Abstract The helicopter main rotor in forward flight is considered in this paper. The results for rigid blades and elastic blades are compared by the method of coupled simulation. The influence of the structural damping coefficient on the blade in-flight deformation is also considered.


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    Titel :

    Coupled CFD/CSD simulation of the helicopter main rotor in high-speed forward flight


    Beteiligte:
    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:

    Russian Aeronautics ; 60 , 2 ; 198-205


    Erscheinungsdatum :

    01.04.2017


    Format / Umfang :

    8 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Coupled CFD/CSD simulation of the helicopter main rotor in high-speed forward flight

    Dehaeze, F. / Barakos, G. N. / Garipova, L. I. et al. | Online Contents | 2017



    MULTIDISCIPLINARY COMPUTATIONAL ROTOR NOISE PREDICTION FOR HELICOPTER ROTOR IN HIGH-SPEED FORWARD FLIGHT

    Liu, Y. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2011


    A LOOSELY COUPLED CFD/CSD SIMULATION OF A HELICOPTER ROTOR IN FORWARD FLIGHT

    Sheng, C. / Ickes, J. / Narramore, J.C. et al. | British Library Conference Proceedings | 2013