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    Title :

    AIAA-2019-2823: A Hybrid Blade Element Momentum Model for Flight Simulation of Rotary Wing Unmanned Aerial Vehicles


    Contributors:

    Conference:

    Applied aerodynamics ; 2019 ; Dallas, TX



    Publication date :

    2019-01-01


    Size :

    21 pages



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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