Abstract Safety factors of the Ansat helicopter main rotor blade are determined in the root section at various flight modes with taking into account the possible damages.


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    Title :

    Calculation of a safety factor of damaged composite main rotor blade according to limit equilibrium theory


    Contributors:

    Published in:

    Publication date :

    2016-07-01


    Size :

    8 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English