DAMAGE TOLERANCE ANALYSIS OF TYPICAL MACHINED WING PANEL
This paper predicted the crack growth life and residual strength of typical machined wing panel based on MCCI（ Modified Crack Closure Integral）. Compared with the result of the test evidence,the deviation of the prediction is acceptable by the engineering application. The results show that this meth...
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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.1001.9669.2017.01.033 |
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| _version_ | 1841535032715378688 |
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| author | KONG TingTing ZHOU LongChao WANG HuiMei |
| author_facet | KONG TingTing ZHOU LongChao WANG HuiMei |
| author_sort | KONG TingTing |
| collection | DOAJ |
| description | This paper predicted the crack growth life and residual strength of typical machined wing panel based on MCCI（ Modified Crack Closure Integral）. Compared with the result of the test evidence,the deviation of the prediction is acceptable by the engineering application. The results show that this method could be used in the research and development phase of the new aircraft project. Otherwise,the test results also show that the feature of machined stiffened panel cannot arrest the crack well. |
| format | Article |
| id | doaj-art-078a59129a3c4ec586d0459dd9408655 |
| 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-078a59129a3c4ec586d0459dd94086552025-01-15T02:35:07ZzhoEditorial Office of Journal of Mechanical StrengthJixie qiangdu1001-96692017-01-013919419730597698DAMAGE TOLERANCE ANALYSIS OF TYPICAL MACHINED WING PANELKONG TingTingZHOU LongChaoWANG HuiMeiThis paper predicted the crack growth life and residual strength of typical machined wing panel based on MCCI（ Modified Crack Closure Integral）. Compared with the result of the test evidence,the deviation of the prediction is acceptable by the engineering application. The results show that this method could be used in the research and development phase of the new aircraft project. Otherwise,the test results also show that the feature of machined stiffened panel cannot arrest the crack well.http://www.jxqd.net.cn/thesisDetails#10.16579/j.issn.1001.9669.2017.01.033Wing panelCrack growthResidual strengthMCCI |
| spellingShingle | KONG TingTing ZHOU LongChao WANG HuiMei DAMAGE TOLERANCE ANALYSIS OF TYPICAL MACHINED WING PANEL Jixie qiangdu Wing panel Crack growth Residual strength MCCI |
| title | DAMAGE TOLERANCE ANALYSIS OF TYPICAL MACHINED WING PANEL |
| title_full | DAMAGE TOLERANCE ANALYSIS OF TYPICAL MACHINED WING PANEL |
| title_fullStr | DAMAGE TOLERANCE ANALYSIS OF TYPICAL MACHINED WING PANEL |
| title_full_unstemmed | DAMAGE TOLERANCE ANALYSIS OF TYPICAL MACHINED WING PANEL |
| title_short | DAMAGE TOLERANCE ANALYSIS OF TYPICAL MACHINED WING PANEL |
| title_sort | damage tolerance analysis of typical machined wing panel |
| topic | Wing panel Crack growth Residual strength MCCI |
| url | http://www.jxqd.net.cn/thesisDetails#10.16579/j.issn.1001.9669.2017.01.033 |
| work_keys_str_mv | AT kongtingting damagetoleranceanalysisoftypicalmachinedwingpanel AT zhoulongchao damagetoleranceanalysisoftypicalmachinedwingpanel AT wanghuimei damagetoleranceanalysisoftypicalmachinedwingpanel |