Aspects of fatigue of complete airplane structure together with numerical applications; formula developed for calculation of fatigue life as function of most important design and fatigue parameters; new method by W.WEIBULL for determination of S-N curves at various probability levels. 18th Wright Brothers Lecture. (See also - discussion p 403-13; Stockholm. Flygtekniska Forsoksanstalten (Aeronautical Research Inst, Sweden) -- Report 60 1955 p 1-125 (discussion) 126-51)


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    Title :

    Fatigue life of airplane structures


    Additional title:

    J Aeronautical Sciences


    Contributors:


    Publication date :

    1955


    Size :

    54 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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