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.
Version: | 0.3-9 |
Depends: | Hmisc (≥ 3.14-3), evd (≥ 2.3-0) |
Published: | 2014-04-22 |
Author: | Keith Halbert |
Maintainer: | Keith Halbert <keith.a.halbert at gmail.com> |
License: | GPL-3 |
NeedsCompilation: | no |
CRAN checks: | crackR results |
Reference manual: | crackR.pdf |
Package source: | crackR_0.3-9.tar.gz |
Windows binaries: | r-devel: crackR_0.3-9.zip, r-release: crackR_0.3-9.zip, r-oldrel: crackR_0.3-9.zip |
OS X El Capitan binaries: | r-release: crackR_0.3-9.tgz |
OS X Mavericks binaries: | r-oldrel: crackR_0.3-9.tgz |
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