| 飞机滑跑响应研究 |
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| 引用本文： | 徐焱. 飞机滑跑响应研究[J]. 飞机设计, 2005, 0(1): 17-19 |
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| 作者姓名： | 徐焱 |
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| 作者单位： | 成都飞机工业(集团)有限责任公司,技术中心,成都,610092 |
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| 摘 要： | 飞机机翼挂装翼尖导弹对机翼结构设计和结构分析提出了诸多全新课题, 如结构的振动响应和气动弹性动响应。本文就某型飞机滑跑的结构振动响应做了初步分析。
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| 关 键 词： | 机翼 翼尖弹 滑跑 振动 响应 频率 |
| 修稿时间： | 2003-12-01 |
An Analysis of Vibration Response of Structures to Aircraft Running |
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| Xu Yan. An Analysis of Vibration Response of Structures to Aircraft Running[J]. Aircraft Design, 2005, 0(1): 17-19 |
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| Authors: | Xu Yan |
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| Abstract: | Missile carrying on the wing tip causes the wing structure design and analysis to face many challenges, such as structural vibration response and aeroelastic response. This paper presents an analysis of vibration response of structures in course of running of an aircraft. |
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| Keywords: | wing wing-tip missile running dynamic response frequency |
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