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 126-51; J Aeronautical Sciences v 22 n 6 June 1955 p 349-402 (discussion) 403-13)
Fatigue life of airplane structures
Stockholm. Flygtekniska Forsoksanstalten (Aeronautical Research Inst, Sweden) -- Report
1955
125 pages
Report
English
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