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A Benchmark Example for Delamination Propagation Predictions Based on the Calibrated End-Loaded Split SpecimenA benchmark example based on the Calibrated End-Loaded Split (C-ELS) specimen is developed and used to assess the performance of recently developed delamination propagation capabilities in the Abaqus/Standard finite element code. The C-ELS specimen has the advantage of a longer region of stable delamination propagation compared to the existing mode II benchmark case. The new benchmark example may therefore provide a better assessment tool by enabling more stable crack growth in regions further away from the boundary conditions or load application. First, a benchmark result is created manually using two-dimensional finite element models of the C-ELS specimen with different delamination lengths. Second, the performance of the delamination propagation capabilities in the Abaqus/Standard finite element code are assessed by comparing the results to the benchmark case. Two examples with different starter delamination lengths are studied. A shorter starter length is chosen to create a scenario with unstable delamination propagation. A longer delamination causes stable delamination propagation. Detailed results from three-dimensional analyses with aligned and mis-aligned meshes and two levels of mesh refinement are provided for several permutations of numerical input parameters. In general, good agreement can be achieved between the results obtained from the quasi-static propagation analysis and the benchmark analysis. However, particular non-default settings are found to be most reliable, accurate, and numerically efficient. Numerical artifacts including anomalous unreleased nodes in the crack wake and zig-zag crack fronts occur, and further development of the Abaqus/Standard VCCT propagation may be required. Use of the benchmark case to assess the continuous improvements in one finite element code illustrates the value of establishing benchmark solutions.
Document ID
20220002098
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Ronald Krueger
(National Institute of Aerospace Hampton, Virginia, United States)
Nelson V. De Carvalho
(Langley Research Center Hampton, Virginia, United States)
Date Acquired
February 7, 2022
Publication Date
February 1, 2022
Subject Category
Composite Materials
Funding Number(s)
WBS: 664817.02.07.03.03.04
CONTRACT_GRANT: 80LARC17C0004
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Peer Committee
Keywords
delamination
fracture mechanics
benchmarking
finite element analysis
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