A lifting surface theory has been developed for a helicopter rotor in forward flight for incompressible flow. The method utilized the concept of the linearized acceleration potential and make use of the vortex lattice procedures. Results in terms of lift coefficient slope for several forward flight conditions are given.


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    Title :

    Lifting surface theory for a helicopter rotor in forward flight


    Contributors:
    Runyan, H. L. (author) / Tai, H. (author)

    Publication date :

    1983-01-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :


    Non-linear helicopter rotor lifting surface theory

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    Free access