METAL FATIGUE

weakened condition induced in metal parts of machines, vehicles, or structures by repeated stresses or loadings, ultimately resulting in fracture under a stress much weaker than that necessary to cause fracture in a single application. Though the term dates back to the 19th century and though considerable observation of the phenomenon was made then and in the first half of the 20th century, only with the spectacular failure of pressure cabins in British Comet jetliners in 1954 did it receive widespread engineering attention. In the 1970s much remained to be learned about metal fatigue, but empirical methods had proved effective in overcoming it. Fatigue-resistant metals had been developed and their performance enhanced by surface treatment, while fatigue stresses were significantly lessened in aircraft and other applications by designing to avoid stress concentrations. Large-scale prototype testing and new testing methods, including the metallurgical microscope, were also employed.