Interaction of delaminations and matrix cracks in a CFRP plate, Part II: Simulation using an enriched shell finite element model
Numerical simulations are presented of a recently developed test which creates multiple delaminations in a CFRP laminate specimen that grow and interact via transverse matrix cracks [1]. A novel shell element enriched with the Floating Node Method, and a damage algorithm based on the Virtual Crack C...
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| Published in | Composites. Part A, Applied science and manufacturing Vol. 103; pp. 252 - 262 |
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| Main Authors | , , |
| Format | Journal Article |
| Language | English |
| Published |
Langley Research Center
Elsevier Ltd
01.12.2017
Elsevier |
| Subjects | |
| Online Access | Get full text |
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| Abstract | Numerical simulations are presented of a recently developed test which creates multiple delaminations in a CFRP laminate specimen that grow and interact via transverse matrix cracks [1]. A novel shell element enriched with the Floating Node Method, and a damage algorithm based on the Virtual Crack Closure Technique, were used to successfully simulate the tests. Additionally, a 3D high mesh fidelity model based on cohesive zones and continuum damage mechanics was used to simulate the tests and act as a representative of other similar state-of-the-art high mesh fidelity modeling techniques to compare to the enriched shell element. The enriched shell and high mesh fidelity models had similar levels of accuracy and generally matched the experimental data. With runtimes of 36 min for the shell model and 55 h for the high mesh fidelity model, the shell model is 92 times faster than the high-fidelity simulation. |
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| AbstractList | Numerical simulations are presented of a recently developed test which creates multiple delaminations in a CFRP laminate specimen that grow and interact via transverse matrix cracks [1]. A novel shell element enriched with the Floating Node Method, and a damage algorithm based on the Virtual Crack Closure Technique, were used to successfully simulate the tests. Additionally, a 3D high mesh fidelity model based on cohesive zones and continuum damage mechanics was used to simulate the tests and act as a representative of other similar state-of-the-art high mesh fidelity modeling techniques to compare to the enriched shell element. The enriched shell and high mesh fidelity models had similar levels of accuracy and generally matched the experimental data. With runtimes of 36 min for the shell model and 55 h for the high mesh fidelity model, the shell model is 92 times faster than the high-fidelity simulation. Numerical simulations are presented of a recently developed test which creates multiple delaminations in a CFRP laminate specimen that grow and interact via transverse matrix cracks [1]. A novel shell element enriched with the Floating Node Method, and a damage algorithm based on the Virtual Crack Closure Technique, were used to successfully simulate the tests. Additionally, a 3D high mesh fidelity model based on cohesive zones and continuum damage mechanics was used to simulate the tests and act as a representative of other similar state-of-the-art high mesh fidelity modeling techniques to compare to the enriched shell element. The enriched shell and high mesh fidelity models had similar levels of accuracy and generally matched the experimental data. With runtimes of 36 minutes for the shell model and 55 hours for the high mesh fidelity model, the shell model is 92 times faster than the high-fidelity simulation. Numerical simulations are presented of a recently developed test which creates multiple delaminations in a CFRP laminate specimen that grow and interact via transverse matrix cracks [ 1 ]. A novel shell element enriched with the Floating Node Method, and a damage algorithm based on the Virtual Crack Closure Technique, were used to successfully simulate the tests. Additionally, a 3D high mesh fidelity model based on cohesive zones and continuum damage mechanics was used to simulate the tests and act as a representative of other similar state-of-the-art high mesh fidelity modeling techniques to compare to the enriched shell element. The enriched shell and high mesh fidelity models had similar levels of accuracy and generally matched the experimental data. With runtimes of 36 minutes for the shell model and 55 hours for the high mesh fidelity model, the shell model is 92 times faster than the high-fidelity simulation. Numerical simulations are presented of a recently developed test which creates multiple delaminations in a CFRP laminate specimen that grow and interact via transverse matrix cracks. A novel shell element enriched with the Floating Node Method, and a damage algorithm based on the Virtual Crack Closure Technique, were used to successfully simulate the tests. Additionally, a 3D high mesh fidelity model based on cohesive zones and continuum damage mechanics was used to simulate the tests and act as a representative of other similar state-of-the-art high mesh fidelity modeling techniques to compare to the enriched shell element. The enriched shell and high mesh fidelity models had similar levels of accuracy and generally matched the experimental data. With runtimes of 36 minutes for the shell model and 55 hours for the high mesh fidelity model, the shell model is 92 times faster than the high- fidelity simulation. |
| Audience | PUBLIC |
| Author | McElroy, Mark W. Pankow, Mark Gutkin, Renaud |
| AuthorAffiliation | 3 North Carolina State University, Raleigh, NC 2 Volvo Cars, Gothenburg, Sweden 1 NASA Langley Research Center, 2 W. Reid St, Mail Stop 188E, Hampton, VA 23451 |
| AuthorAffiliation_xml | – name: 2 Volvo Cars, Gothenburg, Sweden – name: 1 NASA Langley Research Center, 2 W. Reid St, Mail Stop 188E, Hampton, VA 23451 – name: 3 North Carolina State University, Raleigh, NC |
| Author_xml | – sequence: 1 givenname: Mark W. surname: McElroy fullname: McElroy, Mark W. email: mark.w.mcelroy@nasa.gov organization: NASA Langley Research Center, 2 W. Reid St, Mail Stop 188E, Hampton, VA 23681, United States – sequence: 2 givenname: Renaud surname: Gutkin fullname: Gutkin, Renaud organization: Volvo Car Corporation, Durability CAE Body & Trim, Sweden – sequence: 3 givenname: Mark surname: Pankow fullname: Pankow, Mark organization: North Carolina State University, Raleigh, NC 27695, United States |
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| Keywords | D. Finite element analysis (FEA) C. Fracture B. Delamination A. Laminates B. Fracture C. Finite element analysis (FEA) |
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| Snippet | Numerical simulations are presented of a recently developed test which creates multiple delaminations in a CFRP laminate specimen that grow and interact via... |
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| SubjectTerms | A. Laminates B. Delamination C. Fracture Composite Materials D. Finite element analysis (FEA) Structural Mechanics |
| Title | Interaction of delaminations and matrix cracks in a CFRP plate, Part II: Simulation using an enriched shell finite element model |
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