It is suggested that distribution of reversals to failure obtained from fatigue tests on specimens typical of aircraft wing booms can be represented by log-normal curve; method, based on acceptance of certain fatigue failure rate for wing structures, is given for calculating number of reversals to failure on which "safe" life of wing may be based.


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    Title :

    Method for determining "safe" life of aircraft wing from fatigue test results


    Additional title:

    Roy Aeronautical Soc -- J


    Contributors:

    Published in:

    Publication date :

    1954


    Size :

    6 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :



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