Abstract This work proposes a technique for simulation of integral loads created by a hingeless helicopter rotor, which is based on implementing neural network algorithms. A method, which accounts for variation of angular speeds of the main rotor in the simulation model is proposed. Feasibility of the proposed model is justified on an example of computation and simulation of a helicopter operating in steady flight conditions.


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    Title :

    Simulation model of loads created by a hingeless helicopter rotor


    Contributors:

    Published in:

    Publication date :

    2015-04-01


    Size :

    6 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English