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Development of a Mesoscale Finite Element Constitutive Model for Fiber KinkingA mesoscale finite element material model is proposed to analyze structures that fail by the fiber kinking damage mode. To evaluate the assumptions of the mesoscale model, the results were compared with those of a high-fidelity micromechanical model. A direct comparison between the two models shows remarkable correlation, indicating that the key features of the fiber kinking phenomenon are appropriately accounted for in the mesoscale model. The mesoscale model is applied to structural analysis cases to demonstrate the capabilities of the model. A verification study is conducted with an unnotched compression specimen and preliminary validation is demonstrated with a notched compression specimen. The results show that the model is successful at representing the kinematics of fiber kinking while at the same time highlighting the need for further verification and validation.
Document ID
20190000439
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Bergan, Andrew C.
(NASA Langley Research Center Hampton, VA, United States)
Herraez, Miguel
(IMDEA Software Inst. Madrid, Spain)
Gonzalez, Carlos
(IMDEA Software Inst. Madrid, Spain)
Lopes, Claudio S.
(IMDEA Software Inst. Madrid, Spain)
Date Acquired
February 7, 2019
Publication Date
January 8, 2018
Subject Category
Composite Materials
Report/Patent Number
NF1676L-27418
Report Number: NF1676L-27418
Meeting Information
Meeting: AIAA SciTech 2018
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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