Two methods of assessing probable response to fatigue are in common use. The safe life method is based on the expected loading history, laboratory tests and a safety factor.
(1956), "SAE Golden Anniversary Aeronautic Meeting: Summaries of the Papers Presented to the Meeting Held in Los Angeles, October 11–15, 1955", Aircraft Engineering and Aerospace Technology, Vol. 28 No. 1, pp. 28-31. https://doi.org/10.1108/eb032653
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