Effects of stress concentration, deflection, and vibration on life of parts subjected to repeated loading are analyzed; criteria established at Consolidated Vultee Aircraft, based on actual fatigue tests of parts involved compared to life at time of failure in service, are discussed; typical examples given. From paper before Inst Aeronautical Sciences.


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    Title :

    Fatigue failure of aircraft parts -- Their cause and cure


    Additional title:

    Automotive Aviation Industries


    Contributors:
    Davis, D.M. (author)

    Published in:

    Publication date :

    1945


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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