INTERNAL CLADDING LAYER INFLUENCE ON THE DEBONDING OF HAT-STRINGER STIFFENED COMPOSITE PANELS UNDER AXIAL COMPRESSION (MT)
Debonding between flange and skin is the dominate failure mode of stiffened composite panels which are widely used in modern aircraft. The influence of internal cladding layer in hat stringer on the onset of debonding is investigated experimentally and numerically. Cohesive elements are used to simu...
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| Format: | Article |
| Language: | zho |
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Editorial Office of Journal of Mechanical Strength
2022-01-01
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| Series: | Jixie qiangdu |
| Online Access: | http://www.jxqd.net.cn/thesisDetails#10.16579/j.issn.1001.9669.2022.06.030 |
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| author | YUAN Fei LIU Fu CHAI YaNan CHEN XiangMing LIN GuoWei LI XinXiang |
| author_facet | YUAN Fei LIU Fu CHAI YaNan CHEN XiangMing LIN GuoWei LI XinXiang |
| author_sort | YUAN Fei |
| collection | DOAJ |
| description | Debonding between flange and skin is the dominate failure mode of stiffened composite panels which are widely used in modern aircraft. The influence of internal cladding layer in hat stringer on the onset of debonding is investigated experimentally and numerically. Cohesive elements are used to simulate the adhesive layer between skin and flange and Hashin’s failure criterion is adopted to determine damage initiation of composite layers in the numerical simulations. The process of damage initiation, propagation and failure of the stiffened composite panels was simulated in detail. A good agreement between tests and numerical prediction was observed. |
| format | Article |
| id | doaj-art-6e31dce033a6415ca8d6cd63983af5b2 |
| institution | Kabale University |
| issn | 1001-9669 |
| language | zho |
| publishDate | 2022-01-01 |
| publisher | Editorial Office of Journal of Mechanical Strength |
| record_format | Article |
| series | Jixie qiangdu |
| spelling | doaj-art-6e31dce033a6415ca8d6cd63983af5b22025-01-15T02:39:49ZzhoEditorial Office of Journal of Mechanical StrengthJixie qiangdu1001-96692022-01-011490149736350457INTERNAL CLADDING LAYER INFLUENCE ON THE DEBONDING OF HAT-STRINGER STIFFENED COMPOSITE PANELS UNDER AXIAL COMPRESSION (MT)YUAN FeiLIU FuCHAI YaNanCHEN XiangMingLIN GuoWeiLI XinXiangDebonding between flange and skin is the dominate failure mode of stiffened composite panels which are widely used in modern aircraft. The influence of internal cladding layer in hat stringer on the onset of debonding is investigated experimentally and numerically. Cohesive elements are used to simulate the adhesive layer between skin and flange and Hashin’s failure criterion is adopted to determine damage initiation of composite layers in the numerical simulations. The process of damage initiation, propagation and failure of the stiffened composite panels was simulated in detail. A good agreement between tests and numerical prediction was observed.http://www.jxqd.net.cn/thesisDetails#10.16579/j.issn.1001.9669.2022.06.030 |
| spellingShingle | YUAN Fei LIU Fu CHAI YaNan CHEN XiangMing LIN GuoWei LI XinXiang INTERNAL CLADDING LAYER INFLUENCE ON THE DEBONDING OF HAT-STRINGER STIFFENED COMPOSITE PANELS UNDER AXIAL COMPRESSION (MT) Jixie qiangdu |
| title | INTERNAL CLADDING LAYER INFLUENCE ON THE DEBONDING OF HAT-STRINGER STIFFENED COMPOSITE PANELS UNDER AXIAL COMPRESSION (MT) |
| title_full | INTERNAL CLADDING LAYER INFLUENCE ON THE DEBONDING OF HAT-STRINGER STIFFENED COMPOSITE PANELS UNDER AXIAL COMPRESSION (MT) |
| title_fullStr | INTERNAL CLADDING LAYER INFLUENCE ON THE DEBONDING OF HAT-STRINGER STIFFENED COMPOSITE PANELS UNDER AXIAL COMPRESSION (MT) |
| title_full_unstemmed | INTERNAL CLADDING LAYER INFLUENCE ON THE DEBONDING OF HAT-STRINGER STIFFENED COMPOSITE PANELS UNDER AXIAL COMPRESSION (MT) |
| title_short | INTERNAL CLADDING LAYER INFLUENCE ON THE DEBONDING OF HAT-STRINGER STIFFENED COMPOSITE PANELS UNDER AXIAL COMPRESSION (MT) |
| title_sort | internal cladding layer influence on the debonding of hat stringer stiffened composite panels under axial compression mt |
| url | http://www.jxqd.net.cn/thesisDetails#10.16579/j.issn.1001.9669.2022.06.030 |
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