# 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.

- Author
- Keith Halbert
- Date of publication
- 2014-04-22 07:23:26
- Maintainer
- Keith Halbert <keith.a.halbert@gmail.com>
- License
- GPL-3
- Version
- 0.3-9

## Man pages

- analyze
- Perform a probabilistic damage tolerance analysis on a crackR...
- analyzeParallel
- Perform multiple parallel runs of a probabilistic damage...
- calcInterval
- Advance crackR object to the next scheduled inspection
- calcSfpofFromPofInt
- Calculate SFPOF results from interval failure probabilities
- cp4
- Examples CP4, CP6, and CP7, adapted from PRobability Of...
- crackRcalcSfpofMc
- Calculates SFPOF by post-processing an explicit Monte Carlo...
- crackRinit
- Initializes a crackR object (of class Sing, Mult, or CD) from...
- crackRmc
- Performs a probabilistic damage tolerance analysis using...
- crackR-package
- Probabilistic damage tolerance analysis for fatigue cracking...
- inspection
- Predict the results of a future scheduled inspection and...
- lognormalPOD
- Define Probability Of Detection (POD) curve for...
- plot.Sing
- Plotting methods for various crackR objects
- print.Sing
- Printing methods for various crackR objects