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Numerical Simulations of the Low-Velocity Impact Response of Semicylindrical Woven Composite Shells
This paper presents an efficient and reliable approach to study the low-velocity impact response of woven composite shells using 3D finite element models that account for the physical intralaminar and interlaminar progressive damage. The authors’ previous work on the experimental assessment of the e...
Autores principales: | , , |
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Formato: | Online Artículo Texto |
Lenguaje: | English |
Publicado: |
MDPI
2023
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Materias: | |
Acceso en línea: | https://www.ncbi.nlm.nih.gov/pmc/articles/PMC10179751/ https://www.ncbi.nlm.nih.gov/pubmed/37176324 http://dx.doi.org/10.3390/ma16093442 |
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author | Ferreira, Luis M. Coelho, Carlos A. C. P. Reis, Paulo N. B. |
author_facet | Ferreira, Luis M. Coelho, Carlos A. C. P. Reis, Paulo N. B. |
author_sort | Ferreira, Luis M. |
collection | PubMed |
description | This paper presents an efficient and reliable approach to study the low-velocity impact response of woven composite shells using 3D finite element models that account for the physical intralaminar and interlaminar progressive damage. The authors’ previous work on the experimental assessment of the effect of thickness on the impact response of semicylindrical composite laminated shells served as the basis for this paper. Therefore, the finite element models were put to the test in comparison to the experimental findings. A good agreement was obtained between the numerical predictions and experimental data for the load and energy histories as well as for the maximum impact load, maximum displacement, and contact time. The use of the mass-scaling technique was successfully implemented, reducing considerably the computing cost of the solutions. The maximum load, maximum displacement, and contact time are negligibly affected by the choice of finite element mesh discretization. However, it has an impact on the initiation and progression of interlaminar damage. Therefore, to accurately compute delamination, its correct definition is of upmost importance. The validation of these finite element models opens the possibility for further numerical studies on of woven composite shells and enables shortening the time and expenses associated with the experimental testing. |
format | Online Article Text |
id | pubmed-10179751 |
institution | National Center for Biotechnology Information |
language | English |
publishDate | 2023 |
publisher | MDPI |
record_format | MEDLINE/PubMed |
spelling | pubmed-101797512023-05-13 Numerical Simulations of the Low-Velocity Impact Response of Semicylindrical Woven Composite Shells Ferreira, Luis M. Coelho, Carlos A. C. P. Reis, Paulo N. B. Materials (Basel) Article This paper presents an efficient and reliable approach to study the low-velocity impact response of woven composite shells using 3D finite element models that account for the physical intralaminar and interlaminar progressive damage. The authors’ previous work on the experimental assessment of the effect of thickness on the impact response of semicylindrical composite laminated shells served as the basis for this paper. Therefore, the finite element models were put to the test in comparison to the experimental findings. A good agreement was obtained between the numerical predictions and experimental data for the load and energy histories as well as for the maximum impact load, maximum displacement, and contact time. The use of the mass-scaling technique was successfully implemented, reducing considerably the computing cost of the solutions. The maximum load, maximum displacement, and contact time are negligibly affected by the choice of finite element mesh discretization. However, it has an impact on the initiation and progression of interlaminar damage. Therefore, to accurately compute delamination, its correct definition is of upmost importance. The validation of these finite element models opens the possibility for further numerical studies on of woven composite shells and enables shortening the time and expenses associated with the experimental testing. MDPI 2023-04-28 /pmc/articles/PMC10179751/ /pubmed/37176324 http://dx.doi.org/10.3390/ma16093442 Text en © 2023 by the authors. https://creativecommons.org/licenses/by/4.0/Licensee MDPI, Basel, Switzerland. This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC BY) license (https://creativecommons.org/licenses/by/4.0/). |
spellingShingle | Article Ferreira, Luis M. Coelho, Carlos A. C. P. Reis, Paulo N. B. Numerical Simulations of the Low-Velocity Impact Response of Semicylindrical Woven Composite Shells |
title | Numerical Simulations of the Low-Velocity Impact Response of Semicylindrical Woven Composite Shells |
title_full | Numerical Simulations of the Low-Velocity Impact Response of Semicylindrical Woven Composite Shells |
title_fullStr | Numerical Simulations of the Low-Velocity Impact Response of Semicylindrical Woven Composite Shells |
title_full_unstemmed | Numerical Simulations of the Low-Velocity Impact Response of Semicylindrical Woven Composite Shells |
title_short | Numerical Simulations of the Low-Velocity Impact Response of Semicylindrical Woven Composite Shells |
title_sort | numerical simulations of the low-velocity impact response of semicylindrical woven composite shells |
topic | Article |
url | https://www.ncbi.nlm.nih.gov/pmc/articles/PMC10179751/ https://www.ncbi.nlm.nih.gov/pubmed/37176324 http://dx.doi.org/10.3390/ma16093442 |
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