PROCESS PARAMETER MATCHING RESEARCH ON COMPOSITE STRENGTHENING OF TITANIUM ALLOY LUG STRUCTURAL
In order to improve the fatigue performance of the aviation lug structure,a finite element（FE） model of composite strengthening process which contains cold expansion and interference fit has been established. The influence of technological parameters on plastic deformation around hole and fatigue li...
| Main Authors: | , , , , |
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| Format: | Article |
| Language: | zho |
| Published: |
Editorial Office of Journal of Mechanical Strength
2020-01-01
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| Series: | Jixie qiangdu |
| Subjects: | |
| Online Access: | http://www.jxqd.net.cn/thesisDetails#10.16579/j.issn.1001.9669.2020.04.030 |