Using a sampling-based approach (either sequential importance sampling or explicit Monte Carlo), this package can be used to perform a probabilistic damage tolerance for aircraft structures. It can model a single crack, or two simultaneously growing fatigue cracks (the so-called continuing damage problem). With a single crack, multiple types of future repairs are possible.
|Date of publication||2014-04-22 07:23:26|
|Maintainer||Keith Halbert <[email protected]>|
|Package repository||View on CRAN|
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