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- W161577521 abstract "The distribution of initial flaw sizes is one of the key inputs for the calculation of the probability of failure of aircraft structures. In practice, an equivalent flaw size is used instead of the physical flaw size, to avoid numerical difficulties and to provide consistencies. The equivalent flaw size is derived, ultimately, from crack-time data obtained from teardown inspections or purpose-conducted experiments, but different methods may be used to derive the distribution of the equivalent flaw size. In this paper, two such methods are examined, and their effects on probability of failure are assessed." @default.
- W161577521 created "2016-06-24" @default.
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- W161577521 date "2014-01-01" @default.
- W161577521 modified "2023-09-27" @default.
- W161577521 title "Effect of models and derivation methods for initial flaw size distribution on probability of failure of airframes" @default.
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- W161577521 doi "https://doi.org/10.1533/9780081002254.229" @default.
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