform] / by Flint O. Thomas and R.C. Nelson.

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

  • Turbulence modeling validation, testing, and development [microform] / J.E. Bardina, P.G. Huang, T.J. Coakley.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • An experimental study of a separated/reattached flow behind a backward-facing step. Re[subscript h] = 37,000 [microform] / Srba Jovic.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Three-dimensional Navier-Stokes simulations with two-equation turbulence models of intersecting shock-waves/turbulent boundary layer at Mach 8.3 [microform] / J.E. Bardina, T.J. Coakley.

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

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