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A Multiscale Nonlocal Progressive Damage Model for Composite MaterialsIn this paper, the advantages of a nonlocal progressive damage formulation are described and demonstrated. An approximation of the nonlocal formulation was implemented coupled with the MAT162 composite damage model as a User defined material model in the LS DYNA environment. A comparison of the local model and the nonlocal model is simulated for an 8-ply laminate under tension is carried for increasing mesh densities. The results show the regularization achieved by nonlocal models by providing mesh independent results.




Document ID
20200002373
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Kodagali, Karan
(University of South Carolina Columbia, SC, United States)
Sockalingam, Subramani
(University of South Carolina Columbia, SC, United States)
Date Acquired
April 14, 2020
Publication Date
January 7, 2019
Subject Category
Quality Assurance And Reliability
Composite Materials
Report/Patent Number
NF1676L-30199
Report Number: NF1676L-30199
Meeting Information
Meeting: 2019 AIAA SciTech Forum and Exposition
Location: San Diego, CA
Country: United States
Start Date: January 7, 2019
End Date: January 11, 2019
Sponsors: American Institute of Aeronautics and Astronautics (AIAA)
Funding Number(s)
CONTRACT_GRANT: 80LARC17C0004
CONTRACT_GRANT: NNL09AA00A
WBS: 826611.04.07.01
Distribution Limits
Public
Copyright
Public Use Permitted.
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