Abstract The results of stress analysis for the main rotor torsion bar of the ANSAT helicopter based on the finite element method are presented. The analysis was performed for the base types of loading in the linear statement. The analysis results agree well with the experimental data.


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    Title :

    Stress analysis of helicopter main rotor torsion bar


    Contributors:

    Published in:

    Publication date :

    2009-03-01


    Size :

    6 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English




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