Probabilistic damage tolerance analysis for fatigue cracking of metallic aerospace structures
Using a sampling-based approach (either sequential importance sampling 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.
To run a crackR analysis, first create an object of class crackR. This is accomplished by first creating an object of class crackRparameters. This can be done by modifying a supplied data set, such as with data(cp7). Use crackRinit() on the crackRparameters object to generate the crackR object. To perform the analysis, use analyze() or crackRmc().
Maintainer: Keith Halbert <firstname.lastname@example.org>
MIL-STD-1530C (USAF) "General Guidelines For Aircraft Structural Integrity Program (ASIP)", Nov 2005
MIL-HDBK-1823A (Department of Defense, USA) "Nondestructive Evaluation System Reliability Assessment", Apr 2009
PRoF Ver. 3.0 PRobability of Fracture, Software Package, University of Dayton Research Institute, Dayton, OH, 2005
Halbert, K. "Estimation of Probability of Failure for Damage-Tolerant Aerospace Structures" PhD Thesis, Temple University Department of Statistics, Philadelphia, PA, Apr 2014
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