Abstract Basic principles of a mathematical model for disk-wing aircraft balancing and evaluation of power expenditure for flight as compared with a helicopter are presented.


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    Title :

    Mathematical model of balancing for a vertical takeoff and landing disk-wing aircraft


    Contributors:

    Published in:

    Publication date :

    2010-03-01


    Size :

    8 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English





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