crackR: Probabilistic damage tolerance analysis for fatigue cracking of metallic aerospace structures

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>
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:, r-release:, r-oldrel:
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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