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  • Second order modeling of boundary-free turbulent shear flows [microform] / T.-H. Shih, J.-Y. Chen, and J.L. Limley.

    • Text
    • Cleveland, Ohio : NASA Lewis Research Center, Institute for Computational Mechanics in Propulsion ; [Springfield, Va. : National Technical Information Service, distributor, 1991]
    • 1991

  • Analytical investigation of rotor wake formation and geometry [microform] : progress report for NASA grant NAG-2-275 for period April 15, 1985 - October 15, 1985 / Rene Miller, co-principal investigators, Earll M. Murrman, co-principal investigator.

    • Text
    • Cambridge, Mass. : Dept. of Aeronautics and Astronautics, Massachusetts Institute of Technology ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986

  • Experimental analyses of trailing edge flows [microform] : final technical report to NASA Ames Research Center / S.L. Petrie, D.S. Emmer.

    • Text
    • [Moffett Field, Calif.] : The Center ; [Springfield, Va. : National Technical Information Service, distributor, 1986?]
    • 1986

  • Prediction and control of vortex-dominated and vortex-wake flows [microform] : final report for the period December 1, 1993 through December 1, 1995 / by Osama Kandil, principal investigator.

    • Text
    • Norfolk, Va. : Old Dominion University Research Foundation ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Direct numerical simulation of a temporally evolving incompressible plane wake [microform] : effect of initial conditions on evolution and topology / R. Sondergaard, B. Cantwell, and N. Mansour.

    • Text
    • Stanford, CA : Joint Institute for Aeronautics and Acoustics ; [Moffett Field, Calif.] : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • The spectral and statistical properties of turbulence generated by a vortex/blade-tip interaction [microform] : final technical report ... / William J. Devenport, principal investigator; Kenneth S. Wittmer; Christian W. Wenger.

    • Text
    • Blacksburg, VA : Dept. of Aerospace and Ocean Engineering, Virginia Polytechnic Institute and State University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Spatial characteristics of the unsteady differential pressures on 16% F/A-18 vertical tails [microform] : 36th Aerospace Sciences meeting & exhibit : January 12-15, 1998/Reno, NV / Robert W. Moses, Holt Ashley.

    • 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

  • Radar reflectivity in wingtip-generated wake vortices [microform] / Robert E. Marshall, Ashok Mudukutore, and Vicki L.H. Wissel.

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

  • Far-field turbulent vortex-wake/exhaust plume interaction for subsonic and HSCT airplanes [microform] : 27th AIAA Fluid Dynamics Conference, June 17-20, 1996/New Orleans, LA / Osama A. Kandil, Ihab Adam and Tin-Chee Wong.

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

  • Direct numerical simulation of weakly stratified turbulent wake / J.A. Redford, T.S. Lund, Gary N. Coleman.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, September 2014.
    • 2014-9
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo54987

  • On the physics of flow separation along a low pressure turbine blade under unsteady flow conditions / Meinhard T. Schobeiri and Burak Öztürk, David E. Ashpis.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, June 2003.
    • 2003-6
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo81200

  • Intermittency and cessation of vortex shedding in the wake of a thin flat plate with a circular trailing edge / Man Mohan Rai.

    • Text
    • Moffett Field, California : National Aeronautics and Space Administration, Ames Research Center, August 2018.
    • 2018-8
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo111056

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