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)
Fatigue life of airplane structures
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 22 , n 6
1955
54 pages
Aufsatz (Zeitschrift)
Englisch
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