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  1. 1
    Combustion-acoustic stability analysis for premixed gas turbine combustors

    Combustion-acoustic stability analysis for premixed gas turbine combustors

    [Washington, D.C.] : [Springfield, Va.] : National Aeronautics and Space Administration ; [National Technical Information Service, distributor], 1995
    Format: Government Document Book


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  2. 2
    LTCP 2D graphical user interface : application description and user's guide

    LTCP 2D graphical user interface : application description and user's guide by Ball, Robert

    [Washington, DC] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1996
    Format: Government Document Book


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  3. 3
    An experimental study of characteristic combustion-driven flow for CFD validation : final report for NASA contract NAS8-38862

    An experimental study of characteristic combustion-driven flow for CFD validation : final report for NASA contract NAS8-38862 by Santoro, Robert J.

    [Washington, DC] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1997
    Format: Government Document Book


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  4. 4
    Planar imaging of hydroxyl in a high temperature, high pressure combustion facility

    Planar imaging of hydroxyl in a high temperature, high pressure combustion facility

    [Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration ; [National Technical Information Service, distributor], 1995
    Format: Government Document Book


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  5. 5
    Two-dimensional imaging og OH in a lean burning high combustor

    Two-dimensional imaging og OH in a lean burning high combustor

    [Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration ; [National Technical Information Service, distributor], 1995
    Format: Government Document Book


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  6. 6
    PDF methods for combustion in high-speed turbulent flows : second annual technical report

    PDF methods for combustion in high-speed turbulent flows : second annual technical report by Pope, S. B.

    [Washington, D.C.] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1995
    Format: Government Document Book


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  7. 7
    A unique, optically accessible flame tube facility for lean combustor studies

    A unique, optically accessible flame tube facility for lean combustor studies

    [Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration ; [National Technical Information Service, distributor], 1995
    Format: Government Document Book


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  8. 8
    Shock tunnel studies of scramjet phenomena 1994. Supplements 11 and 12

    Shock tunnel studies of scramjet phenomena 1994. Supplements 11 and 12 by Morgan, R. G.

    Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, 1997
    Format: Government Document Book


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  9. 9
    The interactions of a flame and its self-induced boundary layer

    The interactions of a flame and its self-induced boundary layer by Ott, James D.

    [Cleveland, Ohio] : [Springfield, Va.] : National Aeronautics and Space Administration, Glenn Research Center ; [National Technical Information Service, distributor], 1999
    Format: Government Document Book


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  10. 10
    Numerical simulation of shock-induced combustion past blunt bodies using shock-fitting technique : progress report for the period ended June 30, 1994

    Numerical simulation of shock-induced combustion past blunt bodies using shock-fitting technique : progress report for the period ended June 30, 1994 by Ahuja, J. K.

    Norfolk, Va. : [Washington, DC] : [Springfield, Va.] : Old Dominion University Research Foundation ; [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1994
    Format: Government Document Book


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  11. 11
    Advanced CFD methodology for fast transients encountered in nonlinear combustion instability problems : SBIR phase II final report (restricted circulation)

    Advanced CFD methodology for fast transients encountered in nonlinear combustion instability problems : SBIR phase II final report (restricted circulation)

    [Marshall Space Flight Center, Ala.] : [Springfield, Va.] : National Aeronautics and Space Administration, George C. Marshall Space Flight Center ; [National Technical Information Service, distributor], 1992
    Format: Government Document Book


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  12. 12
    Ignition dynamics of a laminar diffusion flame in the field of a vortex embedded in a shear flow

    Ignition dynamics of a laminar diffusion flame in the field of a vortex embedded in a shear flow by Macaraeg, Michele G.

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


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  13. 13
    Shock tunnel studies of scramjet phenomena 1995. Supplement 13

    Shock tunnel studies of scramjet phenomena 1995. Supplement 13 by Morgan, R. G.

    Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1997
    Format: Government Document Book


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  14. 14
    Simulations of turbulent mixing and reacting flows and their applications to turbulence modeling : semiannial progress report / Joel H. Ferziger, Brian J. Cantwell, principal investigators.

    Simulations of turbulent mixing and reacting flows and their applications to turbulence modeling : semiannial progress report / Joel H. Ferziger, Brian J. Cantwell, principal inves... by Ferziger, Joel H.

    [Washington, DC] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1986
    Format: Government Document Book


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  15. 15
    The mechanisms of flame holding in the wake of a bluff body

    The mechanisms of flame holding in the wake of a bluff body by Strehlow, Roger A.

    [Washington, D.C.] : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [National Technical Information Service, distributor], 1985
    Format: Government Document Book


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  16. 16
    Computational study of flow establishment in a ram accelerator

    Computational study of flow establishment in a ram accelerator by Yungster, S.

    [Cleveland, Ohio] : [Springfield, Va.] : National Aeronautics and Space Administration, Lewis Research Center, Institute for Computational Mechanics in Propulsion ; [National Technical Information Service, distributor], 1995
    Format: Government Document Book


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  17. 17
    Imaging of combustion species in a radially-staged gas turbine combustor

    Imaging of combustion species in a radially-staged gas turbine combustor

    [Washington, D.C.] : [Springfield, Va.] :; [Washington, D.C.] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1996
    Format: Government Document Book


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  18. 18
    A planar reacting shear layer system for the study of fluid dynamics-combustion interaction

    A planar reacting shear layer system for the study of fluid dynamics-combustion interaction

    [Washington, D.C.] : [St. Louis, Mo.] : [Springfield, Va.] :; [Washington, D.C.] : [St. Louis, Mo.] : [Springfield, Va. :] : NASA ; US Army Aviation Systems Command ; [For sale by the National Technical Information Service], 1990
    Format: Government Document Book


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  19. 19
    Achromatic emission velocity measurements in luminous flows

    Achromatic emission velocity measurements in luminous flows by Schneider, Samuel J.

    [Washington, D.C.] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1997
    Format: Government Document Book


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  20. 20
    Inviscid spatial stability of a compressible mixing layer. Part II, The flame sheet model

    Inviscid spatial stability of a compressible mixing layer. Part II, The flame sheet model by Jackson, Thomas L. (Thomas Luther), 1957-

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


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