TRANSEP Calculates flow field about low-speed single-element airfoil at high-angle-of-attack and high-lift conditions with massive boundary-layer separation. TRANSEP includes effects of weak viscous interactions and can be used for subsonic/transonic airfoil design and analysis. The approach used in TRANSEP is based on direct-inverse method and its ability to use either displacement surface or pressure as airfoil boundary condition.


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    Title :

    High-Lift Separated Flow About Airfoils


    Contributors:

    Published in:

    Publication date :

    1982-12-01



    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English


    Keywords :


    Computation of separated flow about airfoils

    De Matteis, P. / Dima, C. | British Library Conference Proceedings | 1993





    Application of Viscous-Inviscid Interaction Methods for a Separated Flow Calculation about Airfoils and High-Lift Systems

    Lyapunov, S. V. / Wolkov, A. V. / American Institute of Aeronautics and Astronautics et al. | British Library Conference Proceedings | 1996