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 gmail.com> |
| License: |
GPL-3 |
| NeedsCompilation: |
no |
| CRAN checks: |
crackR results |
Downloads: