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  • The structure and development of streamwise vortex arrays embedded in a turbulent boundary layer [microform] / Bruce J. Wendt and Isaac Greber and Warren R. Hingst.

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

  • Supersonic jet mixing enhancement by 'delta-tabs' [microform] / K.B.M.Q. Zaman and M.F. Reeder and M. Samimy.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1992]
    • 1992

  • Application of computational fluid dynamics to the study of vortex flow control for the management of inlet distortion [microform] / Bernhard H. Anderson and James Gibb.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1992]
    • 1992

  • On the receptivity problem for 0 (1) wavelength [microform] / Andrew P. Bassom, Philip Hall.

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

  • On the stabliity of nonlinear viscous vortices in three-dimensional boundary layers [microform] / Andrew P. Bassom, S.R. Otto.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1992]
    • 1992

  • Improving diffusing S-duct performance by secondary flow control [microform] / Bruce A. Reichert and Bruce J. Wendt.

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

  • A design strategy for the use of vortex generators to manage inlet-engine distortion using computational fluid dynamics [microform] / Bernhard H. Anderson and Ralph Levy.

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

  • Mars vertical axis wind machines [microform] : the design of a tornado vortex machine for use on Mars.

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

  • The effects of vortex ingestion on the flow in a diffusing S-DUCT [microform] / B.J. Wendt and B.A. Reichert.

    • 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

  • Measurements and modeling of flow structure in the wake of a low profile "wishbone" vortex generator [microform] / B.J. Wendt and W.R. Hingst.

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

  • Three dimensional compressible turbulent flow computations for a diffusing S-duct with/without vortex generators [microform] / by Soo-Yong Cho and Isaac Greber.

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

  • Experimental studies of vortex flows [microform] : final report, NASA grant NCC 2-294, report covering the period March 1984 - May 1988 / principal investigator, L. Roberts ; project leader, R. Mehta.

    • Text
    • Stanford, CA : Joint Institute for Aeronautics and Acoustics, Dept. of Aeronautics and Astronautics, Stanford University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1988]
    • 1988

  • Collected papers on wind turbine technology [microform] / David A. Spera, editor.

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

  • The decay of longitudinal vortices shed from airfoil vortex generators [microform] / Bruce J. Wendt, Bruce A. Reichert, Jeffry D. Foster.

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

  • A wind tunnel investigation of the effects of micro-vortex generators and Gurney flaps on the high-lift characteristics of a business jet wing [microform] / by Michelle Therese Martuccio.

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

  • 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

  • PARC3D calculations of the F/A-18A HARV inlet vortex generators [microform] / Steve D. Podleski.

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

  • 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

  • A computational-experimental development of vortex generator use for a transitioning S-diffuser [microform] / Bruce J. Wendt and Julianne C. Dudek.

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

  • 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

  • Spanwise spacing effects on the initial structure and decay of axial vortices [microform] : under contract NAS3-27377 / B.J. Wendt and B.A. Reichert.

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

  • Low-pressure turbine separation control [microform] : comparison with experimental data / Vijay K. Garg.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2002]
    • 2002
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS36070

  • Initial circulation and peak vorticity behavior of vortices shed from airfoil vortex generators [microform] / Bruce J. Wendt.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2001]
    • 2001
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS48268

  • Feasibility of generating an "artificial" burst in a turbulent boundary layer [microform] / Mohamed Gad-el-Hak.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.
    • 1986

  • Transient growth theory prediction of optimal placing of passive and active flow control devices for separation delay in LPT airfoils [microform] / Anatoli Tumin, David E. Ashpis.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center, [2003]
    • 2003

  • Low-pressure turbine separation control--comparison with experimental data [microform] / Vijay K. Garg.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; [Springfield, Va.. : For sale by the National Technical Information Service, 2002]
    • 2002
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS60165

  • 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

  • The effects of blade mounted vortex generators on the noise from a MOD-2 wind turbine generator [microform] / Harvey H. Hubbard and Kevin P. Shepherd.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1984]
    • 1984

  • Double-branched vortex generator [microform] / Elizabeth R. Cantwell, Russell V. Westphal, R.D. Mehta.

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

  • Numerical simulation of the tip vortex off a low-aspect-ratio wing at transonic speed [microform] / N.N. Mansour.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1984]
    • 1984

  • Vortex generating flow passage design for increased film-cooling effectiveness and surface coverage [microform] / S. Stephen Papell.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration, 1984]
    • 1984

  • Calibration of the NASA Glenn 8- by 6-foot supersonic wind tunnel (1996 and 1997 tests) / E. Allen Arrington.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
    • 2011
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo27462

  • Micro-ramp flow control for oblique shock interactions : comparisons of computational and experimental data / Stefanie M. Hirt, David B. Reich, Michael B. O'Connor.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo30949

  • Experimental study of boundary layer flow control using an array of ramp-shaped vortex generators / Stefanie M. Hirt, Khairul B.M.Q. Zaman, and Timothy J. Bencic.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo32070

  • A computational-experimental development of vortex generator use for a transitioning S-diffuser / Bruce J. Wendt and Julianne C. Dudek.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, November 1996.
    • 1996-11
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo70670

  • Boundary layer flow control by an array of ramp-shaped vortex generators / K. B. M. Q. Zaman, S. M. Hirt, and T .J. Bencic.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo28429

  • Experimental studies of low-pressure turbine flows and flow control : final report / Raplh J. Volino.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo37136

  • Flow control under low-pressure turbine conditions using pulsed jets : final report / Ralph J. Volino, Mounir B. Ibrahim.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo37222

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