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  1. 1
    Development of an automatic block generation algorithm : final report

    Development of an automatic block generation algorithm : final report by Eberhardt, D. Scott

    [Seattle, Wash.] : [Washington, DC] : [Springfield, Va.] : [University of Washington] ; [National Aeronautics and Space Administration] ; [For sale by the National Technical Information Service], 1995
    Format: Government Document Book


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  2. 2
    Aerostructural vortical flow interactions with applications to F/A-18 and F-117 tail buffet

    Aerostructural vortical flow interactions with applications to F/A-18 and F-117 tail buffet by Kandil, Osama A.

    [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
    Computation of flow over a drag prediction workshop wing/body transport configuration using CFL3D

    Computation of flow over a drag prediction workshop wing/body transport configuration using CFL3D by Rumsey, C. L. (Christopher Lockwood), 1961-

    Hampton, Va. : Hanover Md. :; Hampton, Va. : Hanover MD : National Aeronautics and Space Administration, Langley Research Center ; Available from NASA Center for AeroSpace Information (CASI), 2001
    Format: Government Document Book


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  4. 4
    Coarse grid modeling of turbine film cooling flows using volumetric source terms

    Coarse grid modeling of turbine film cooling flows using volumetric source terms by Heidmann, James D.

    [Cleveland, Ohio] : Hanover, MD :; [Cleveland, Ohio] : Hanover, MD : National Aeronautics and Space Administration, Glenn Research Center ; Available from NASA Center for Aerospace Information, 2001
    Format: Government Document Book


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  5. 5
    Plane smoothers for multiblock grids : computational aspects

    Plane smoothers for multiblock grids : computational aspects by Llorente, Ignacio M.

    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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  6. 6
    Calculation of multistage turbomachinery using steady characteristic boundary conditions

    Calculation of multistage turbomachinery using steady characteristic boundary conditions by Chima, Rodrick V.

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


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  7. 7
    Some approaches towards constructing optimally efficient multigrid solvers for the inviscid flow equations

    Some approaches towards constructing optimally efficient multigrid solvers for the inviscid flow equations by Sidilkover, D.

    Hampton, VA : [Springfield, Va.] : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [National Technical Information Service, distributor], 1997
    Format: Government Document Book


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  8. 8
    Numerical solution of the full potential equation using a chimera grid approach

    Numerical solution of the full potential equation using a chimera grid approach by Holst, Terry L.

    Moffett Field, Calif. : [Springfield, Va.] : National Aeronautics and Space Administration, Ames Research Center ; [National Technical Information Service, distributor], 1995
    Format: Government Document Book


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  9. 9
    On automating domain connectivity for overset grids : final report for NASA grant 2-783 submitted to NASA Ames Research Center, Advanced Design Cycle Branch

    On automating domain connectivity for overset grids : final report for NASA grant 2-783 submitted to NASA Ames Research Center, Advanced Design Cycle Branch by Chiu, Ing-Tsau

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


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  10. 10
    Heat transfer on a film-cooled rotating blade

    Heat transfer on a film-cooled rotating blade by Garg, Vijay K.

    [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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  11. 11
    A note on multi-block relaxation schemes for multigrid solvers

    A note on multi-block relaxation schemes for multigrid solvers by Jones, Jim E.

    Hampton, VA : [Springfield, Va.] : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [National Technical Information Service, distributor], 1997
    Format: Government Document Book


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  12. 12
    Multigrid methods for aerodynamic problems in complex geometries : final report

    Multigrid methods for aerodynamic problems in complex geometries : final report by Caughey, D. A. (David A.)

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


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