CALCULATION RESEARCH ON THE RESIDUAL COMPRESSIVE STRENGTH OF STITCHED COMPOSITE LAMINATES AFTER IMPACT DAMAGE
Stitched composite material not only suppresses delamination expansion, but also improves inter-laminar toughness and compressive characteristics after impact by introducing stitch in the thickness direction. Equivalent hole method simulates the initial damage of stitched plate. The finite element a...
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| Format: | Article |
| Language: | zho |
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Editorial Office of Journal of Mechanical Strength
2017-01-01
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| Series: | Jixie qiangdu |
| Subjects: | |
| Online Access: | http://www.jxqd.net.cn/thesisDetails#10.16579/j.issn.1001.9669.2017.05.022 |
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| _version_ | 1841535311447851008 |
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| author | CHEN Tao XU XiWu MAO ChunJian |
| author_facet | CHEN Tao XU XiWu MAO ChunJian |
| author_sort | CHEN Tao |
| collection | DOAJ |
| description | Stitched composite material not only suppresses delamination expansion, but also improves inter-laminar toughness and compressive characteristics after impact by introducing stitch in the thickness direction. Equivalent hole method simulates the initial damage of stitched plate. The finite element analysis method with damage evolution process based on threedimensional Hashin criterion with 3D solid element modelling laminates,3D bar element modelling stitch simulated the stitched composite laminates damage evolution effectively. The calculation results were in good agreement with the experimental data. |
| format | Article |
| id | doaj-art-83d44ff7858e4c96b992a4b001cc268e |
| institution | Kabale University |
| issn | 1001-9669 |
| language | zho |
| publishDate | 2017-01-01 |
| publisher | Editorial Office of Journal of Mechanical Strength |
| record_format | Article |
| series | Jixie qiangdu |
| spelling | doaj-art-83d44ff7858e4c96b992a4b001cc268e2025-01-15T02:33:32ZzhoEditorial Office of Journal of Mechanical StrengthJixie qiangdu1001-96692017-01-01391126113130599629CALCULATION RESEARCH ON THE RESIDUAL COMPRESSIVE STRENGTH OF STITCHED COMPOSITE LAMINATES AFTER IMPACT DAMAGECHEN TaoXU XiWuMAO ChunJianStitched composite material not only suppresses delamination expansion, but also improves inter-laminar toughness and compressive characteristics after impact by introducing stitch in the thickness direction. Equivalent hole method simulates the initial damage of stitched plate. The finite element analysis method with damage evolution process based on threedimensional Hashin criterion with 3D solid element modelling laminates,3D bar element modelling stitch simulated the stitched composite laminates damage evolution effectively. The calculation results were in good agreement with the experimental data.http://www.jxqd.net.cn/thesisDetails#10.16579/j.issn.1001.9669.2017.05.022CompositeStitched laminatesImpact damageResidual compression strength |
| spellingShingle | CHEN Tao XU XiWu MAO ChunJian CALCULATION RESEARCH ON THE RESIDUAL COMPRESSIVE STRENGTH OF STITCHED COMPOSITE LAMINATES AFTER IMPACT DAMAGE Jixie qiangdu Composite Stitched laminates Impact damage Residual compression strength |
| title | CALCULATION RESEARCH ON THE RESIDUAL COMPRESSIVE STRENGTH OF STITCHED COMPOSITE LAMINATES AFTER IMPACT DAMAGE |
| title_full | CALCULATION RESEARCH ON THE RESIDUAL COMPRESSIVE STRENGTH OF STITCHED COMPOSITE LAMINATES AFTER IMPACT DAMAGE |
| title_fullStr | CALCULATION RESEARCH ON THE RESIDUAL COMPRESSIVE STRENGTH OF STITCHED COMPOSITE LAMINATES AFTER IMPACT DAMAGE |
| title_full_unstemmed | CALCULATION RESEARCH ON THE RESIDUAL COMPRESSIVE STRENGTH OF STITCHED COMPOSITE LAMINATES AFTER IMPACT DAMAGE |
| title_short | CALCULATION RESEARCH ON THE RESIDUAL COMPRESSIVE STRENGTH OF STITCHED COMPOSITE LAMINATES AFTER IMPACT DAMAGE |
| title_sort | calculation research on the residual compressive strength of stitched composite laminates after impact damage |
| topic | Composite Stitched laminates Impact damage Residual compression strength |
| url | http://www.jxqd.net.cn/thesisDetails#10.16579/j.issn.1001.9669.2017.05.022 |
| work_keys_str_mv | AT chentao calculationresearchontheresidualcompressivestrengthofstitchedcompositelaminatesafterimpactdamage AT xuxiwu calculationresearchontheresidualcompressivestrengthofstitchedcompositelaminatesafterimpactdamage AT maochunjian calculationresearchontheresidualcompressivestrengthofstitchedcompositelaminatesafterimpactdamage |