Abstract Flows around rotor blade sections equipped with active flaps with a degree of freedom in the flap deflection angle are considered in this paper. Results for oscillating flaps are presented. The resultant flap motion was found to couple with the unsteady air loads for cases of blade section in oscillatory translation.


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    Titel :

    Simulation of flow around oscillating rotor blade section with 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 :

    2015-10-01


    Format / Umfang :

    7 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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