Damage mechanism of composite laminates under multiple ice impacts at high velocity
•Different impact schemes including single-point and multi-point impact were carried out.•Three routes including visual analysis, C-Scan analysis and X-ray tomography were used to observe the intralaminar and interlaminar damage patterns.•An innovative damage category induced by multiple ice impacts...
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| Published in | International journal of impact engineering Vol. 168; p. 104296 |
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| Main Authors | , , , , , , |
| Format | Journal Article |
| Language | English |
| Published |
Elsevier Ltd
01.10.2022
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| Subjects | |
| Online Access | Get full text |
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| Abstract | •Different impact schemes including single-point and multi-point impact were carried out.•Three routes including visual analysis, C-Scan analysis and X-ray tomography were used to observe the intralaminar and interlaminar damage patterns.•An innovative damage category induced by multiple ice impacts were summarized.•The sequence and morphology of delamination damage between plies are different in single-point and multi-point impact.•A strain-rate dependent continuum damage model with interlayer cohesive element was successfully used to evaluate the damage behavior in CFRP laminates.
Unlike most research on ice impact threats with single impact and multiple repeated impact, different impact schemes such as single-point repeated impact and multi-point sequential impact were carried out in this article, considering the actual circumstance of hail impacts on aerospace structures. To study the response of CFRP laminates to multiple ice impacts, ice projectiles with a diameter of 25 mm were projected onto laminates. Three different routes, including visual analysis, C-Scan analysis and X-ray tomography, were then used to observe the intralaminar and interlaminar damage patterns. An innovative damage category induced by different impact schemes was summarized from the whole experimental results through the visual analysis. The extent of delamination damage was characterized by C-Scan and CT. Both the damage mode and the area of delamination are not only related to the magnitude of single impact energy, but also to the density of impact points. For numerical approach, a strain-rate dependent continuum damage model with interlayer cohesive element was used to predict the damage evolution in CFRP laminates. It was first verified and then combined with the test data to reveal different damage mechanisms of single-point repeated impact and multi-point sequential impact. |
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| AbstractList | •Different impact schemes including single-point and multi-point impact were carried out.•Three routes including visual analysis, C-Scan analysis and X-ray tomography were used to observe the intralaminar and interlaminar damage patterns.•An innovative damage category induced by multiple ice impacts were summarized.•The sequence and morphology of delamination damage between plies are different in single-point and multi-point impact.•A strain-rate dependent continuum damage model with interlayer cohesive element was successfully used to evaluate the damage behavior in CFRP laminates.
Unlike most research on ice impact threats with single impact and multiple repeated impact, different impact schemes such as single-point repeated impact and multi-point sequential impact were carried out in this article, considering the actual circumstance of hail impacts on aerospace structures. To study the response of CFRP laminates to multiple ice impacts, ice projectiles with a diameter of 25 mm were projected onto laminates. Three different routes, including visual analysis, C-Scan analysis and X-ray tomography, were then used to observe the intralaminar and interlaminar damage patterns. An innovative damage category induced by different impact schemes was summarized from the whole experimental results through the visual analysis. The extent of delamination damage was characterized by C-Scan and CT. Both the damage mode and the area of delamination are not only related to the magnitude of single impact energy, but also to the density of impact points. For numerical approach, a strain-rate dependent continuum damage model with interlayer cohesive element was used to predict the damage evolution in CFRP laminates. It was first verified and then combined with the test data to reveal different damage mechanisms of single-point repeated impact and multi-point sequential impact. |
| ArticleNumber | 104296 |
| Author | Chen, Wei Fu, Xinqiang Zhao, Zhenhua Xu, Kailong Zhu, Xinying Luo, Gang Liu, Lulu |
| Author_xml | – sequence: 1 givenname: Xinying surname: Zhu fullname: Zhu, Xinying organization: Jiangsu Province Key Laboratory of Aerospace Power System, College of Energy and Power Engineering, Nanjing University of aeronautics and Astronautics, China – sequence: 2 givenname: Xinqiang surname: Fu fullname: Fu, Xinqiang organization: Jiangsu Province Key Laboratory of Aerospace Power System, College of Energy and Power Engineering, Nanjing University of aeronautics and Astronautics, China – sequence: 3 givenname: Lulu surname: Liu fullname: Liu, Lulu email: liululu@nuaa.edu.cn organization: Jiangsu Province Key Laboratory of Aerospace Power System, College of Energy and Power Engineering, Nanjing University of aeronautics and Astronautics, China – sequence: 4 givenname: Kailong surname: Xu fullname: Xu, Kailong organization: Jiangsu Province Key Laboratory of Aerospace Power System, College of Energy and Power Engineering, Nanjing University of aeronautics and Astronautics, China – sequence: 5 givenname: Gang surname: Luo fullname: Luo, Gang organization: State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics, China – sequence: 6 givenname: Zhenhua surname: Zhao fullname: Zhao, Zhenhua organization: State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics, China – sequence: 7 givenname: Wei surname: Chen fullname: Chen, Wei organization: Jiangsu Province Key Laboratory of Aerospace Power System, College of Energy and Power Engineering, Nanjing University of aeronautics and Astronautics, China |
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| SubjectTerms | Damage mechanism Laminate Multi-point sequential impact Multiple ice impacts Single-point repeated impact |
| Title | Damage mechanism of composite laminates under multiple ice impacts at high velocity |
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