The CFL3D/CFL3DE CFD codes and the industrial use status of the codes are outlined. Comparison of grid density, pressure, heat transfer, and aerodynamic coefficience are presented. Future plans related to the National Aerospace Plane Program are briefly outlined.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Hypersonic Cfd Applications at NASA Langley Using CFL3D and CFL3DE


    Contributors:

    Publication date :

    1989


    Size :

    16 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





    NASA Langley Aerothermodynamics Laboratory: Hypersonic Testing Capabilities

    Berger, Karen T. / Hollingsworth, Kevin E. / Wright, Shelia A. et al. | AIAA | 2015


    NASA Langley Aerothermodynamics Laboratory: Hypersonic Testing Capabilities

    Karen Berger / Shann Rufer / Kevin Hollingsworth et al. | NTRS


    NASA Langley Aerothermodynamics Laboratory: Hypersonic Testing Capabilities

    K. Berger / S. Rufer / K. Hollingsworth et al. | NTIS | 2022


    Compendium of NASA Langley Reports on Hypersonic Aerodynamics

    F. E. Sabo / A. M. Cary / S. W. Lawson | NTIS | 1987