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Development of a Benchmark Example for Delamination Fatigue Growth PredictionThe development of a benchmark example for cyclic delamination growth prediction is presented and demonstrated for a commercial code. The example is based on a finite element model of a Double Cantilever Beam (DCB) specimen, which is independent of the analysis software used and allows the assessment of the delamination growth prediction capabilities in commercial finite element codes. First, the benchmark result was created for the specimen. Second, starting from an initially straight front, the delamination was allowed to grow under cyclic loading in a finite element model of a commercial code. The number of cycles to delamination onset and the number of cycles during stable delamination growth for each growth increment were obtained from the analysis. In general, good agreement between the results obtained from the growth analysis and the benchmark results could be achieved by selecting the appropriate input parameters. Overall, the results are encouraging but further assessment for mixed-mode delamination is required
Document ID
20100027539
Acquisition Source
Langley Research Center
Document Type
Contractor Report (CR)
Authors
Krueger, Ronald
(National Inst. of Aerospace Hampton, VA, United States)
Date Acquired
August 24, 2013
Publication Date
July 1, 2010
Subject Category
Composite Materials
Report/Patent Number
NF1676L-10903
NIA No. 2010-04
NASA/CR-2010-216723
Funding Number(s)
WBS: WBS 814358.02.01.07
CONTRACT_GRANT: NNL09AA00A
Distribution Limits
Public
Copyright
Public Use Permitted.
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