Abstract The basic equations of the main rotor blade motion with the preservation of nonlinear terms are presented. The results of analyzing the term values for nonlinear equations obtained for different flight regimes and several aeroelasticity problems are given.


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    Title :

    Study of feasibility and exactness for the mathematical “semirigid” nonlinear model of the helicopter main rotor


    Contributors:

    Published in:

    Publication date :

    2012-10-01


    Size :

    9 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English





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