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Fracture mechanics life analytical methods verification testingVerification and validation of the basic information capabilities in NASCRAC has been completed. The basic information includes computation of K versus a, J versus a, and crack opening area versus a. These quantities represent building blocks which NASCRAC uses in its other computations such as fatigue crack life and tearing instability. Several methods were used to verify and validate the basic information capabilities. The simple configurations such as the compact tension specimen and a crack in a finite plate were verified and validated versus handbook solutions for simple loads. For general loads using weight functions, offline integration using standard FORTRAN routines was performed. For more complicated configurations such as corner cracks and semielliptical cracks, NASCRAC solutions were verified and validated versus published results and finite element analyses. A few minor problems were identified in the basic information capabilities of the simple configurations. In the more complicated configurations, significant differences between NASCRAC and reference solutions were observed because NASCRAC calculates its solutions as averaged values across the entire crack front whereas the reference solutions were computed for a single point.
Document ID
19940032507
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Favenesi, J. A.
(Nichols Research Corp. Huntsville, AL, United States)
Clemmons, T. G.
(Nichols Research Corp. Huntsville, AL, United States)
Lambert, T. J.
(Nichols Research Corp. Huntsville, AL, United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1994
Subject Category
Structural Mechanics
Report/Patent Number
M-748
NAS 1.26:4602
NASA-CR-4602
Report Number: M-748
Report Number: NAS 1.26:4602
Report Number: NASA-CR-4602
Accession Number
94N37015
Funding Number(s)
CONTRACT_GRANT: NAS8-38103
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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