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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

  • Hot film wall shear instrumentation for boundary layer transition research [microform] / Steven P. Schneider.

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

  • Turbulence modeling of free shear layers for high performance aircraft [microform] / Douglas Sondak.

    • Text
    • San Jose, CA : MCAT Institute ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1993]
    • 1993

  • Hypersonic turbulent boundary-layer and free shear database [microform] / Gary S. Settles and Lori J. Dodson.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1993]
    • 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

  • Transverse vorticity measurements using an array of four hot-wire probes [microform] / John F. Foss, Casey L. Klewicki, and Peter J. Disimile.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986

  • Enhanced mixing of an axisymmetric jet by aerodynamic excitation [microform] / Ganesh Raman.

    • Text
    • Cleveland, Ohio : Lewis Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1986]
    • 1986

  • Aerodynamics of seeing on large transport aircraft [microform] : progress report, December 1, 1985 through May 31, 1986 / by William C. Rose.

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

  • Grid resolution and turbulent inflow boundary condition recommendations for NPARC calculations [microform] / Nicholas J. Georgiadis and Julianne C. Dudek and Thomas P. Tierney.

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

  • Effect of density gradients in confined supersonic shear layers [microform] / Oshin Peroomian and R.E. Kelly.

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

  • Rotor vortex filaments [microform] : living on the slipstream's edge / Larry A. Young.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 199 ]
    • 1997

  • Wave number selection for incompressible parallel jet flows periodic in space [microform] / Jeffrey Hilton Miles.

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

  • Performance of low dissipative high order shock-capturing schemes for shock-turbulence interactions [microform] / N.D. Sandham and H.C. Yee.

    • Text
    • [Moffett Field, Calif.] : Research Institute for Advanced Computer Science, NASA Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998

  • Noise from supersonic coaxial jets. Part 3, Inverted velocity profile [microform] / M.D. Dahl and P.J. Morris.

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

  • Mixing enhancement by tabs in round supersonic jets [microform] / John M. Seiner, C.E. Grosch.

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

  • Comparison of several numerical methods for simulation of compressible shear layers [microform] / Christopher A. Kennedy, Mark H. Carpenter.

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

  • A reduced order model of the linearized incompressible Navier-Strokes equations for the sensor/actuator placement problem [microform] / Brian G. Allan.

    • Text
    • Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [2000]
    • 2000

  • The effects of forcing on a single stream shear layer and its parent boundary layer [microform] / prepared by Richard C. Haw, John F. Foss.

    • Text
    • East Lansing, MI : College of Engineering, Michigan State University, [1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS67980

  • 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

  • The stability of two-dimensional wakes and shear-layers at high Mach numbers [microform] / D.T. Papageorgiou.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS69039

  • A planar reacting shear layer system for the study of fluid dynamics-combustion interaction [microform] / C.J. Marek ... [et al.] ; prepared for the 23rd International Symposium on Combustion sponsored by the Combustion Institute, University of Orléans, France, July 22-27, 1990.

    • Text
    • [Washington, D.C.] : NASA ; [St. Louis, Mo.] : US Army Aviation Systems Command ; [Springfield, Va. : For sale by the National Technical Information Service, 1990?]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS70057

  • On the interaction of a sound pulse with the shear layer of an axisymmetric jet. III. Nonlinear effects [microform] / Alvin Bayliss, Lucio Maestrello, Eli Turkel.

    • Text
    • Hampton, Va. : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, [1985]
    • 1985

  • Calculation of reattaching shear layers in divergent channel with a multiple-time-scale turbulence model [microform] / S.-W. Kim.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration ; Cleveland, Ohio : Lewis Research Center, Institute for Computational Mechanics in Propulsion, [1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS108069

  • Shear layer excitation, experiment versus theory [microform] / Dietrich W. Bechert and Bernhard Stahl.

    • Text
    • Cleveland, Ohio : NASA Lewis Research Center ; Gèottingen, Germany : Institut fèur Experimentelle Strèomungsmechanik, [1984]
    • 1984

  • Design and calibration of the mixing layer and wind tunnel / by James H. Bell and Rabindra D. Mehta.

    • Text
    • [Stanford, CA] : Joint Institute for Aeronautics and Acoustics, National Aeronautics and Space Administration, Ames Research Center, Stanford University, [1989]
    • 1989
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo30612

  • Design and calibration of the mixing layer and wind tunnel [microform] / by James H. Bell and Rabindra D. Mehta.

    • Text
    • [Stanford, CA] : Joint Institute for Aeronautics and Acoustics, National Aeronautics and Space Administration, Ames Research Center, Stanford University, [1989]
    • 1989

  • Comparison of high-order and low-order methods for large-eddy simulation of a compressible shear layer / Mina R. Mankbadi, Nicholas J. Georgiadis, and James R. DeBonis.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, June 2015.
    • 2015-6
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo64049

  • Wave number selection for incompressible parallel jet flows periodic in space / Jeffrey Hilton Miles.

    • Text
    • Cleveland, OH : National Aeronautics and Space Administration, Lewis Research Center, June 1997.
    • 1997-6
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo72625

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