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  • A stable penalty method for the compressible Navier-Stokes equations. I., Open boundary conditions [microform] / J.S. Hesthaven, D. Gottlieb.

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

  • A fast numerical solution of scattering by a cylinder [microform] : spectral method for the boundary integral equations / Fang Q. Hu.

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

  • Numerical study of unsteady shockwave reflections using an upwind TVD scheme [microform] / Andrew T. Hsu and Meng-Sing Liou.

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

  • Control of oscillatory forces on a circular cylinder by rotation [microform] / Yuh-Roung Ou.

    • Text
    • Hampton, Va. : Institute for Computer Applications in Science and Enginering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1991]
    • 1991

  • The inviscid axisymmetric stability of the supersonic flow along a circular cylinder [microform] / Peter W. Duck.

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

  • Control of separated flow past a cylinder using tangential wall jet blowing [microform] / by Sejong Oh and Leonard Roberts.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1989]
    • 1989

  • Circular electrode geometry metal-semiconductors-metal photodetectors [microform] / inventors, James A. McAddo ... [et al.].

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

  • The influence of jet-grid turbulence on heat transfer from the stagnation region of a cylinder in crossflow [microform] / James E. O'Brien and G. James VanFossen, Jr.

    • Text
    • [Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center ; Springfield, Va. : National Technical Information Service, distributor, 1985]
    • 1985

  • Prediction of vortex shedding from circular and noncircular bodies in subsonic flow [microform] / Michael R. Mendenhall and Daniel J. Lesieutre.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space 16
    • 1986

  • Computation of sound generated by viscous flow over a circular cylinder [microform] / Jared S. Cox ... [et al.].

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

  • Drag reduction on circular cylinders by ejecting jet from rear stagnation region [microform] : progress report for the period ending June 30, 1997 ... under Cooperative Agreement NCC1-232 / by S. Atsuchi and S.N. Tiwari.

    • Text
    • Norfolk, Va. : Dept. of Mechanical Engineering, College of Engineering and Technology, Old Dominion University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Stability of capillary surfaces in rectangular containers [microform] : the right square cylinder / M.M. Weislogel and K.C. Hsieh.

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

  • 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

  • Optimal control of lift/drag ratios on a rotating cylinder [microform] / Yuh-roung Ou and John A. Burns.

    • Text
    • Hampton, Va. : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center : [Springfield, Va. : For sale by the National Technical Information Service, 1991]
    • 1991
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS59878

  • Modal ring method for the scattering of sound [microform] / Kenneth J. Baumeister and Kevin L. Kreider.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1993]
    • 1993
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS60633

  • SSME LOX post flow analysis/fluid structure interaction [microform]. Volume 1, Flow analysis : final report / by Roger W. Burke.

    • Text
    • Huntsville, AL : Lockheed Missiles and Space Co., Huntsville Engineering Center ; Marshall Space Flight Center, Ala. : National Aeronautics and Space Administration, George C. Marshall Space Flight Center ; [Springfieldl, Va. : National Technical Information Service, distributor, 1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS61869

  • Secondary frequencies in the wake of a circular cylinder with vortex shedding [microform] / Saul S. Abarbanel ... [et al.].

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS67941

  • SSME LOX post flow analysis/fluid structure interaction [microform] : final report.

    • Text
    • Huntsville, AL : Lockheed Missiles & Space Co. ; [Washington, D.C. : National Aeronautics and Space Administration, 1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS61869

  • Effect of a rotor wake on the local heat transfer on the forward half of a circular cylinder [microform] / Kim A. Morehouse and Robert J. Simoneau.

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

  • On the stability of the unsteady boundary layer on a cylinder oscillating transversely in a viscous fluid [microform] / Philip Hall.

    • Text
    • Hampton, Va. : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, [1983]
    • 1983

  • A Finite element-boundary integral method for cavities in a circular cylinder [microform] / Leo C. Kempel and J. L. Volakis.

    • Text
    • Ann Arbor, Mich. : University of Michigan, Radiation Laboratory, Dept. of Electrical Engineering and Computer Science ; Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1992]
    • 1992
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS97568

  • Effect of a rotor wake on heat transfer from a circular cylinder [microform] / Robert J. Simoneau, ... [et al.].

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

  • Heat transfer distributions around nominal ice accretion shapes formed on a cylinder in the NASA Lewis icing research tunnel [microform] / G. J. Van Fossen, ... [et al.].

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS98924

  • Investigation of the effects of pressure gradient, temperature, and wall temperature ratio on the stagnation point heat transfer for circular cylinders and gas turbine vanes [microform] / by H.T. Nagamatsu and R. E. Duffy.

    • Text
    • Troy, N.Y. : Rensselaer Polytechnic Institute, [1984]
    • 1984

  • Surface settling in partially filled containers upon step reduction in gravity / Mark M. Weislogel and Howard D. Ross.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, November 1990.
    • 1990-11

  • The evolution equations for Taylor vortices in the small gap limit / Philip Hall.

    • Text
    • Hampton, Va. : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, [1983]
    • 1983
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo29171

  • Buckling of structures : Symposium, Cambridge/USA, June 17-21, 1974 / editor, Bernard Budiansky.

    • Text
    • Berlin ; New York : Springer-Verlag, 1976.
    • 1976
    • 1 Item
    FormatCall NumberItem Location
    Text TA656.2.S95 1974Off-site

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