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  • Increased heat transfer to a cylindrical leading edge due to spanwise variations in the freestream velocity [microform] / D.L. Rigby and G.J. Van Fossen

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

  • Towards enhancing and delaying disturbances in free shear flows [microform] / W.O. Criminale, T.L. Jackson, D.G. Lasseigne.

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

  • Surface documentation of a 3-D supersonic, shock-wave-boundary layer interaction [microform] / Jeffrey K. Wideman ... [et al.].

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames 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

  • Detailed flow-field measurements over a 75⁰ swept delta wing [microform] / Scott O. Kjelgaard and William L. Sellers III.

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

  • On the freestream matching condition for stagnation point turbulent flows [microform] / Charles G. Speziale.

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

  • Parametric study of shock-induced combustion in a hydrogen air system [microform] / by J.K. Ahuja and S.N. Tiwari (principal investigator).

    • Text
    • Norfolk, Va. : Institute for Computational and Applied Mechanics, Old Dominion University ; Hampton, Va. : NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • 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

  • The influence of free-stream turbulence on separation of turbulent boundary layers in incompressible, two-dimensional flow [microform] : final report / J. Leith Potter ... [et al.].

    • Text
    • Nashville, TN : Vanderbilt University, School of Engineering, Dept. of Mechanical & Materials Engineering ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986

  • The effect of a row of helmholtz resonators on the turbulence in a boundary layer [microform] : semi-annual progress report, 30 September 1986, NASA research grant NAG-1-610 / Ronald L. Panton.

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

  • A zonal computational procedure adapted to the optimization of two-dimensioal thrust augmentor inlets [microform] / by T.S. Lund, D.A. Tavella, and L. Roberts.

    • Text
    • Stanford, CA : Stanford University, Dept. of Aeronautics and Astronautics : National Aeronautics and Space Administration, Ames Research Center, Joint Institute for Aeronautics and Acoustics ; [Springfield, Va. : For sale by the National Technical Information Service, 1985]
    • 1985

  • Exploratory flow visualization investigation of mast-mounted sights in presence of a rotor [microform] / Terence A. Ghee, Henry L. Kelley.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [St. Louis, Mo.] : US Army Aviation Systems Command, Aviation R&T Activity, [1995]
    • 1995

  • 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

  • The role of freestream turbulence scale in subsonic flow separation [microform] : interim progress report 2 ... 1 January 1985 - 30 June 1985 / J. Leith Potter ... [et al.].

    • Text
    • Nashville, TN : Vanderbilt University, School of Engineering, Dept. of Mechanical & Materials Engineering ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1985]
    • 1985

  • Pitot-pressure measurements in flow fields behind a rectangular nozzle with exhaust jet for free-stream mach numbers of 0.00, 0,60, and 1.20 [microform] / Lawrence E. Putnam and Charles E. Mercer.

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

  • Hydrogen file cooling with incident and swept-shock interactions in a Mach 6.4 nitrogen free stream [microform] / George C. Olsen and Robert J. Nowak.

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

  • Viscous-flow analysis of a subsonic transport aircraft high-lift system and correlation with flight data [microform] : final report / by R.C. Potter and C.P. van Dam.

    • Text
    • Davis, CA : Dept. of Mechanical and Aeronautical Engineering, University of California ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Pressure distributions from subsonic tests of a NACA 0012 semispan wing model [microform] / Zachary T. Applin.

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

  • The effect of three-dimensional freestream disturbances on the supersonic flow past a wedge [microform] : NASA contract no. NAS1-19480 / Peter W. Duck, D. Glenn Lasseigne, M.Y. Hussaini.

    • Text
    • Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Effect of surface waviness on transition in three-dimensional boundary-layer flow [microform] / Jamal A. Masad.

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

  • Receptivity of flat-plate boundary layer in a non-uniform free stream (vorticity normal to the plate) [microform] : under cooperative agreement NCC1-241 / M.N. Kogan and M.V. Ustinov.

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

  • Comparison of turbulence models for nozzle-afterbody flows with propulsive jets [microform] / William B. Compton III.

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

  • Effect of curvature on the impact damage characteritiscs and residual strength of composite plates [microform] / Damodar R. Ambur and James H. Starnes, Jr.

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

  • Magellan aerodynamic characteristics during the termination experiment including thruster plume-free stream interaction [microform] : under cooperative agreement NCC1-104 / Francisco J. Cestero and Robert H. Tolson.

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

  • Water tunnel flow visualization study through poststall of 12 novel planform shapes [microform] / Gregory M. Gatlin, Dan H. Neuhart.

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

  • Measurements in transitional boundary layers under high free-stream turbulence and strong acceleration conditions [microform] : under grant NAG3-1249 / Ralph J. Volino and Terrence W. Simon.

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

  • The effect of vortex generators on a jet in a cross-flow [microform] / K.B.M.Q. Zaman and J.K. Foss.

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

  • Self-similar compressible free vortices [microform] / Karl von Ellenrieder.

    • Text
    • [Stanford, Calif.] : Joint Institute for Aeronautics and Acoustics, National Aeronautics and Space Administration, Ames Research Center : Joint Institute for Aeronautics and Acoustics, Stanford University ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998

  • Receptivity of flat-plate boundary layer in a non-uniform free stream (vorticity normal to the plate) [microform] : final report / M.N. Kogan ... [et al.].

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

  • Artificial boundary conditions for computation of oscillating external flows [microform] / S.V. Tsynkov.

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

  • Skin-friction measurements in a 3-D, supersonic shock-wave/boundary-layer interaction [microform] : 32nd Aerospace Sciences Meeting & Exhibit, January 10-13, 1994/Reno, NV / by Jeffrey K. Wideman ... [et al.].

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

  • Summary report of the orbital X-34 wing static aeroelastic study [microform] / Ramadas K. Prabhu ; prepared ... under contract NAS1-96014.

    • Text
    • Hampton, Va. : National Aeronautics and Science Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2001]
    • 2001

  • Hypersonic flows about a 25̊ sharp cone [microform] / James N. Moss.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Hanover MD : Available from NASA Center for AeroSpace Information (CASI), [2001]
    • 2001
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS27166

  • The unsteady laminar boundary layer on an axisymmetric body subject to small amplitude fluctuations in the free-stream velocity [microform] / Peter W. Duck.

    • 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, 1991]
    • 1991
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS59768

  • Separation characteristics of generic stores from lee side of an inclined flat plate at Mach 6 [microform] / Floyd J. Wilcox, Jr.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, VA : For sale by the National Technical Information Service, 1995]
    • 1995
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS60637

  • Jet vortex generators for turbulent flow separation control [microform] / by Gregory Selby.

    • Text
    • Norfolk, Va. : Old Dominion University Research Foundation ; Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS64231

  • A new methodology for free wake analysis using curved vortex elements [microform] / Donald B. Bliss, Milton E. Teske, and Todd R. Quackenbush.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.
    • 1987
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS67054

  • Free wake analysis of hover performance using a new influence coefficent method [microform] / Todd R. Quackenbush ... [et al.].

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1990.
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS67089

  • Demonstration of the feasibility of laser induced fluorescence for arc jet flow diagnostics [microform] / prepared by Sivaram Arepalli.

    • Text
    • Houston, Tex. : Lockheed Engineering and Sciences Company : Structures and Mechanics Division and Advanced Programs Office, National Aeronautics and Space Administration, Lyndon B. Johnson Space Center, [1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS71812

  • The effects of anisotropic free-stream turbulence on turbulent boundary layer behavior [microform] / Fang Liang-Wei, Jon A. Hoffman.

    • Text
    • [Moffett Field, Calif.] : National Aeronautics and Space Administration, Ames Research Center, [1985]
    • 1985

  • The effects of anisotropic free-stream turbulence on turbulent boundary layer behavior / Fang Liang-Wei, Jon A. Hoffman.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1985]
    • 1985
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo21937

  • Computational analyses of the LIMX TBCC inlet high-speed flowpath / Vance F. Dippold, III.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo25003

  • Research on supersonic inlet bleed / David O. David, Manan A. Vyas, and John W. Slater.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo32068

  • Interaction between Tollmien-Schlichting waves and free-stream disturbances in boundary-layer flows / R. J. Bodonyi.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, [1986]
    • 1986

  • Iodine Tagging Velocimetry and mechanism in the hypersonic near wake of a MultiPurpose Crew Vehicle / R. Jeffrey Balla.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, July 2013.
    • 2012-7
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo47609

  • Interaction between Tollmien-Schlichting waves and free-stream disturbances in boundary-layer flows / R. J. Bodonyi.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, 1986.
    • 1986
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo30303

  • Water tunnel flow visualization study through poststall of 12 novel planform shapes / Gregory M. Gatlin, Dan H. Neuhart.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, March 1996.
    • 1996-3
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo65353

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