Measurements in wind tunnel yield data for validation of computations. Report describes experimental investigation of three-dimensional interaction of helicopter rotor blade with vortex like that generated by preceeding rotor blade. Provides theoretical aerodynamicists with data for validation of computer simulations of aerodynamic flow.


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    Title :

    Interaction Of A Helicopter Blade With A Vortex


    Contributors:

    Published in:

    Publication date :

    1989-09-01



    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English


    Keywords :


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