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    Title :

    Discrete Vortex Method for Simulating Unsteady Flow Around Pitching Aerofoils



    Published in:

    Publication date :

    1997



    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English



    Classification :

    BKL:    50.93 / 55.50 Luftfahrzeugtechnik / 50.93 Weltraumforschung / 55.60 Raumfahrttechnik / 55.50 / 55.60
    Local classification TIB:    770/7040



    Discrete vortex method for simulating unsteady flow around pitching aerofoils

    Lin, H. / Vezza, M. / Galbraith, R.A.McD. | Tema Archive | 1997


    A Pure Vortex Method for Simulating Unsteady, Incompressible, Separated Flows Around Static and Pitching Aerofoils

    Lin, H. Q. / Vezza, M. / American Institute of Aeronautics and Astronautics et al. | British Library Conference Proceedings | 1996



    Discrete Vortex Method for Simulating Unsteady Flow

    Hequan Lin / Marco Vezza / R. A. Mcd. Galbraith | AIAA | 1997


    Mechanism of Vortex Perturbation via Unsteady Pitching

    Strangfeld, Christoph / Nayeri, Christian N. / Paschereit, Christian O. et al. | AIAA | 2018