OUT-OF-PLANE TENSION FAILURE ANALYSIS OF COMPOSITE STRINGER FOR AIRCRAFT
The nonlinear effects of geometry, material and contact are considered, the finite element analysis（hereinafter FEA） method of composite stringer out-of-plane tension failure is established precisely by using Hoffman material failure criteria and Newton-Raphson increment iteration method. A verifica...
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| Format: | Article |
| Language: | zho |
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Editorial Office of Journal of Mechanical Strength
2019-01-01
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| Series: | Jixie qiangdu |
| Subjects: | |
| Online Access: | http://www.jxqd.net.cn/thesisDetails#10.16579/j.issn.1001.9669.2019.03.041 |
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| author | HUANG WenChao ZHU ZhaoZe |
| author_facet | HUANG WenChao ZHU ZhaoZe |
| author_sort | HUANG WenChao |
| collection | DOAJ |
| description | The nonlinear effects of geometry, material and contact are considered, the finite element analysis（hereinafter FEA） method of composite stringer out-of-plane tension failure is established precisely by using Hoffman material failure criteria and Newton-Raphson increment iteration method. A verification test is designed to test the failure load and failure mode of three different stringer configurations.Then the load-displacement curve is drawn to verify the validity of the FEA method.The influence factors of out-of-plane tension failure of composite stringer are studied, which can guide the strength design of aircraft. |
| format | Article |
| id | doaj-art-7098a180c2d1467d84a3fd7c4f2d00a9 |
| institution | DOAJ |
| issn | 1001-9669 |
| language | zho |
| publishDate | 2019-01-01 |
| publisher | Editorial Office of Journal of Mechanical Strength |
| record_format | Article |
| series | Jixie qiangdu |
| spelling | doaj-art-7098a180c2d1467d84a3fd7c4f2d00a92025-08-20T02:41:54ZzhoEditorial Office of Journal of Mechanical StrengthJixie qiangdu1001-96692019-01-014175375730604956OUT-OF-PLANE TENSION FAILURE ANALYSIS OF COMPOSITE STRINGER FOR AIRCRAFTHUANG WenChaoZHU ZhaoZeThe nonlinear effects of geometry, material and contact are considered, the finite element analysis（hereinafter FEA） method of composite stringer out-of-plane tension failure is established precisely by using Hoffman material failure criteria and Newton-Raphson increment iteration method. A verification test is designed to test the failure load and failure mode of three different stringer configurations.Then the load-displacement curve is drawn to verify the validity of the FEA method.The influence factors of out-of-plane tension failure of composite stringer are studied, which can guide the strength design of aircraft.http://www.jxqd.net.cn/thesisDetails#10.16579/j.issn.1001.9669.2019.03.041NonlinearComposite meterialStringerOut-of-plane tension |
| spellingShingle | HUANG WenChao ZHU ZhaoZe OUT-OF-PLANE TENSION FAILURE ANALYSIS OF COMPOSITE STRINGER FOR AIRCRAFT Jixie qiangdu Nonlinear Composite meterial Stringer Out-of-plane tension |
| title | OUT-OF-PLANE TENSION FAILURE ANALYSIS OF COMPOSITE STRINGER FOR AIRCRAFT |
| title_full | OUT-OF-PLANE TENSION FAILURE ANALYSIS OF COMPOSITE STRINGER FOR AIRCRAFT |
| title_fullStr | OUT-OF-PLANE TENSION FAILURE ANALYSIS OF COMPOSITE STRINGER FOR AIRCRAFT |
| title_full_unstemmed | OUT-OF-PLANE TENSION FAILURE ANALYSIS OF COMPOSITE STRINGER FOR AIRCRAFT |
| title_short | OUT-OF-PLANE TENSION FAILURE ANALYSIS OF COMPOSITE STRINGER FOR AIRCRAFT |
| title_sort | out of plane tension failure analysis of composite stringer for aircraft |
| topic | Nonlinear Composite meterial Stringer Out-of-plane tension |
| url | http://www.jxqd.net.cn/thesisDetails#10.16579/j.issn.1001.9669.2019.03.041 |
| work_keys_str_mv | AT huangwenchao outofplanetensionfailureanalysisofcompositestringerforaircraft AT zhuzhaoze outofplanetensionfailureanalysisofcompositestringerforaircraft |