Abstract In this paper, simulation is considered of flow around flapped rotor sections with a degree of freedom in the flap deflection angle. For steady state validation, comparisons one made of numerical results for the flow around a flapped wing with experimental data. Modelling of a blade section with an 1-DOF aeroelastic flap is also considered.


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    Titel :

    Simulation of flow around blade section with one degree of freedom aeroelastic flap


    Beteiligte:
    Steijl, R. (Autor:in) / Dehaeze, F. (Autor:in) / Barakos, G. N. (Autor:in) / Garipova, L. I. (Autor:in) / Kusyumov, A. N. (Autor:in) / Mikhailov, S. A. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    01.04.2015


    Format / Umfang :

    6 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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