| 直接供气预旋转静系的换热 |
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| 引用本文： | 徐国强,赵熙,罗翔,蔡旭,余鸿鹏.直接供气预旋转静系的换热[J].航空动力学报,2012,27(10):2161-2168. |
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| 作者姓名： | 徐国强 赵熙 罗翔 蔡旭 余鸿鹏 |
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| 作者单位： | 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： | 用实验方法研究了直接供气转静系预旋腔内转盘表而的换热情况得到了转盘表而的局部努塞尔数分布云图、周向平均努塞尔数沿径向的分布以及转盘表而平均努塞尔数随转速和流量的变化规律.实验结果表明：相同流量系数下旋转雷诺数较低时主盘而局部努塞尔数的峰值区出现在低半径小分离区的上方，旋转雷诺数较高时，局部努塞尔数的峰值区向高半径移动和扩展，且覆盖的半径范围变宽.相同旋转雷诺数下，流量系数越大，局部努塞尔数的峰值区向低半径移动，其覆盖的半径范围变窄；主盘面的平均努塞尔数与旋转雷诺数或流量系数均呈单调增大关系.
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| 关 键 词： | 直接供气系统 转静系 预旋 旋转盘腔 换热 |
| 收稿时间： | 1/4/2012 12:00:00 AM |
Heat transfer in direct transfer pre-swirl rotor-stator system |
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| XU Guo-qiang,ZHAO Xi,LUO Xiang,CAI Xu and YU Hong-peng.Heat transfer in direct transfer pre-swirl rotor-stator system[J].Journal of Aerospace Power,2012,27(10):2161-2168. |
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| Authors: | XU Guo-qiang ZHAO Xi LUO Xiang CAI Xu and YU Hong-peng |
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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;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;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: | Heat transfer of direct transfer pre-swirl rotor-stator system was investigated by experiments.Contours of local Nusselt number on the rotating disk,distribution of circumferential-averaged Nusselt number along radial direction,and variation of average Nusselt number with rotating Reynolds number and mass flow rate coefficient were obtained.The results show that with the same mass flow rate and low rotational Reynolds number,peak zones of local Nusselt number arise at small radius.When rotational Reynolds number increases,peak zones of local Nusselt number move to larger radius and expand.With the same rotational Reynolds number,peak zones of local Nusselt number move to smaller radius and their ranges decreases.Average Nusselt number would increase when rotational Reynolds number or mass flow rate coefficient increases. |
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| Keywords: | direct transfer system rotor-stator pre-swirl rotating cavity heat transfer |
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