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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    Title :

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


    Contributors:

    Published in:

    Publication date :

    2015-04-01


    Size :

    6 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English




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