PANAIR uses high-order panel method to predict inviscid subsonic or supersonic flows about arbitrary configuration. Panel method solves linear partial differential equation numerically by approximating configuration surface with panels on which unknown "singularity strengths" are defined. PANAIR includes advanced software technology as well as advanced aerodynamic technology.


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    Title :

    Higher-Order Panel Method for Aerodynamic Flow Analysis


    Contributors:
    Erickson, L. (author) / Carmichael, R. L. (author) / Levin, A. D. (author) / Magnus, A. (author) / Epton, M. (author) / Baruah, P. (author) / Massena, B. (author) / Bussoletti, J. (author) / Sidwell, K. (author) / Johnson, F. (author)

    Published in:

    Publication date :

    1982-12-01



    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English


    Keywords :


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