摘要
The aeroelasticity (especially the aerothermoelasticity) of the high-speed aircraft is raising more and more attention in recent years. First of all, this paper summarizes the recent progress of the aeroelasticity problems according to different numerical methodologies. Then, based on the problems emerging in engineering practice, the thermal aeroelastic problems of high-speed vehicles are divided into issues related to thermal aeroelasticity of the aircraft and the thermal aeroelasticity of the inner runners, and their research status and future development are discussed. Particularly, the aerothermoelasticity problems related to the engine (including the panel flutter inside the ramjet engine and the aeroelasticity of the rocket engine nozzle) are investigated in detail and the significance of this issue in future work is pointed out.
| 投稿的翻译标题 | Progress and prospects on aeroelasticity of hypersonic vehicles |
|---|---|
| 源语言 | 繁体中文 |
| 页(从-至) | 984-994 |
| 页数 | 11 |
| 期刊 | Kongqi Donglixue Xuebao/Acta Aerodynamica Sinica |
| 卷 | 36 |
| 期 | 6 |
| DOI | |
| 出版状态 | 已出版 - 1 12月 2018 |
关键词
- Aerothermoelasticity
- Fluid-structure coupling
- Hypersonic speed vehicles
- Nozzles
- Scramjet
指纹
探究 '高超声速飞行器气动弹性的近期进展与发展展望' 的科研主题。它们共同构成独一无二的指纹。引用此
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