This paper is devoted to the results of studies prospective unmanned aerial vehicle scheme “flying wing”. Using aerodynamic configuration “flying wing”, which force greater than that of aircraft of the normal circuit losses balancing aerodynamic qualities are still not widely available in aviation, but “flying wing” allows you to fully realize their positive properties to create a new generation of unmanned aerial vehicles.


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    Title :

    Aerodynamic and flight characteristics of prospective UAV scheme “flying wing”


    Contributors:


    Publication date :

    2015-10-01


    Size :

    1957795 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



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