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  • Effect of pressure gradient on first mode of instability in high-speed boundary layers [microform] / Jamal A. Masad, Yousef H. Zurigat.

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

  • Development of a near-wall Reynolds-stress closure based on the SSG model for the pressure strain [microform] / R.M.C. So ... [et al.].

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

  • Nonlinear stability of oscillatory core-annular flow [microform] : a generalized Kuramoto-Sivashinsky equation with time periodic coefficients / Adrian V. Coward, Demetrios T. Papageorgiou, Yiorgos S. Smyrlis.

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

  • Improved two-equation k - [omega] turbulence models for aerodynamic flows [microform] / Florian R. Menter.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1992]
    • 1992

  • On the prediction of free turbulent jets with swirl using a quadratic pressure-strain model [microform] / Bassam A. Younis, Thomas B. Gatski, Charles G. Speziale.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, Institute for Computer Applications in Science and Engineering ; [Springfield, Va. : For sale by the National Technical Information Service, 1994]
    • 1994

  • A modified mixing length turbulence model for zero and adverse pressure gradients [microform] / J.M. Conley and B.P. Leonard.

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

  • Control of separated flow past a cylinder using tangential wall jet blowing [microform] / by Sejong Oh and Leonard Roberts.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1989]
    • 1989

  • The influence of free-stream turbulence on turbulent boundary layers with mild adverse pressure gradients [microform] : final report, NASA Cooperative Agreement NCC2-450 covering the period January, 1987-January 1989 / by J.A. Hoffmann, S.M. Kassir, S.M. Larwood.

    • Text
    • San Luis Obispo, Calif. : Aeronautical Engineering Dept., California Polytechnic State University ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1988]
    • 1988

  • 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

  • Wake measurements in a strong adverse pressure gradient [microform] / R. Hoffenberg, J.P. Sullivan, S.P. Schneider.

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

  • Near field pressure fluctuations in a circular jet [microform] : final report / principal investigator: Ho, Chih-Ming.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1985?]
    • 1985

  • Some features of surface pressure fluctuations in turbulent boundary layers with zero and favorable pressure gradients [microform] / B.E. McGrath and R.L. Simpson.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1987.
    • 1987

  • Modification of a variational objective analysis model for new equations for pressure gradient and vertical velocity in the lower troposphere and for spatial resolution and accuracy of satellite data [microform] / G.L. Achtemeier.

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

  • Transitional boundary layers under the influence of high free stream turbulence, intensive wall cooling and high pressure gradinets in hot gas circulation [microform] / Klaus Rued.

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

  • A root-mean-square pressure fluctuations model for internal flow applications [microform] / Y.S. Chen.

    • 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

  • 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

  • Experimental and theoretical studies of capillary-pumped loop heat pipes [microform] : progress report for period January 15, 1994-July 15, 1994 / N.T. Obot.

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

  • Numerical solutions of the complete Navier-Stokes equations [microform] : progress report no. 27 for the period October 1, 1995 to September 30, 1996 / prepared by H.A. Hassan.

    • Text
    • Raleigh, N.C. : Dept. of Mechanical and Aerospace Engineering, North Carolina State University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Bidirectional brush seals [microform] / Robert C. Hendricks ... [et al.].

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

  • Effect of pressure gradients on plate response and radiation in a supersonic turbulent boundary layer [microform] / Abdelkader Frendi.

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

  • A review of hypersonic boundary layer stability experiments in a quiet Mach 6 wind tunnel [microform] / Stephen P. Wilkinson.

    • Text
    • Reston, VA : American Institute of Astronautics and Aeronautics ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Investigation of the effect of two-dimensional cavities on boundary layers in an adverse pressure gradient [microform] / Richard J. Margason.

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

  • Summary of work on shock wave feature extraction in 3-D datasets [microform] / principal investigator, Lambertus Hesselink.

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

  • Swept-wing receptivity studies using distributed roughness [microform] : annual technical report / William S. Saric.

    • Text
    • Tempe, AZ : Mechanical and Aerospace Engineering, College of Engineering and Applied Science, Arizona State University ; Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998

  • The thin oil film equation [microform] / James L. Brown and Jonathan W. Naughton.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
    • 1999

  • Effectiveness of micro-blowing technique in adverse pressure gradients [microform] / Gerard E. Welch ... [et al.].

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Springfield, VA : National Technical Information Service, distributor, [2001]
    • 2001

  • Heat transfer and pressure drop performance of a finned-tube heat exchanger proposed for use in the NASA Lewis altitude wind tunnel [microform] / G. James Van Fossen.

    • Text
    • [Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, 1985]
    • 1985

  • Trailing edge flow conditions as a factor in airfoil design [microform] / by A. I. Ormsbee and Mark D. Maughmer.

    • Text
    • Urbana, Ill. : Aeronautical and Astronautical Engineering Dept., University of Illinois ; [Washington, DC : National Aeronautics and Space Administration, 1984]
    • 1984
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS86754

  • Nested subcritical flows within supercritical systems / R.C. Hendricks ... [and others].

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, [1985]
    • 1985
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS105611

  • Nested subcritical flows within supercritical systems [microform] / R.C. Hendricks ... [et al.].

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, [1985]
    • 1985
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS105611

  • Determination of the thermal stability of perfluoroalkylethers by tensimetry : instrumentation and procedure / Larry S. Helmick and William R. Jones, Jr.

    • Text
    • [Washington, D.C.] : [National Aeronautics and Space Administration] ; [Springfield, Va.] : [For sale by the National Technical Information Service], [1989]
    • 1989
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS108769

  • Determination of the thermal stability of perfluoroalkylethers by tensimetry [microform] : instrumentation and procedure / Larry S. Helmick and William R. Jones, Jr.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1989]
    • 1989

  • Development of the variational SEASAT data analysis technique [microform] : final report / submitted by Dr. Yoshi K. Sasaki, Dr. Lang-Ping Chang, and Dr. James S. Goerss.

    • Text
    • [Greenbelt, Md.] : National Aeronautics and Space Administration, Goddard Space Flight Center, [1985]
    • 1985

  • Autoclave processing for composite material fabrication. 1 An analysis of resin flows and fiber compactions for thin laminate [microform] / T.H. Hou.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1985]
    • 1985

  • Investigation of the effects of pressure gradient, temperature, and wall temperature ratio on the stagnation point heat transfer for circular cylinders and gas turbine vanes [microform] / by H.T. Nagamatsu and R. E. Duffy.

    • Text
    • Troy, N.Y. : Rensselaer Polytechnic Institute, [1984]
    • 1984

  • Bidirectional brush seals / Robert C. Hendricks [and three others].

    • Text
    • Cleveland, Ohio : National National Aeronautics and Space Administration, Lewis Research Center, January 1997.
    • 1997-1
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo70398

  • Evolution of a planar wake in adverse pressure gradient / David M. Driver, George G. Mateer.

    • Text
    • Moffett Field, California : National Aeronautics and Space Administration, Ames Research Center, February 2016.
    • 2016-2
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo73014

  • Effectiveness of micro-blowing technique in adverse pressure gradients / Gerard E. Welch [and three others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center : U.S. Army Research Laboratory, January 2001.
    • 2001-1
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo86659

  • Large Eddy Simulation of a film cooling flow injected from an inclined discrete cylindrical hole into a crossflow with zero-pressure gradient turbulent boundary layer / Perry L. Johnson, Vikram Shyam.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo32522

  • Vandenberg Air Force Base pressure gradient wind study / Jaclyn A. Shafer.

    • Text
    • Kennedy Space Center, FL : National Aeronautics and Space Administration, Kennedy Space Center, September 2013.
    • 2013-9
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo53510

  • High-fidelity simulation of turbulent flow past a Gaussian bump / Ali Uzun and Mujeeb R. Malik.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, May 2021.
    • 2021-5
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo158441

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