Abstract The paper describes a mathematical model of drop tests on the landing gear of the Ka-62 helicopter. The model is formulated using the multibody system simulation procedure based on the Lagrange equations of the first kind.


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    Title :

    Drop test simulation for a helicopter tail landing gear


    Contributors:

    Published in:

    Russian Aeronautics ; 60 , 3 ; 342-348


    Publication date :

    2017-07-01


    Size :

    7 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English




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