Study of the behavior of damaged low-velocity impact carbon/epoxy/AL2024-T3 hybrid laminates
Abstract Aluminium and layered composite structures currently play a crucial role in the aviation sector. These structures may be susceptible to inadvertent impacts from several sources. Low-velocity impact is a type of unintended aggression that causes severe harm to composite materials and can gre...
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| Main Authors: | , , , , , , , |
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| Format: | Article |
| Language: | English |
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Springer
2025-01-01
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| Series: | Discover Materials |
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| Online Access: | https://doi.org/10.1007/s43939-025-00191-0 |
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| author | Fatima Zohra Daouache Amin Houari Mourad Lounis Lecheb Samir Salah Amroune Kouider Madani Barhm Mohamad Mohamed Belhouari |
| author_facet | Fatima Zohra Daouache Amin Houari Mourad Lounis Lecheb Samir Salah Amroune Kouider Madani Barhm Mohamad Mohamed Belhouari |
| author_sort | Fatima Zohra Daouache |
| collection | DOAJ |
| description | Abstract Aluminium and layered composite structures currently play a crucial role in the aviation sector. These structures may be susceptible to inadvertent impacts from several sources. Low-velocity impact is a type of unintended aggression that causes severe harm to composite materials and can greatly diminish their residual resistance. This research presents a novel stack of unconventional hybrid laminates aimed at improving both stiffness and elasticity through a multi-material design. We focus on analyzing the main factors responsible for impact damage in hybrid structure. Tie contact were used between plies of the composite plate in all models. Using the HASHIN criterion, we analyze the impact velocity, impact sequence, composite thickness, impact energy level, impact efforts, and damaged zones in the composite, matrices, and fibers. The primary results indicate that both impact energy and composite thickness have a substantial influence on the energy absorbed by the composite and the impact exerted in the affected area. |
| format | Article |
| id | doaj-art-3885ed6e1c494cc2b334987ea8fbf96a |
| institution | Kabale University |
| issn | 2730-7727 |
| language | English |
| publishDate | 2025-01-01 |
| publisher | Springer |
| record_format | Article |
| series | Discover Materials |
| spelling | doaj-art-3885ed6e1c494cc2b334987ea8fbf96a2025-02-02T12:47:17ZengSpringerDiscover Materials2730-77272025-01-015111910.1007/s43939-025-00191-0Study of the behavior of damaged low-velocity impact carbon/epoxy/AL2024-T3 hybrid laminatesFatima Zohra Daouache0Amin Houari1Mourad Lounis2Lecheb Samir3Salah Amroune4Kouider Madani5Barhm Mohamad6Mohamed Belhouari7Mechanical Engineering Department, Relizane UniversityLaboratory of Motor Dynamics and Vibroacoustics (LDMV), M’hamed Bougara University of BoumerdesMechanical Engineering Department, Relizane UniversityLaboratory of Motor Dynamics and Vibroacoustics (LDMV), M’hamed Bougara University of BoumerdesMechanical Engineering Department, M’sila UniversityLMSS Laboratory, Department of Mechanical Engineering, Djillali Liabes University of Sidi Bel-AbbesDepartment of Petroleum Technology, Koya Technical Institute, Erbil Polytechnic UniversityLMSS Laboratory, Department of Mechanical Engineering, Djillali Liabes University of Sidi Bel-AbbesAbstract Aluminium and layered composite structures currently play a crucial role in the aviation sector. These structures may be susceptible to inadvertent impacts from several sources. Low-velocity impact is a type of unintended aggression that causes severe harm to composite materials and can greatly diminish their residual resistance. This research presents a novel stack of unconventional hybrid laminates aimed at improving both stiffness and elasticity through a multi-material design. We focus on analyzing the main factors responsible for impact damage in hybrid structure. Tie contact were used between plies of the composite plate in all models. Using the HASHIN criterion, we analyze the impact velocity, impact sequence, composite thickness, impact energy level, impact efforts, and damaged zones in the composite, matrices, and fibers. The primary results indicate that both impact energy and composite thickness have a substantial influence on the energy absorbed by the composite and the impact exerted in the affected area.https://doi.org/10.1007/s43939-025-00191-0Hybrid compositeLow-velocity impactEnergyDamage |
| spellingShingle | Fatima Zohra Daouache Amin Houari Mourad Lounis Lecheb Samir Salah Amroune Kouider Madani Barhm Mohamad Mohamed Belhouari Study of the behavior of damaged low-velocity impact carbon/epoxy/AL2024-T3 hybrid laminates Discover Materials Hybrid composite Low-velocity impact Energy Damage |
| title | Study of the behavior of damaged low-velocity impact carbon/epoxy/AL2024-T3 hybrid laminates |
| title_full | Study of the behavior of damaged low-velocity impact carbon/epoxy/AL2024-T3 hybrid laminates |
| title_fullStr | Study of the behavior of damaged low-velocity impact carbon/epoxy/AL2024-T3 hybrid laminates |
| title_full_unstemmed | Study of the behavior of damaged low-velocity impact carbon/epoxy/AL2024-T3 hybrid laminates |
| title_short | Study of the behavior of damaged low-velocity impact carbon/epoxy/AL2024-T3 hybrid laminates |
| title_sort | study of the behavior of damaged low velocity impact carbon epoxy al2024 t3 hybrid laminates |
| topic | Hybrid composite Low-velocity impact Energy Damage |
| url | https://doi.org/10.1007/s43939-025-00191-0 |
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