Estimated maximum percentage reduction in fatigue limits compared with standard polished specimens; effect of vee notch on fatigue limit of different kinds of materials; properties and composition of aircraft metals and alloys; effect of corrosion on endurance; causes of fatigue failures.


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    Title :

    Fatigue of aircraft parts


    Additional title:

    Aviation


    Contributors:

    Published in:

    Aviation ; 30 , n 9


    Publication date :

    1931


    Size :

    5 pages


    Remarks:

    11 Figs


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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