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Fracture mechanics life analytical methods verification testingThe objective was to evaluate NASCRAC (trademark) version 2.0, a second generation fracture analysis code, for verification and validity. NASCRAC was evaluated using a combination of comparisons to the literature, closed-form solutions, numerical analyses, and tests. Several limitations and minor errors were detected. Additionally, a number of major flaws were discovered. These major flaws were generally due to application of a specific method or theory, not due to programming logic. Results are presented for the following program capabilities: K versus a, J versus a, crack opening area, life calculation due to fatigue crack growth, tolerable crack size, proof test logic, tearing instability, creep crack growth, crack transitioning, crack retardation due to overloads, and elastic-plastic stress redistribution. It is concluded that the code is an acceptable fracture tool for K solutions of simplified geometries, for a limited number of J and crack opening area solutions, and for fatigue crack propagation with the Paris equation and constant amplitude loads when the Paris equation is applicable.
Document ID
19950017686
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Favenesi, J. A.
(Nichols Research Corp. Huntsville, AL, United States)
Clemons, T. G.
(Nichols Research Corp. Huntsville, AL, United States)
Riddell, W. T.
(Nichols Research Corp. Huntsville, AL, United States)
Ingraffea, A. R.
(Nichols Research Corp. Huntsville, AL, United States)
Wawrzynek, P. A.
(Nichols Research Corp. Huntsville, AL, United States)
Date Acquired
September 6, 2013
Publication Date
September 16, 1994
Subject Category
Quality Assurance And Reliability
Report/Patent Number
NASA-CR-196555
NAS 1.26:196555
Report Number: NASA-CR-196555
Report Number: NAS 1.26:196555
Accession Number
95N24106
Funding Number(s)
CONTRACT_GRANT: NAS8-38103
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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