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  1. 1
    The kinetic nonequilibrium processes in the internal flow and in the plume of subsonic and supersonic aircrafts : summary of research, from August 28, 1996 to August 28, 1997, NAG3-1957

    The kinetic nonequilibrium processes in the internal flow and in the plume of subsonic and supersonic aircrafts : summary of research, from August 28, 1996 to August 28, 1997, NAG3... by Starik, A. M. (Alexander M.)

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


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  2. 2
    The acoustic characteristics of turbomachinery cavities

    The acoustic characteristics of turbomachinery cavities

    [MSFC, Ala.] : [Springfield, Va.] : National Aeronautics and Space Administration, Marshall Space Flight Center ; [National Technical Information Service, distributor], 1995
    Format: Government Document Book


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  3. 3
    Variational methods in sensitivity analysis and optimization for aerodynamic applications : progress report for the period ended June 30, 1996 ... under research grant NCC1-68

    Variational methods in sensitivity analysis and optimization for aerodynamic applications : progress report for the period ended June 30, 1996 ... under research grant NCC1-68 by Ibrahim, A. H.

    Norfolk , Va. : [Washington, DC] : [Springfield, Va.] : Dept. of Mechanical Engineering, College of Engineering & Technology, Old Dominion University ; [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1996
    Format: Government Document Book


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  4. 4
    Supersonic reacting internal flow fields

    Supersonic reacting internal flow fields by Drummond, J. Philip

    [Washington, D.C.?] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1990
    Format: Government Document Book


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  5. 5
    A general fluid system simulation program to model secondary flows in turbomachinery

    A general fluid system simulation program to model secondary flows in turbomachinery by Majumdar, Alok K.

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


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  6. 6
    SRM internal flow test and computational fluid dynamic analyses : final report : contract NAS8-39095

    SRM internal flow test and computational fluid dynamic analyses : final report : contract NAS8-39095

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


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  7. 7
    Laser doppler velocimeter system for subsonic jet mixer nozzle testing at the NASA Lewis Aeroacoustic Propulsion Lab

    Laser doppler velocimeter system for subsonic jet mixer nozzle testing at the NASA Lewis Aeroacoustic Propulsion Lab

    [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
    Calculations of diffuser flows with an anisotropic K-[epsilon] model

    Calculations of diffuser flows with an anisotropic K-[epsilon] model by Zhu, Jieping

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


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  9. 9
    Comparison of numerical results and multicavity purge and rim seal data with extensions to dynamics

    Comparison of numerical results and multicavity purge and rim seal data with extensions to dynamics

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


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  10. 10
    Heat transfer computations of internal duct flows with combined hydraulic and thermal developing length

    Heat transfer computations of internal duct flows with combined hydraulic and thermal developing length

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


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  11. 11
    Application of thin-film thermocouples to localized heat transfer measurements

    Application of thin-film thermocouples to localized heat transfer measurements by Lepicovsky, J.

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


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  12. 12
    Contribution to the optimal shape design of two-dimensional internal flows with embedded shocks

    Contribution to the optimal shape design of two-dimensional internal flows with embedded shocks by Iollo, Angelo

    Hampton, VA : [Springfield, Va.] : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [National Technical Information Service, distributor], 1995
    Format: Government Document Book


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  13. 13
    Analysis of internal flow in a ventral nozzle for STOVL aircraft

    Analysis of internal flow in a ventral nozzle for STOVL aircraft by Smith, C. Frederic

    [Washington, D.C.] : [Springfield, Va.] :; [Washington, D.C.] : [Springfield, Va. :] : NASA ; [For sale by the National Technical Information Service], 1990
    Format: Government Document Book


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  14. 14
    Internal aerodynamics of a generic three-dimensional scramjet inlet at Mach 10

    Internal aerodynamics of a generic three-dimensional scramjet inlet at Mach 10 by Holland, Scott D.

    Hampton, Va. : Linthicum Heights, Md. : Springfield, Va. : National Aeronautics and Space Administration, Langley Research Center ; NASA Center for AeroSpace Information, distributor ; National Technical Information Service, distributor, 1995
    Format: Government Document Book


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  15. 15
    Euler flow computations on non-matching unstructured meshes

    Euler flow computations on non-matching unstructured meshes by Gumaste, Udayan

    [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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  16. 16
    NASA low-speed axial compressor for fundamental research

    NASA low-speed axial compressor for fundamental research by Wasserbauer, Charles A.

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


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  17. 17
    Computations of viscous flows in complex geometries using multiblock grid systems

    Computations of viscous flows in complex geometries using multiblock grid systems by Steinthorsson, Erlendur

    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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  18. 18
    A root-mean-square pressure fluctuations model for internal flow applications

    A root-mean-square pressure fluctuations model for internal flow applications by Chen, Y. S.

    [Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1985
    Format: Government Document Book


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  19. 19
    PSP measurement of stator vane surface pressures in a high speed fan

    PSP measurement of stator vane surface pressures in a high speed fan by Lepicovsky, Jan

    [Cleveland, Ohio] : [Springfield, Va.] : National Aeronautics and Space Administration, Lewis Research Center ; [National Technical Information Service, distributor], 1998
    Format: Government Document Book


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  20. 20
    Static investigation of a multiaxis thrust-vectoring nozzle with variable internal contouring ability

    Static investigation of a multiaxis thrust-vectoring nozzle with variable internal contouring ability by Wing, David J.

    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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