RESEARCH ON SIMPLIFICATION OF LOADING SPECTRUM FOR FATIGUE CRACK GROWTH TEST
A new subsection-loading method has been used for solving question that was taken for aircraft structure cracking growth testing（ CGT） in a long time.Based on technology of low load cut-off,the random loading spectrum used in CGT,associated with the stress intensity factor in crack tip of specimens,...
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| Format: | Article |
| Language: | zho |
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Editorial Office of Journal of Mechanical Strength
2015-01-01
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| Series: | Jixie qiangdu |
| Subjects: | |
| Online Access: | http://www.jxqd.net.cn/thesisDetails#10.16579/j.issn.1001.9669.2015.05.027 |
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| _version_ | 1841534650452803584 |
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| author | ZHANG Kan DONG DengKe CHEN Li |
| author_facet | ZHANG Kan DONG DengKe CHEN Li |
| author_sort | ZHANG Kan |
| collection | DOAJ |
| description | A new subsection-loading method has been used for solving question that was taken for aircraft structure cracking growth testing（ CGT） in a long time.Based on technology of low load cut-off,the random loading spectrum used in CGT,associated with the stress intensity factor in crack tip of specimens,was investigated.Furthermore,Testing verification of panel specimen has been completed.The testing result showed that pre-simplification agrees with subsection of the random loading spectrum,and application of the method can reduce the time of CGT reliably（ time reducing by 27% in the testing）.Finally,it can be concluded that the method can directly be applied for CGT of fuselage panel and other aircraft structures. |
| format | Article |
| id | doaj-art-1e9e46cb87a544c095b5c9fb8935860b |
| institution | Kabale University |
| issn | 1001-9669 |
| language | zho |
| publishDate | 2015-01-01 |
| publisher | Editorial Office of Journal of Mechanical Strength |
| record_format | Article |
| series | Jixie qiangdu |
| spelling | doaj-art-1e9e46cb87a544c095b5c9fb8935860b2025-01-15T02:37:44ZzhoEditorial Office of Journal of Mechanical StrengthJixie qiangdu1001-96692015-01-013784584830592530RESEARCH ON SIMPLIFICATION OF LOADING SPECTRUM FOR FATIGUE CRACK GROWTH TESTZHANG KanDONG DengKeCHEN LiA new subsection-loading method has been used for solving question that was taken for aircraft structure cracking growth testing（ CGT） in a long time.Based on technology of low load cut-off,the random loading spectrum used in CGT,associated with the stress intensity factor in crack tip of specimens,was investigated.Furthermore,Testing verification of panel specimen has been completed.The testing result showed that pre-simplification agrees with subsection of the random loading spectrum,and application of the method can reduce the time of CGT reliably（ time reducing by 27% in the testing）.Finally,it can be concluded that the method can directly be applied for CGT of fuselage panel and other aircraft structures.http://www.jxqd.net.cn/thesisDetails#10.16579/j.issn.1001.9669.2015.05.027Technology of low cut-offSubsection-loading methodStress intensity factorTypical panel |
| spellingShingle | ZHANG Kan DONG DengKe CHEN Li RESEARCH ON SIMPLIFICATION OF LOADING SPECTRUM FOR FATIGUE CRACK GROWTH TEST Jixie qiangdu Technology of low cut-off Subsection-loading method Stress intensity factor Typical panel |
| title | RESEARCH ON SIMPLIFICATION OF LOADING SPECTRUM FOR FATIGUE CRACK GROWTH TEST |
| title_full | RESEARCH ON SIMPLIFICATION OF LOADING SPECTRUM FOR FATIGUE CRACK GROWTH TEST |
| title_fullStr | RESEARCH ON SIMPLIFICATION OF LOADING SPECTRUM FOR FATIGUE CRACK GROWTH TEST |
| title_full_unstemmed | RESEARCH ON SIMPLIFICATION OF LOADING SPECTRUM FOR FATIGUE CRACK GROWTH TEST |
| title_short | RESEARCH ON SIMPLIFICATION OF LOADING SPECTRUM FOR FATIGUE CRACK GROWTH TEST |
| title_sort | research on simplification of loading spectrum for fatigue crack growth test |
| topic | Technology of low cut-off Subsection-loading method Stress intensity factor Typical panel |
| url | http://www.jxqd.net.cn/thesisDetails#10.16579/j.issn.1001.9669.2015.05.027 |
| work_keys_str_mv | AT zhangkan researchonsimplificationofloadingspectrumforfatiguecrackgrowthtest AT dongdengke researchonsimplificationofloadingspectrumforfatiguecrackgrowthtest AT chenli researchonsimplificationofloadingspectrumforfatiguecrackgrowthtest |