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  • Analysis of aerospike plume induced base-heating environment [microform] / T.-S. Wang.

    • 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

  • Low speed analysis of mission adaptive flaps on a high speed civil transport configuration [microform] / Victor R. Lessard.

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

  • An experimental study of the flowfield on a semispan rectangular wing with a simulated glaze ice accretion [microform] / Abdollah Khodadoust.

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

  • Control of low-speed turbulent separated flow over a backward-facing ramp [microform] / by John C. Lin.

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

  • Effect of acoustic excitation on stalled flows over an airfoil [microform] / K.B.M.Q. Zama.

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

  • 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

  • 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 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

  • A study of the factors affecting boundary layer two-dimensionality in wind tunnels [microform] / by R.D. Mehta and P.H. Hoffmann.

    • Text
    • Stanford, CA : Stanford University, Dept. of Aeronautics and Astronautics : Joint Institute for Aeronautics and Acoustics ; [Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986

  • 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

  • 3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet [microform] / M. Mizukami and J.D. Saunders.

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

  • Control & reduction of unsteady pressure loads in separated shock wave turbulent boundary layer interaction [microform] : final report on NASA grant NAG 1-1471 for the period 01/09/93 through 01/01/95 / David S. Dolling and J.W. Barter.

    • Text
    • Austin, Tex. : Center for Aerodynamics Research, Dept. of Aerospace Engineering & Engineering Mechanics, University of Texas at Austin ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • 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

  • Development of a low-Reynolds number, nonlinear [kappa-epsilon] model for the reduced Navier-Stokes equations [microform] : a final technical report for NASA-LeRC grant NAG-1781 / David A. Boger, T.R. Govindan, and Henry McDonald.

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

  • Final report on study of organized structures in the post-stall flow over wings [microform] / Steven Yon; Joseph Katz, principal investigator; James Ross, principal investigator.

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

  • 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

  • Experimental and computational investigation of lift-enhancing tabs on a multi-element airfoil [microform] / Dale Ashby.

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

  • Laser anemometer measurements of the flow field in a 4:1 pressure ratio centrifugal impeller [microform] / G.J. Skoch ... [et al.].

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

  • Experimental study of saddle point of attachment in laminar juncture flow [microform] / Michael D. Coon and Murray Tobak.

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

  • Study of boundary layer development in a two-stage low-pressure turbine [microform] / Daniel J. Dorney ... [et al.].

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

  • Experimental study of boundary layer behavior in a simulated low pressure turbine [microform] / Rickey J. Shyne.

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

  • The three dimensional flow field at the exit of an axial-flow turbine rotor [microform] / B. Lakshminarayana, D. Ristic, and S. Chu.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; Springfield, VA : National Technical Information Service [distributor, 1998]
    • 1998

  • Effects of convoluted divergent flap contouring on the performance of a fixed-geometry nonaxisymmetric exhaust nozzle [microform] / Scott C. Asbury and Craig A. Hunter.

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

  • Implementation and validation of the Chien k-[epsilon] turbulence model in the Wind Navier-Stokes code [microform] / Dennis A. Yoder and Nicholas J. Georgiadis.

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

  • Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method [microform] : EUROMECH-Colloquium 349, simulation of fluid-structure interaction in aeronautics, Göttingen, Germany, September 16-18, 1996 / John W. Edwards.

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

  • Investigation of flow separation in a transonic-fan linear cascade using visualization methods [microform] / Jan Lepicovsky ... [et al.].

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Springfield, VA : National Technical Information Service, distributor, [2000]
    • 2000

  • Closed-loop separation control using oscillatory flow excitation [microform] / Brian G. Allan ... [et al.] ; [prepared for ... under contract NAS1-97046].

    • Text
    • Hampton, Va. : ICASE, National Aeronautics and Science Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2000]
    • 2000

  • Enhanced design of turbo-jet LPT by separation control using phased plasma actuators [microform] / Thomas C. Corke and Flint O. Thomas.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Administration ; Springfield, VA : National Technical Information Service [distributor, 2003]
    • 2003
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS55124

  • Demonstration of separation delay with glow-discharge plasma actuators [microform] / Lennart S. Hultgren and David E. Ashpis.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, Md. : Available from the NASA Center for Aerospace Information ; Springfield, VA : National Technical Information Service [distributor, 2003]
    • 2003
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS55252

  • Some observations on transitory stall in conical diffusers [microform] / K.B.M.Q. Zaman and M.D. Dahl.

    • Text
    • Cleveland, Ohio : Lewis Research Center, [1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS58502

  • Flow separation in shock wave boundary layer interactions at hypersonic speeds [microform] / A. Hamed.

    • 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/LPS61576

  • 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

  • Experimental parametric study of jet vortex generators for flow separation control [microform] / by Gregory Selby.

    • Text
    • Norfolk, Va. : Old Dominion University Research Foundation, [1991]
    • 1991
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS65621

  • Control of flow separation and mixing by aerodynamic excitation [microform] / Edward J. Rice and John M. Abbott ; prepared for the 17th Congress of the International Council of Aeronautical Sciences sponsored by the American Institute of Aeronautics and Astronautics, Stockholm, Sweden, September 9-14, 1990.

    • Text
    • [Washington, D.C.] : NASA ; [Springfield, Va. : For sale by the National Technical Information Service, 1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS67478

  • Unsteady three-dimensional marginal separation, including breakdown [microform] / Peter W. Duck.

    • Text
    • [Washington, D.C.] : NASA ; [Cleveland, Ohio] : Institute for Computational Mechanics in Propulsion, NASA Lewis Research Center, Case Western Reserve University ; [Springfield, Va. : For sale by the National Technical Information Service, 1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS67526

  • Computation of Navier-Stokes equations for three-dimensional flow separation [microform] / Ching-Mao Hung.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS70413

  • Simulation of glancing shock wave and boundary layer interaction [microform] / Ching-Mao Hung.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS73542

  • Numerical approach for the aerodynamic analysis of airfoils with laminar separation [microform] / prepared by David W. Halt and Dean R. Bristow.

    • Text
    • St. Louis, Mo. : McDonnel Douglas Corporation, McDonnel Aircraft Company ; Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1985]
    • 1985

  • Physics of forced unsteady separation [microform] : proceedings of a NASA/AFOSR/ARO workshop held at NASA Ames Research Center, Moffett Field, California, April 17-19, 1990 / edited by L.W. Carr.

    • Text
    • Moffett Field, Calif. : Ames Research Center, 1992.
    • 1992
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS93577

  • 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

  • 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

  • Investigation of materials for boundary layer control in a supersonic wind tunnel / Alexander C. Braafladt, John M. Lucero and Stefanie M. Hirt.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, November 2013.
    • 2013-11
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo50546

  • A computational study for the utilization of jet pulsations in gas turbine film cooling and flow control / Olga V. Kartuzova.

    • Text
    • Cleveland, Ohio : Cleveland State University : National Aeronautics and Space Administration, Glenn Research Center, September 2012.
    • 2012-9
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo53818

  • Computational aerodynamic simulations of a 1484 ft/sec tip speed quiet high-speed fan system model for acoustic methods assessment and development / Daniel L. Tweedt.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, October 2014.
    • 2014-10
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo55842

  • Supersonic retropropulsion test 1853 in NASA LaRC Unitary Plan Wind Tunnel test section 2 / Scott A. Berry and Matthew N. Rhode.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, April 2014.
    • 2014-4
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo54425

  • On parametric sensitivity of Reynolds-averaged Navier-Stokes SST turbulence model : 2D hypersonic shock-wave boundary-layer interactions / James L. Brown.

    • Text
    • Moffett Field, CA : National Aeronautics and Space Administration, Ames Research Center, May 2014.
    • 2014-5
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo65203

  • Guide to AERO2S and WINGDES computer codes for prediction and minimization of drag due to lift / Harry W. Carlson [and three others].

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, November 1997.
    • 1997-11
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo63076

  • Passive rocket diffuser testing : reacting flow performance of four second-throat geometries / Daniel R. Jones, Daniel C. Allgood, Grady P. Saunders.

    • Text
    • [Stennis Space Center, Mississippi] : National Aeronautics and Space Administration, [Stennis Space Center], December 2016.
    • 2016-12
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo78205

  • Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method / John W. Edwards.

    • Text
    • [Washington, DC] : [National Aeronautics and Space Administration], [1996]
    • 1996
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo78886

  • Evaluation of full Reynolds stress turbulence models in FUN3D / Julianne C. Dudek, Jan-Renee Carlson.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, September 2017.
    • 2017-9
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo85654

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