By assumption of standard distribution of load, it is possible to calculate rapidly corresponding resultant aerodynamic bending moment at any given fraction of blade radius.


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    Title :

    Airscrew blade stressing


    Additional title:

    Flight


    Contributors:

    Published in:

    Flight ; 37 , n 1644


    Publication date :

    1940


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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