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.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    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




    Simulation model of loads created by a hingeless helicopter rotor

    Girfanov, A. M. / Ledyankina, O. A. | Online Contents | 2015



    New design of hingeless helicopter rotor improves stability

    Ormiston, R. A. / Bousman, W. G. / Hodges, D. H. et al. | NTRS | 1975


    Hingeless variable pitch propeller hub, helicopter rotor wing and helicopter

    HAN SHUHONG / ZHANG RUIFANG / MENG CHENG et al. | European Patent Office | 2023

    Free access

    Stability and Control of Hingeless Rotor Helicopter Ground Resonance

    Maurice I. Young / David J. Bailey | AIAA | 1974