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An Enriched Shell Finite Element for Progressive Damage Simulation in Composite LaminatesA formulation is presented for an enriched shell nite element capable of progressive damage simulation in composite laminates. The element uses a discrete adaptive splitting approach for damage representation that allows for a straightforward model creation procedure based on an initially low delity mesh. The enriched element is veri ed for Mode I, Mode II, and mixed Mode I/II delamination simulation using numerical benchmark data. Experimental validation is performed using test data from a delamination-migration experiment. Good correlation was found between the enriched shell element model results and the numerical and experimental data sets. The work presented in this paper is meant to serve as a rst milestone in the enriched element's development with an ultimate goal of simulating three-dimensional progressive damage processes in multidirectional laminates.
Document ID
20160010546
Acquisition Source
Langley Research Center
Document Type
Technical Publication (TP)
Authors
McElroy, Mark W.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 23, 2016
Publication Date
June 1, 2016
Subject Category
Mathematical And Computer Sciences (General)
Composite Materials
Report/Patent Number
NF1676L-24558
NASA/TP-2016-219211
L-20716
Funding Number(s)
WBS: WBS 826611.04.07.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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