合成射流控制下低压高负荷透平叶片边界层分离大涡模拟

叶冬挺 1; 2; 张荻 1; 蓝吉兵 1; 谢永慧 1

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合成射流控制下低压高负荷透平叶片边界层分离大涡模拟

更新时间：2025-07-09

- 合成射流控制下低压高负荷透平叶片边界层分离大涡模拟
- Large-Eddy Simulation on Boundary Separation of High-Lift Low-Pressure Turbine Blade with Synthetic Jet Control
- 西安交通大学学报 2011年45卷第3期页码：58-64
- 作者机构：
  
  1. 西安交通大学能源与动力工程学院,西安,710049
  2. 上海电气电站设备有限公司,上海,201100
- 作者简介：
- 基金信息：
  
  : 2010-07-24. 作者简介: 叶冬挺(1983-),男,硕士生;谢永慧(联系人),男,教授. 基金项目: 国家高科技研究发展规划资助项目(2009AA04Z102);国家自然科学基金资助项目(10602044)
- DOI：
  中图分类号： TK26
- 网络首发：2011-03-10，
  
  纸质出版：2011
- 稿件说明：
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叶冬挺 1, 2, 张荻 1, 等. 合成射流控制下低压高负荷透平叶片边界层分离大涡模拟[J]. 西安交通大学学报, 2011,45(3):58-64.

Large-Eddy Simulation on Boundary Separation of High-Lift Low-Pressure Turbine Blade with Synthetic Jet Control[J]. 2011, 45(3): 58-64.
叶冬挺 1, 2, 张荻 1, 等. 合成射流控制下低压高负荷透平叶片边界层分离大涡模拟[J]. 西安交通大学学报, 2011,45(3):58-64. DOI：

Large-Eddy Simulation on Boundary Separation of High-Lift Low-Pressure Turbine Blade with Synthetic Jet Control[J]. 2011, 45(3): 58-64. DOI：

摘要

为了研究合成射流对低压高负荷透平叶片边界层流动分离进行控制的效果及机理

采用大涡模拟方法对利用合成射流控制低压高负荷透平Pak-B叶栅内的非稳态流动分离特性进行了研究.在合成射流控制下的结果表明:Pak-B叶栅吸力面流动分离位置变化不大

再附位置明显提前

叶栅吸力面尾缘区域逆压梯度明显减小

总压损失系数降低

分离泡尺寸缩小; 叶栅吸力面大部分剪切层黏附于壁面

也未出现大尺度二维展向涡

静压脉动特征频率向高频转移

低频脉动幅值降低

大尺度涡旋结构发生变化.通过研究还发现:在吹气过程中

边界层外部高能流体被射流卷吸进入边界层内

边界层内流体能量增大进而抑制了分离; 在吸气过程中

射流孔上游区域边界层厚度减小

流速增大

从而抑制了下游流动分离.

Abstract

In order to understand the effect and mechanism of controlling blade boundary flow separation using synthetic jets for a high-lift low-pressure turbine(LPT)cascade

the large-eddy simulation(LES)method was adopted to investigate the unsteady separation flow characteristics of the LPT Pak-B cascade with and without flow control using synthetic jets. The results indicate that the separation location in the controlled case changes slightly but the reattachment location moves upstream significantly on the suction surface of the Pak-B blade. The adverse pressure gradient

total pressure loss coefficient and the size of separation bubble near the cascade trailing edge all decrease remarkably. On the suction surface of the blade

the most part of the shear layer attaches to the wall and the large-scale two-dimensional vortex does not exist. The spectrums of static pressure in the trailing edge of the Pak-B cascade clearly show the conversion of characteristic frequency to high frequency

the decrease of low frequency domain and variation of the large-scale vortex structure. In addition

in the blowing stage

the fluid with high energy out of the boundary layer are entrained into the boundary layer and the energy of the fluid inside the boundary layer increases to inhibit the flow separation; in the suction stage

the boundary layer in the upstream domain of the jet hole becomes thinner and the flow rate rises

inhibiting the flow separation downstream.

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Keywords

references

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