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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    Titel :

    Fatigue failure of aircraft parts -- Their cause and cure


    Weitere Titelangaben:

    Automotive Aviation Industries


    Beteiligte:
    Davis, D.M. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1945


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


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