Abstract The motion of blades relative to the disk wing at the extension and retraction modes is defined. The general solution is obtained including the fuselage motion under the action of control or external disturbance.


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    Title :

    A mathematical model of transforming the vertical takeoff and landing aircraft with a disk wing at maneuvering (on a deck)


    Contributors:

    Published in:

    Russian Aeronautics ; 59 , 4 ; 507-516


    Publication date :

    2016-10-01


    Size :

    10 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English