| 跨音速轴流压气机叶顶间隙泄漏流对微喷气的非定常响应机制和扩稳效果研究 |
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| 引用本文： | 耿少娟,张宏武,陈静宜,黄伟光. 跨音速轴流压气机叶顶间隙泄漏流对微喷气的非定常响应机制和扩稳效果研究[J]. 工程热物理学报, 2009, 30(12) |
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| 作者姓名： | 耿少娟 张宏武 陈静宜 黄伟光 |
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| 作者单位： | 中国科学院工程热物理研究所,先进能源动力重点实验室,北京,100190 |
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| 基金项目： | 国家重点基础研究发展规划(973计划)，国家自然科学基金 |
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| 摘 要： | 本文将叶顶微喷气方法应用于 NASA Rotor37 跨音速轴流压气机转子,在近失速工况,利用数值模拟方法研究了不同喷气量时叶顶间隙泄漏流对微喷气的非定常响应机理和叶顶微喷气的扩稳效果.结果表明,喷气使得叶顶区域的叶表压力随喷嘴与叶片相对位置的变化沿弦向发生波动,抑制了叶顶泄漏流的自激非定常波动,使叶顶泄漏流轨迹沿叶片吸力面向下游移动,实现了提高压气机性能和稳定性的目的.采用喷射气流的无量纲总动量可关联亚音速和跨音速轴流压气机不同喷气方案的扩稳效果,该无量纲总动量与来流总动量和喷射气流高度成反比,而与叶高和喷射气流总动量成正比.
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| 关 键 词： | 轴流压气机 叶顶间隙流 非定常 喷气 扩稳 |
UNSTEADY RESPONSE OF TIP LEAKAGE FLOW TO DISCRETE MICRO TIP INJECTION IN A TRANSONIC AXIAL COMPRESSOR AND ITS EFFECT ON STABILITY ENHANCEMENT |
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| GENG Shao-Juan,ZHANG Hong-Wu,CHEN Jing-Yi,HUANG Wei-Guang. UNSTEADY RESPONSE OF TIP LEAKAGE FLOW TO DISCRETE MICRO TIP INJECTION IN A TRANSONIC AXIAL COMPRESSOR AND ITS EFFECT ON STABILITY ENHANCEMENT[J]. Journal of Engineering Thermophysics, 2009, 30(12) |
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| Authors: | GENG Shao-Juan ZHANG Hong-Wu CHEN Jing-Yi HUANG Wei-Guang |
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| Affiliation: | GENG Shao-Juan ZHANG Hong-Wu CHEN Jing-Yi HUANG Wei-Guang (Key Laboratory of Advanced Energy and Power,Institute of Engineering Thermophysics,Chinese Academy of Sciences,Beijing 100190,China) |
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| Abstract: | Numerical simulation is utilized to investigate the response mechanism of unsteady tip leakage flow to discrete micro tip injection for the NASA transonic axial compressor Rotor37 at near stall operating point by varying injected mass flow rate.The effects of different injection schemes on stability enhancement are summarized and compared with the experimental results in open literatures. Injection mainly influences the rotor tip region.Under the influence of injected flow,the transient pressure distributio... |
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| Keywords: | axial compressor tip leakage flow unsteady flow air injection stall margin improvement |
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