The papers present an analysis of the advantages and disadvantages of application joined wing layout for unmanned aerial vehicle. Synthesis of optimal layout by criteria for aerodynamic efficiency, flight duration and weight of the structure are given in the article


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    Title :

    Possibility of application joined wing layout for UAV


    Contributors:


    Publication date :

    2015-10-01


    Size :

    2186670 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



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