SECONDARY BENDING ANALYSIS OF AIRPLANE TYPICAL SINGLE-SHEAR LAP JOINT
As an important structural component of a plane in its fatigue design,typical single-shear lap joint usually requires the analysis of its secondary bending. With the flat shells, by rational modelestablishing and analysis, the papergot the secondary bending of all fatigue detail points. At the same...
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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.1001.9669.2019.02.021 |
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| _version_ | 1841535649271775232 |
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| author | YANG Jing JIANG XingChang WANG HuiMei |
| author_facet | YANG Jing JIANG XingChang WANG HuiMei |
| author_sort | YANG Jing |
| collection | DOAJ |
| description | As an important structural component of a plane in its fatigue design,typical single-shear lap joint usually requires the analysis of its secondary bending. With the flat shells, by rational modelestablishing and analysis, the papergot the secondary bending of all fatigue detail points. At the same time, the paper validated the flat shells method. The calculation results and conclusionspresented in the paper are of reference value for the fatigue design of airplane’s typical single-shear lap jointstructures. |
| format | Article |
| id | doaj-art-b84746cb5e744c89a476a5cdffbb3b1c |
| institution | Kabale University |
| 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-b84746cb5e744c89a476a5cdffbb3b1c2025-01-15T02:30:29ZzhoEditorial Office of Journal of Mechanical StrengthJixie qiangdu1001-96692019-01-014138939230604627SECONDARY BENDING ANALYSIS OF AIRPLANE TYPICAL SINGLE-SHEAR LAP JOINTYANG JingJIANG XingChangWANG HuiMeiAs an important structural component of a plane in its fatigue design,typical single-shear lap joint usually requires the analysis of its secondary bending. With the flat shells, by rational modelestablishing and analysis, the papergot the secondary bending of all fatigue detail points. At the same time, the paper validated the flat shells method. The calculation results and conclusionspresented in the paper are of reference value for the fatigue design of airplane’s typical single-shear lap jointstructures.http://www.jxqd.net.cn/thesisDetails#10.16579/j.issn.1001.9669.2019.02.021Single-shear lap jointThe secondary bendingThe flat shells methodMethod validation |
| spellingShingle | YANG Jing JIANG XingChang WANG HuiMei SECONDARY BENDING ANALYSIS OF AIRPLANE TYPICAL SINGLE-SHEAR LAP JOINT Jixie qiangdu Single-shear lap joint The secondary bending The flat shells method Method validation |
| title | SECONDARY BENDING ANALYSIS OF AIRPLANE TYPICAL SINGLE-SHEAR LAP JOINT |
| title_full | SECONDARY BENDING ANALYSIS OF AIRPLANE TYPICAL SINGLE-SHEAR LAP JOINT |
| title_fullStr | SECONDARY BENDING ANALYSIS OF AIRPLANE TYPICAL SINGLE-SHEAR LAP JOINT |
| title_full_unstemmed | SECONDARY BENDING ANALYSIS OF AIRPLANE TYPICAL SINGLE-SHEAR LAP JOINT |
| title_short | SECONDARY BENDING ANALYSIS OF AIRPLANE TYPICAL SINGLE-SHEAR LAP JOINT |
| title_sort | secondary bending analysis of airplane typical single shear lap joint |
| topic | Single-shear lap joint The secondary bending The flat shells method Method validation |
| url | http://www.jxqd.net.cn/thesisDetails#10.16579/j.issn.1001.9669.2019.02.021 |
| work_keys_str_mv | AT yangjing secondarybendinganalysisofairplanetypicalsingleshearlapjoint AT jiangxingchang secondarybendinganalysisofairplanetypicalsingleshearlapjoint AT wanghuimei secondarybendinganalysisofairplanetypicalsingleshearlapjoint |