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NASA NTRS ยท 19820036973

A root-mean-square approach for predicting fatigue crack growth under random loading

Abstract

A method for predicting fatigue crack growth under random loading which employs the concept of Barsom (1976) is presented. In accordance with this method, the loading history for each specimen is analyzed to determine the root-mean-square maximum and minimum stresses, and the predictions are made by assuming the tests have been conducted under constant-amplitude loading at the root-mean-square maximum and minimum levels. The procedure requires a simple computer program and a desk-top computer. For the eleven predictions made, the ratios of the predicted lives to the test lives ranged from 2.13 to 0.82, which is a good result, considering that the normal scatter in the fatigue-crack-growth rates may range from a factor of two to four under identical loading conditions.

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BibTeXRIS

Hudson, C. M.. 1981-01-01. A root-mean-square approach for predicting fatigue crack growth under random loading. https://ntrs.nasa.gov/citations/19820036973

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