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  • High Reynolds number research : a workshop / sponsored by Joint Institute for Advancement of Flight Sciences, the George Washington University, and NASA Langley Research Center and held at Hampton, Virginia, October 27-28, 1976 ; edited by Donald D. Baals.

    • Text
    • Washington : Scientific and Technical Information Office, National Aeronautics and Space Administration ; Springfield, Va. : for sale by National Technical Information Service, 1977.
    • 1977
    • 1 Item
    FormatCall NumberItem Location
    Text JSF 78-218Offsite

  • Low Reynolds number flow heat exchangers : advanced study institute book / edited by S. Kakaç, R.K. Shah, A.E. Bergles.

    • Text
    • Washington, D.C. : Hemisphere Pub. Corp., c1983.
    • 1983
    • 1 Item
    FormatCall NumberItem Location
    Text JSE 84-403Offsite

  • Inlet Reynolds number and temperature effects on the steady-state performance of a TFE731-2 turbofan engine / George A. Bobula and Roy A. Lottig.

    • Text
    • Washington : National Aeronautics and Space Administration ; Springfield, Va. : for sale by the National Technical Information Service, 1977.
    • 1977
    • 1 Item
    FormatCall NumberItem Location
    Text JBY Q-908Offsite

  • High Reynolds number flows using liquid and gaseous helium : discussion of liquid and gaseous helium as test fluids : including papers from the Seventh Oregon Conference on Low Temperature Physics, University of Oregon, October 23 to 25 1989 / Russell J. Donnelly, editor.

    • Text
    • New York : Springer-Verlag, c1991.
    • 1991
    • 1 Item
    FormatCall NumberItem Location
    Text JSE 93-302Offsite

  • 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

  • Navier-Stokes simulation of several high-lift reference H configurations [microform] / Wendy B. Lessard.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for AeroSpace Information ; Springfield, VA : National Technical Information Service [distributor, 1999]
    • 1999

  • A finite Reynolds number approach for the prediction of boundary layer receptivity in localized regions [microform] / Meelan Choudhari, Craig L. Streett.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1991]
    • 1991-1991

  • Comment on "Local energy transfer and nonlocal interactions in homogeneous, isotropic turbulence" [Phys. Fluids A2, 413 (1990)] [microform] / Robert G. Deissler.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1990]
    • 1990

  • Numerical solution for the velocity-derivative skewness of a low-Reynolds-number decaying Navier-Stokes flow [microform] / Robert G. Deissler.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1990]
    • 1990

  • An efficient and robust algorithm for two dimensional time dependent incompressible Navier-Stokes equations [microform] : high Reynolds number flows / John W. Goodrich.

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

  • Elliptic flow computation by low Reynolds number two-equation turbulence models [microform] / V. Michelassi and T.-H. Shih.

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

  • Final design proposal [microform] : Dawdler : 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 ; [Springfield, Va.? : National Technical Information Service, distributor, 1990]
    • 1991

  • Fast methods to numerically integrate the Reynolds equation for gas fluid films [microform] / Florin Dimofte.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va.? : National Technical Information Service, distributor, 1992]
    • 1992

  • Evaluation of high reynolds number flow in a 180 degree turn-around duct [microform] / by V.A. Sandborn and S.J. Marcy.

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

  • On the drag of model dendrite fragments at low Reynolds number [microform] / R. Zakhem and P.D. Weidman and H.C. de Groh III.

    • Text
    • [Washington, D.C.] : NASA ; [Springfield, Va. : National Technical Information Service, distributor, 1993]
    • 1993

  • Final report for the grant integration of viscous effects into inviscid computational methods [microform] / submitted to NASA Ames Research Center by Joseph Katz; principal investigator.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1990]
    • 1990

  • The three-dimensional flow past a rapidly rotating circular cylinder [microform] / James P. Denier, Peter W. Duck.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1993]
    • 1993

  • Analysis of fluctuating static pressure measurements in a large high Reynolds number transonic cryogenic wind tunnel [microform] / by William B. Igoe.

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

  • Unstructured and adaptive mesh generation for high Reynolds number viscous flows [microform] / Dimitri J. Mavriplis.

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

  • Reynolds number influences in aeronautics [microform] / Dennis M. Bushnell ... [et al.].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1993]
    • 1993

  • Low-speed tests of a high-aspect-ratio, supercritical-wing transport model equipped with a high-lift flap system in the Langley 4- by 7-meter and Ames 12-foot pressure tunnels [microform] / Harry L. Morgan, Jr., and Scott O. Kjelgaard.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : National Technical Information Service, distributor], 1983.
    • 1983

  • High Reynolds number tests of a NASA SC(3)-0712(b) airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnels [microform] / William G. Johnson, Jr., Acquilla S. Hill, and Otto Eichmann.

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

  • Drag 'n' fly [microform] : a proposal in response to a low Reynolds number station keeping mission / Hypersonic Minds, design team, Mark Foohey ... [et al,].

    • Text
    • Notre Dame, IN : Dept. of Aeropace and Mechanical Engineering, University of Notre Dame ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1990]
    • 1990

  • Flight Mechanics/Estimation Theory Symposium, 1989 [microform] : proceedings of a symposium sponsored by NASA Goddard Space Flight Center and held at Goddard Space Flight Center, Greenbelt, Maryland, May 23-24, 1989 / Thomas Stengle, editor.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : For sale by the National Technical Information Service, distributor, 1989]
    • 1989

  • An investigation of turbulence structure in a low-Reynolds-number incompressible turbulent boundary [microform] : final report / B.R. White, principal investigator, C.J. Strataridakis, graduate research assistant.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1987]
    • 1987

  • F/A-18 forebody vortex control [microform] / Brian R. Kramer ... [et al.].

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

  • The effects of viscosity on the stability of a trailing-line vortex in compressible flow [microform] / Jillian A.K. Stott, 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, 1994]
    • 1994

  • Hot-jet simulation in cryogenic wind tunnels [microform] / Keisuke Asai.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : For sale by the National Technical Information Service], 1989.
    • 1989

  • Reynolds-stress and dissipation rate budgets in a turbulent channel flow [microform] / N.N. Mansour, J. Kim, P. Moin.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1987]
    • 1987

  • Transonic Navier-Stokes calculations about a 65⁰ delta wing [microform] / W. Kelly Londenberg.

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

  • 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

  • Acoustic receptivity due to weak surface inhomogeneities in adverse pressure gradient boundary layers [microform] / Meelan Choudhari, Lian Ng, and Craig Streett.

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

  • Wing pressure distributions from subsonic tests of a high-wing transport model [microform] / Zachary T. Applin and Carl L. Gentry, Jr., M.A. Takallu.

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

  • 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

  • An application of a two-equation model of turbulence to three-dimensional chemically reacting flows [microform] / J. Lee.

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

  • Correlation of transonic-cone Preston-tube data and skin friction [microform] : final report (research grant number NAG 2-76) (Nov. 80 - May 84) / prepared by A. S. Abu-Mostafa and T.D. Reed.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1984]
    • 1984

  • Rapport d'essais du profil CAST 10 en transition dʹeclenchʹee, effectuʹes dans la soufflerie transsonique cryogʹenique T2 en pr'esence de parois auto-adaptables [microform] = Report on tests of a CAST 10 airfoil with fiexed transition in the T2 transonic cryogenic wind tunnel with self-adaptive walls / A. Seraudie, A. Blanchard, J.F. Breil.

    • Text
    • Toulouse : Centre DʹEtudes et de Recherches de Toulouse, Dept., DʹEtudes et de Recherches en Aerothermodynamique ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1985]
    • 1985

  • Low Reynolds number boundary layers in a disturbed environment [microform] / Dong-Kee Paik and Eli Reshotko.

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

  • Effects of droplet interactions on droplet transport at intermediate Reynolds numbers [microform] / Jian-Shun Shuen.

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

  • Influence of turbulence parameters, Reynolds number, and body shape on stagnation-region heat transfer [microform] / G. James Van Fossen and Robert J. Simoneau, Chan Y. Ching.

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

  • NASA Dryden Flow Visualization Facility [microform] / John H. Del Frate.

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

  • Control of unsteady separated flow associated with the dynamic stall of airfoils [microform] : final report, 95-09 / M.C. Wilder.

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

  • Experimental study of the effects of reynolds number on high angle of attack aerodynamic characteristics of forebodies during rotary motion [microform] / H. Pauley, J. Ralston, and E. Dickes.

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

  • Radial and circumferential flow surveys at the inlet and exit of the Space Shuttle Main Engine High Pressure Fuel Turbine model [microform] / S.T. Hudson ... [et al.].

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

  • The evolution of condensates in shock tube flow [microform] : final technical report, May 1, 1994 to April 30, 1995 / submitted by Joseph A. Johnson III.

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

  • Computational heat transfer analysis for oscillatory channel flows [microform] / Mounir Ibrahim and Mohan Kannapareddy.

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

  • A concept for transition mapping on a 10⁰-cone in the National Transonic Facility using flow-pressure variation [microform] / Ehud Gartenberg.

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

  • User manual for NASA Lewis 10- by 10-foot supersonic wind tunnel [microform] / Ronald H. Soeder.

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

  • A performance comparison of two small rocket nozzles [microform] / Lynn A. Arrington, Brian D. Reed, Angel Rivera, Jr.

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

  • Computation of sound generated by viscous flow over a circular cylinder [microform] / Jared S. Cox ... [et al.].

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

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