This paper presents an Unstructured Navier-Stokes Analysis of Full TCA (Technology Concept Airplane) Configuration. The topics include: 1) Motivation; 2) Milestone and approach; 3) Overview of the unstructured-grid system; 4) Results on full TCA W/B/N/D/E configuration; 5) Concluding remarks; and 6) Future directions.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Unstructured Navier-Stokes Analysis of Full TCA Configuration


    Contributors:


    Publication date :

    1999-12-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English


    Keywords :


    Finite element Navier-Stokes solver for unstructured grids

    MARCUM, D. L. / AGARWAL, R. K. | AIAA | 1992


    Discrete Adjoint Method for Unstructured Navier-Stokes Solver

    Kim, H.-J. / Nakahashi, K. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2005


    Adaptive unstructured Navier-Stokes solver on the CM5

    Lau, Hin-Fan / Knight, Doyle | AIAA | 1996


    Adaptive Unstructured Navier-Stokes Solver on the CM5

    Lau, H.-F. / Knight, D. D. / AIAA | British Library Conference Proceedings | 1996


    "Large-Scale Parallel Unstructured Navier-Stokes Analysis for Aerodynamic Configurations"

    Mavriplis, D. J. / Canadian Aeronautics and Space Institute | British Library Conference Proceedings | 1999