AIRCRAFT SPOILER SUSPENSION STIFFNESS TEST AND ANALYSIS (MT)
In order to reduce the influence of wing box deformation on the spoiler control surface of an aircraft, a linkage mechanism was adopted for the suspension at both ends of the spoiler. During the stiffness characteristic test, it was found that the monitoring data of the spoiler structure showed a ju...
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| Main Authors: | , |
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| Format: | Article |
| Language: | zho |
| Published: |
Editorial Office of Journal of Mechanical Strength
2023-01-01
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| Series: | Jixie qiangdu |
| Subjects: | |
| Online Access: | http://www.jxqd.net.cn/thesisDetails#10.16579/j.issn.1001.9669.2023.01.031 |
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