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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.
Package details |
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Author | Keith Halbert |
Maintainer | Keith Halbert <keith.a.halbert@gmail.com> |
License | GPL-3 |
Version | 0.3-9 |
Package repository | View on CRAN |
Installation |
Install the latest version of this package by entering the following in R:
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