Abstract The accelerations that emerge in the disk wing during rotation have been found. The loading of wing elements have been determined when the blades are extended and retracted.


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    Title :

    Dynamics of Main Rotor to Disk Wing Conversion


    Contributors:

    Published in:

    Russian Aeronautics ; 61 , 1 ; 56-63


    Publication date :

    2018-01-01


    Size :

    8 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English




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