NASA NTRS ยท 20180004385
Simulation Tool for Damage in Composite Laminates
Abstract
A numerical simulation tool for progressive failure in laminates utilizes a low fidelity approach. The numerical model includes an enriched element that is initially in a low fidelity form. The enriched elements may increase fidelity by splitting locally to simulate an ongoing damage process such as delamination.
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McElroy, Mark W.. 2018-07-31. Simulation Tool for Damage in Composite Laminates. https://ntrs.nasa.gov/citations/20180004385
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