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Heat transfer characteristics in a narrow confined channel with discrete impingement cooling
作者姓名:Yang LI  Tao LIU  Jianjun TAO  Weihua YANG  Likun DONG
作者单位:1. Hunan Key Laboratory of Turbomachinery on Small and Medium Aero-Engine, AECC Hunan Aviation Powerplant Research Institute;2. College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics
基金项目:supported by Hunan Provincial Natural Science Foundation of China (No. 2019JJ50701);
摘    要:Heat transfer characteristics in a narrow confined channel with discrete impingement cooling were investigated using thermal infrared camera. Detailed heat transfer distributions and comparisons on three surfaces with three impact diameters were experimentally studied in the range of Reynolds number of 3000 to 30000. The experimental results indicated that the strong impingement jet leaded to a high strength heat transfer zone in the ΔX=±2.5Dj range of the impact center,which was 1.3–...

收稿时间:14 December 2020

Heat transfer characteristics in a narrow confined channel with discrete impingement cooling
Yang LI,Tao LIU,Jianjun TAO,Weihua YANG,Likun DONG.Heat transfer characteristics in a narrow confined channel with discrete impingement cooling[J].Chinese Journal of Aeronautics,2022,35(4):220-229.
Institution:1. Hunan Key Laboratory of Turbomachinery on Small and Medium Aero-Engine, AECC Hunan Aviation Powerplant Research Institute, Zhuzhou 412002, China;2. College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
Abstract:Heat transfer characteristics in a narrow confined channel with discrete impingement cooling were investigated using thermal infrared camera. Detailed heat transfer distributions and comparisons on three surfaces with three impact diameters were experimentally studied in the range of Reynolds number of 3000 to 30000. The experimental results indicated that the strong impingement jet leaded to a high strength heat transfer zone in the ΔX=±2.5Dj range of the impact center, which was 1.3–2.5 times of the average heat transfer value of the impingement wall. With the same coolant mass flow rate, small diameter case had lower heat transfer coefficient on both inner wall and outside wall, while the impingement wall was insensitive to the impact diameter. The surface averaged Nusselt number of inner wall was only 43%–57% of impingement wall, while the outside wall can reach up to 80%–90%. The larger the diameter, the higher heat transfer enhancement and the smaller the channel flow resistance was observed in term of Reynolds number. The surface averaged Nusselt numbers were developed as the function of Reynolds number and the impingement height-to-diameter for further engineering applications.
Keywords:Aero-engine  Heat transfer characteristics  Impingement cooling  Narrow confined channel  Turbine blade
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