| 波形隔板形状对通道流动和换热的影响 |
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| 引用本文： | 李莉,徐国强,丁水汀,邓宏武.波形隔板形状对通道流动和换热的影响[J].航空动力学报,2011,26(9):1941-1946. |
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| 作者姓名： | 李莉 徐国强 丁水汀 邓宏武 |
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| 作者单位： | 1. 北京航空航天大学能源与动力工程学院航空发动机气动热力国家级重点实验室,北京100191／华北电力大学能源动力与机械工程学院,北京102206
2. 北京航空航天大学能源与动力工程学院航空发动机气动热力国家级重点实验室,北京,100191 |
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| 摘 要： | 采用数值模拟的方法,对基于波形隔板结构涡轮叶片尾缘复合通道的换热和流阻特性进行研究.设计了一种直隔板和三种不同折角的波形隔板结构,研究波形角度对通道中流动和换热的影响.数值结果表明,波形隔板结构折角越小,对整个通道,换热越好,尤其是对于第1通道,换热增强最大可达30%;同时折角越小,通道的流阻系数越大;从换热和流阻的综...
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| 关 键 词： | 换热 流阻 折角 数值模拟 涡轮叶片 |
| 收稿时间： | 2010/9/28 0:00:00 |
| 修稿时间： | 2011/4/14 0:00:00 |
Effect of the shape of divider wall on heat transfer and flow resistance characteristic of passage |
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| LI Li,XU Guo-qiang,DING Shui-ting and DENG Hong-wu.Effect of the shape of divider wall on heat transfer and flow resistance characteristic of passage[J].Journal of Aerospace Power,2011,26(9):1941-1946. |
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| Authors: | LI Li XU Guo-qiang DING Shui-ting and DENG Hong-wu |
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| Institution: | National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics, School of Jet Propulsion, Beijing University of Aeronautics and Astronautics, Beijing 100191, China;School of Energy and Mechanical Engineering, North China Electric Power University, Beijing 102206, China;National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics, School of Jet Propulsion, Beijing University of Aeronautics and Astronautics, Beijing 100191, China;National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics, School of Jet Propulsion, Beijing University of Aeronautics and Astronautics, Beijing 100191, China;National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics, School of Jet Propulsion, Beijing University of Aeronautics and Astronautics, Beijing 100191, China |
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| Abstract: | Numerical simulation was performed to obtain heat transfer and flow resistance characteristics in a channel with zigzag divider wall in the trailing edge passage of turbine blade.One traditional divider wall and three configurations of zigzag divider walls with different angles were applied to research the effect of angle on the heat transfer and flow resistance.The calculated results indicate that the heat transfer is improved with decrease of the angle of the zigzag shape.For the first passage,the highest improvement was nearly 30 percent.At the same time,the passage with small angle divider wall encountered bigger flow resistance.By comparison of integrated effect of heat transfer,the configurations with smaller angle divider walls have higher values than those with larger angle divider walls. |
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| Keywords: | heat transfer flow resistance angle numerical simulation turbine blade |
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