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  1. 1
    Development of three-dimensional code for the analysis of jet mixing problem

    Development of three-dimensional code for the analysis of jet mixing problem by Abdol-Hamid, Khaled S. (Khaled Sayed), 1957-

    Washington, D.C., Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Division ; For sale by the National Technical Information Service, 1988
    Format: Government Document Book


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  2. 2
    Multistage schemes with multigrid for Euler and Navier-Stokes equations : components and analysis

    Multistage schemes with multigrid for Euler and Navier-Stokes equations : components and analysis by Swanson, R. Charles

    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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  3. 3
    Multigrid calculation of three-dimensional turbomachinery flows

    Multigrid calculation of three-dimensional turbomachinery flows by Caughey, D. A. (David A.)

    Ithaca, New York : [Washington, D.C.] : [Springfield, Va.] : Fluid Dynamics and Aerodynamics Program, Sibley School of Mechanical and Aerospace Engineering, Cornell University ; National Aeronautics and Space Administration ; [National Technical Information Service, distributor], 1989
    Format: Government Document Book


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  4. 4
    Streamwise vorticity generation in laminar and turbulent jets

    Streamwise vorticity generation in laminar and turbulent jets by Demuren, A. O.

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


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  5. 5
    Navier-Stokes calculations for a highly-twisted rotor near stall

    Navier-Stokes calculations for a highly-twisted rotor near stall by Yamauchi, Gloria K.

    [Washington, D.C.] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1994
    Format: Government Document Book


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  6. 6
    Turbulence model comparisons for a high-speed aircraft

    Turbulence model comparisons for a high-speed aircraft by Rivers, Melissa B.

    Hampton, Va. : Hanover, MD : Springfield, VA : National Aeronautics and Space Administration, Langley Research Center ; Available from NASA Center for AeroSpace Information ; National Technical Information Service [distributor], 1999
    Format: Government Document Book


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  7. 7
    Impact of periodic unsteadiness on performance and heat load in axial flow turbomachines

    Impact of periodic unsteadiness on performance and heat load in axial flow turbomachines

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


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  8. 8
    Solution-adaptive Cartesian cell approach for viscous and inviscid flows

    Solution-adaptive Cartesian cell approach for viscous and inviscid flows by Coirier, William J.

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


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  9. 9
    CMOTT turbulence module for NPARC : under cooperative agreement NCC3-520

    CMOTT turbulence module for NPARC : under cooperative agreement NCC3-520 by Zhu, J.

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


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  10. 10
    Euler technology assessment : SPLITFLOW code applications for stability and control analysis on an advanced fighter model employing innovative control concepts

    Euler technology assessment : SPLITFLOW code applications for stability and control analysis on an advanced fighter model employing innovative control concepts by Jordan, Keith J.

    Hampton, Va. : Springfield, VA : National Aeronautics and Space Administration, Langley Research Center ; National Technical Information Service, distributor, 1998
    Format: Government Document Book


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  11. 11
    Energy efficient engine low pressure subsystem flow analysis

    Energy efficient engine low pressure subsystem flow analysis

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


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  12. 12
    Methodology for sensitivity analysis, approximate analysis, and design optimization in CFD for multidisciplinary applications : progress report for the period April 15, 1992 to January 31, 1993

    Methodology for sensitivity analysis, approximate analysis, and design optimization in CFD for multidisciplinary applications : progress report for the period April 15, 1992 to Jan... by Taylor, Arthur C.

    Norfolk, Va. : [Washington, D.C.] : [Springfield, Va.] : Old Dominion University Research Foundation ; [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1993
    Format: Government Document Book


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  13. 13
    Computational investigation of flap-edges : final report, NASA award NCC-2-857

    Computational investigation of flap-edges : final report, NASA award NCC-2-857 by Cummings, Russell M. (Russell Mark)

    San Luis Obispo, CA : [Washington, DC] : [Springfield, Va.] : California Polytechnic State University ; [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1997
    Format: Government Document Book


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  14. 14
    Methodology for sensitivity analysis, approximate analysis, and design optimization in CFD for multidisciplinary applications : final report for the period ended December 31, 1995

    Methodology for sensitivity analysis, approximate analysis, and design optimization in CFD for multidisciplinary applications : final report for the period ended December 31, 1995 by Taylor, Arthur C.

    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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  15. 15
    Steady and unsteady three-dimensional transonic flow computations by integral equation method : final technical report

    Steady and unsteady three-dimensional transonic flow computations by integral equation method : final technical report by Hu, Hong, 1105-1155

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


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  16. 16
    Computation of asymmetric supersonic flows around cones at large incidence : final report

    Computation of asymmetric supersonic flows around cones at large incidence : final report by Degani, David

    Technion City, Haifa, Israel : [Washington, D.C.] : [Springfield, Va.] : Technion Research & Development Foundation ; [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1987
    Format: Government Document Book


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  17. 17
    Advanced Subsonic Technology (AST) Area of Interest (AOI) 6 : develop and validate aeroleastic codes for turbomachinery

    Advanced Subsonic Technology (AST) Area of Interest (AOI) 6 : develop and validate aeroleastic codes for turbomachinery

    [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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  18. 18
    Final technical report for Euler/Navier-Stokes solvers applied to ducted fan configurations : NASA grant number NAG3-1230 : grant duration, December 20, 1990 to December 20, 1996

    Final technical report for Euler/Navier-Stokes solvers applied to ducted fan configurations : NASA grant number NAG3-1230 : grant duration, December 20, 1990 to December 20, 1996 by Keith, Theo G.

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


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  19. 19
    Optimal control of thermally coupled Navier Stokes equations

    Optimal control of thermally coupled Navier Stokes equations by Ito, Kazufumi

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


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  20. 20
    Numerical simulation of complex turbomachinery flows

    Numerical simulation of complex turbomachinery flows by Chernobrovkin, A. A.

    [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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