摘要
An energy method was proposed to consider the effect of the wake induced by the upstream stator on the aeroelasticity of the rotor blade based on the phase lagged method, and then validated by the time-marching method. The effects of wake on aerodynamic damping of rotor blades under different modes and interblade phase angles were investigated. The results showed that the wake had a significant effect on the aeroelasticity of the rotor blades, and can be simulated by the developed method accurately and efficiently. Compared with the first torsional mode, the wake had a more serious impact on the aeroelasticity of the first bending mode. Furthermore, for different interblade phase angles, the wake can weaken the low aerodynamic damping and strengthen the high damping for the first bending mode, in contrast to the first torsion mode.
| 投稿的翻译标题 | Influence of stator wake on aeroelasticity of rotor blade |
|---|---|
| 源语言 | 繁体中文 |
| 页(从-至) | 2219-2227 |
| 页数 | 9 |
| 期刊 | Hangkong Dongli Xuebao/Journal of Aerospace Power |
| 卷 | 33 |
| 期 | 9 |
| DOI | |
| 出版状态 | 已出版 - 1 9月 2018 |
关键词
- Aeroelasticity
- Interblade phase angle
- Modal shape
- Turbomachinery
- Wake
指纹
探究 '静子尾迹对转子叶片气弹稳定性的影响' 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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