Distributive loading rotational theory for helicopter rotor noise generation, considering steady and fluctuating force radiation and impulsive blade slap


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    Title :

    Helicopter rotor noise generation.


    Contributors:

    Conference:

    AERODYNAMICS OF ROTARY WING AND V/STOL AIRCRAFT, SYMPOSIUM ; 1969 ; BUFFALO, NY


    Publication date :

    1969-01-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English


    Keywords :


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