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Analysis of Progressive Damage in Cross-Ply and Quasi-Isotropic Panels Subjected to Quasi-Static IndentationThe performance of a three-dimensional continuum damage mechanics (CDM) model for intralaminar damage, coupled with a cohesive zone model for delamination, is examined for damage prediction in cross-ply and quasi-isotropic laminated plates subjected to quasi-static transverse indentation. Details of the CDM model based on the deformation gradient decomposition (DGD) method and the finite element (FE) modeling strategy are presented and discussed. Critical features of the damage model and FE modeling approach are assessed by comparing analysis predictions to experimental data for cross-ply and quasi-isotropic panels in which damage is dominated by complex interactions between matrix cracks and delaminations.
Document ID
20190000435
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Song, Kyongchan
(Analytical Mechanics Associates, Inc. Hampton, VA, United States)
Leone, Frank A.
(NASA Langley Research Center Hampton, VA, United States)
Rose, Cheryl A.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
February 5, 2019
Publication Date
January 8, 2018
Subject Category
Composite Materials
Report/Patent Number
NF1676L-27401
Meeting Information
Meeting: AIAA Science and Technology Forum and Exposition
Location: Kissimmee, FL
Country: United States
Start Date: January 8, 2018
End Date: January 12, 2018
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 826611.04.07.01
Distribution Limits
Public
Copyright
Public Use Permitted.
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