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  1. 1
    Preprocessor that enables the use of GridPro grids for unsteady Reynolds-averaged Navier-Stokes code TURBO /
    by Shyam, Vikram
    Published 2010
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    Government Document eBook
  2. 2
    A three-dimensional unsteady CFD model of compressor stability /
    by Chima, Rodrick V.
    Published 2006
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    Government Document Conference Proceeding eBook
  3. 3
    Harmonic balance computations of fan aeroelastic stability /
    by Bakhle, Milind A.
    Published 2010
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    Government Document Conference Proceeding eBook
  4. 4
    LES of a jet excited by the Localized Arc Filament Plasma Actuators /
    by Brown, Clifford A.
    Published 2011
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    Government Document Conference Proceeding eBook
  5. 5
    An experimental study of airfoil-spoiler aerodynamics /
    by McLachlan, Blair G.
    Published 1984
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    Government Document eBook
  6. 6
    Flow control under low-pressure turbine conditions using pulsed jets : final report /
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    Government Document eBook
  7. 7
    Structure of the small amplitude motion on transversely sheared mean flows /
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    Government Document eBook
  8. 8
    Time-filtered Navier-Stokes approach and emulation of turbulence-chemistry interaction /
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    Government Document Conference Proceeding eBook
  9. 9
    Experimental investigation of unsteady flows at large incidence angles in a linear oscillating cascade /
    by Buffum, Daniel H.
    Published 1996
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    Government Document eBook
  10. 10
    Computation of sound generated by viscous flow over a circular cylinder /
    by Cox, Jared S.
    Published 1997
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    Government Document eBook
  11. 11
    On the physics of flow separation along a low pressure turbine blade under unsteady flow conditions /
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    Government Document eBook
  12. 12
    Investigation of unsteady pressure-sensitive paint (uPSP) and a dynamic loads balance to predict launch vehicle buffet environments /
    by Schuster, D. M. (David M.)
    Published 2016
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    Government Document eBook
  13. 13
    Characterization of cavity flow fields using pressure data obtained in the Langley 0.3-meter transonic cryogenic tunnel /
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    Government Document eBook
  14. 14
    Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method /
    by Edwards, John W.
    Published 1996
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    Government Document eBook
  15. 15
    A simplified model for the investigation of acoustically driven combustion instabilities /
    by Quinn, D. Dane, Paxson, Daniel E.
    Published 1998
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    Government Document eBook
  16. 16
    Comparison of experimental and theoretical turbulence reduction characteristics for screens, honeycomb, and honeycomb-screen combinations /
    by Scheiman, James
    Published 1981
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    Government Document eBook
  17. 17
    A moving grid capability for NPARC /
    by Slater, John W.
    Published 1998
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    Government Document eBook
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