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    Title :

    Generalized Flight Dynamic Model of Quadrotor Using Hybrid Blade Element Momentum Theory


    Contributors:

    Published in:

    Journal of Aircraft ; 55 , 5 ; 2162-2168


    Publication date :

    2018-04-30


    Size :

    7 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English






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