摘要
In the process of aircraft service, it will experience complex dynamic processes such as ground taxiing and maneuver etc. The aircraft structure and airborne equipment will bear the individual or joint effect of various dynamic loads during these processes. The induced structural dynamic problems are directly related to the aircraft service safety and passengers' ride comfort. This paper sorts out the requirements of structural dynamics in the military airplane structural integrity program and strength specification, as well as the airworthiness regulation of civil aircraft. The relationship between the structural dynamics and R&D of aviation equipment is presented. The main issues of aircraft structural dynamics are classified from the aspects of loads, structure, response and control. At last, the prospect of aircraft structural dynamics is briefly concluded considering the needs in aircraft equipment research and the newly developed vibration techniques.
投稿的翻译标题 | Progress and prospect of aviation structural dynamics research |
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源语言 | 繁体中文 |
页(从-至) | 409-436 |
页数 | 28 |
期刊 | Yingyong Lixue Xuebao/Chinese Journal of Applied Mechanics |
卷 | 39 |
期 | 3 |
DOI | |
出版状态 | 已出版 - 15 6月 2022 |
关键词
- Aircraft structure
- Dynamic load
- Extreme environment
- Structural dynamics
- Vibration control
- Vibration fatigue