| 航空发动机高压旋转涡轮盘腔流动与换热 |
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| 引用本文： | 丁水汀,张东,陶智,徐国强.航空发动机高压旋转涡轮盘腔流动与换热[J].推进技术,2003,24(2):118-121. |
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| 作者姓名： | 丁水汀 张东 陶智 徐国强 |
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| 作者单位： | 北京航空航天大学,动力系,北京,100083 |
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| 摘 要： | 在同模型实验参数范围内，且数值解和实验解基本吻合的前提下，对发动机原型参数进行数值模拟，求解了旋转系下流体流动与换热微分方程组，通过对气体域和固体域进行共扼计算，并将动量方程与能量方程福合求解。结果表明利用低参数下实验数据支持的数值计算程序对真实参数的模拟是合理的，对于复杂的非线性现象，数值外推法比传统实验外推更加准确。
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| 关 键 词： | 航空发动机 涡轮盘 传热 混合长度流动理论 数值仿真 |
| 文章编号： | 1001-4055(2003)02-0118-04 |
| 修稿时间： | 2002年2月25日 |
Numerical simulation for flow and heat transfer of a rotating turbine cavity with realistic engine parameters |
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| DING Shui-ting,ZHANG Dong,Tao Zhi and XU Guo-qiang.Numerical simulation for flow and heat transfer of a rotating turbine cavity with realistic engine parameters[J].Journal of Propulsion Technology,2003,24(2):118-121. |
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| Authors: | DING Shui-ting ZHANG Dong Tao Zhi and XU Guo-qiang |
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| Institution: | Dept. of Jet Propulsion, Beijing Univ. of Aeronautics and Astronautics, Beijing 100083, China;Dept. of Jet Propulsion, Beijing Univ. of Aeronautics and Astronautics, Beijing 100083, China;Dept. of Jet Propulsion, Beijing Univ. of Aeronautics and Astronautics, Beijing 100083, China;Dept. of Jet Propulsion, Beijing Univ. of Aeronautics and Astronautics, Beijing 100083, China |
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| Abstract: | Numerical simulation was extended with the proposed mixing length equation for the cavity model with realistic engine parameters and the prediction was quite reasonable. It was believed that, for highly non-linear phenomena such as coolant through rotating cavity, this extension was more accurate than direct application of correlations from model tests. |
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| Keywords: | Aircraft engine Turbine wheel Mixing length flow theory Heat transfer Numerical simulation |
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