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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    Title :

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


    Contributors:

    Published in:

    Russian Aeronautics ; 60 , 2 ; 198-205


    Publication date :

    2017-04-01


    Size :

    8 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English




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