航空发动机叶片气动弹性动力响应的数值方法研究进展

张章; 侯安平; 脱伟; 夏爱国

doi:10.6052/1000-0992-11-121

航空发动机叶片气动弹性动力响应的数值方法研究进展

doi: 10.6052/1000-0992-11-121

张章^1, ,,
侯安平¹,
脱伟²,
夏爱国²

1.
北京航空航天大学航空发动机气动热力重点实验室, 北京 100191
2. 北京航空工程技术研究中心, 北京 100076

基金项目: 国家自然科学基金重点资助项目(60934001)

详细信息

作者简介:
侯安平,1975年生,湖南常德人.2003年毕业于北航动力学院并获得博士学位.2004～2005年在北航博士后流动站作博士后研究,2005年底留校任教,2006年评为副教授.现任北航高等工程学院副院长、北航理学基础部部长,中国空气动力学会气动弹性专业委员会委员.主要研究方向为叶轮机械气动弹性、叶轮机械非定常流动机理、风扇/压气机气动设计.已经完成或正在进行的工作主要涉及压气机气动弹性、涡轮气热固耦合、压气机进气畸变及高负荷风扇/压气机气动优化设计等工作.

通讯作者:
张章

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出版历程
- 收稿日期: 2011-08-29
- 修回日期: 2012-05-25
- 刊出日期: 2012-09-25

A REVIEW OF NUMERICAL RESEARCH ON AEROELASTIC DYNAMICAL RESPONSE OF AERO-ENGINE BLADES

1.
Chinese National Key Laboratory of Aerodynamics & Thermodynamics on Aero-engine, Beihang University, Beijing 100191, China
2. Beijing Aeronautical Technology Research Center, Beijing 100076, China

Funds: The project was supported by the National Natural Science Foundation of China (60934001).

More Information

Corresponding author: ZHANG Zhang

摘要

摘要: 流动诱发振动造成的航空发动机叶片高周疲劳失效问题深受关注.对叶片的气动弹性动力响应研究的数值方法及进展进行了回顾,总结了航空发动机叶片振动响应实验研究和数值模拟研究的典型成果与特点,并对未来研究发展趋势进行展望.指出进一步的机理研究将集中于不稳定流动因素引发叶片强迫振动发作规律的探索以及更贴近流固耦合物理机制的气动弹性数值模拟方法的发展;在工程需求牵引下,建立适用于工程预测的动力响应分析模型,在设计过程中科学评价叶片气动弹性动力响应问题的潜在风险和发展流动控制基础上的气动阻尼减振技术值得进一步关注.
- 叶片 /
- 气动弹性 /
- 动力响应 /
- 数值模拟 /
- 流固耦合
Abstract: The high cycle fatigue failure of aero-engine blades occurs frequently.Aeroelastic dynamic response is a major concern in engineer applications.A review of numerical researches on blade aeroelastic dynamic response is presented in the paper,including numerical simulation,test study and possible research trends.The flow-induced vibration mechanism of blade dynamic response and the numerical method about fluid-structure interaction will be the focus in further mechanism study.For engineer applications,it is valuable to develop a prediction model for dynamic response and to evaluate its potential risks with resonance in the design process.And more attention should be paid on the aerodynamic damping technology based on flow control.
- blade /
- aeroelasticity /
- dynamic response /
- numerical simulation /
- fluid-structure interaction

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