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Fracture-Based Mesh Size Requirements for Matrix Cracks in Continuum Damage Mechanics ModelsThis paper evaluates the ability of progressive damage analysis (PDA) finite element (FE) models to predict transverse matrix cracks in unidirectional composites. The results of the analyses are compared to closed-form linear elastic fracture mechanics (LEFM) solutions. Matrix cracks in fiber-reinforced composite materials subjected to mode I and mode II loading are studied using continuum damage mechanics and zero-thickness cohesive zone modeling approaches. The FE models used in this study are built parametrically so as to investigate several model input variables and the limits associated with matching the upper-bound LEFM solutions. Specifically, the sensitivity of the PDA FE model results to changes in strength and element size are investigated.
Document ID
20170001032
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Leone, Frank A.
(NASA Langley Research Center Hampton, VA, United States)
Davila, Carlos G.
(NASA Langley Research Center Hampton, VA, United States)
Mabson, Gerald E.
(Boeing Research and Technology Seattle, WA, United States)
Ramnath, Madhavadas
(Boeing Commercial Airplane Group Seattle, WA, United States)
Hyder, Imran
(Boeing Research & Technology North Charleston, SC, United States)
Date Acquired
January 31, 2017
Publication Date
January 9, 2017
Subject Category
Structural Mechanics
Numerical Analysis
Composite Materials
Report/Patent Number
NF1676L-24617
Report Number: NF1676L-24617
Meeting Information
Meeting: 2017 AIAA SciTech Forum
Location: Grapevine, TX
Country: United States
Start Date: January 9, 2017
End Date: January 13, 2017
Sponsors: American Society of Civil Engineers, American Society for Composites, American Helicopter Society International, 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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