工程车辆翼型管散热器冷侧翅片信噪比分析
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  • 英文篇名:Signal to Noise Ratio Analysis on Air-side Fin From Radiators With NACA Airfoil Tubes for Construction Vehicles
  • 作者:王宝中 ; 冯少聪 ; 刘佳鑫 ; 蒋炎坤
  • 英文作者:WANG Bao-Zhong;FENG Shao-Cong;LIU Jia-Xin;JIANG Yan-Kun;School of Mechanical Engineering, North China University of Science and Technology;School of Energy and Power Engineering Huazhong University of Science and Technology;
  • 关键词:散热器 ; 数值仿真 ; 翼型管 ; 综合评价因子 ; 信噪比
  • 英文关键词:radiator;;numerical simulation;;wing-shaped tube;;comprehensive evaluation factor;;signal-to-noise ratio
  • 中文刊名:GCRB
  • 英文刊名:Journal of Engineering Thermophysics
  • 机构:华北理工大学机械工程学院;华中科技大学能源与动力学院;
  • 出版日期:2018-08-15
  • 出版单位:工程热物理学报
  • 年:2018
  • 期:v.39
  • 基金:国家科技支撑计划(No.2013BAF07B04);; 湖北省技术创新专项基金资助项目(No.2016AAA045);; 博士科研启动项目(No.28406999)
  • 语种:中文;
  • 页:GCRB201808033
  • 页数:9
  • CN:08
  • ISSN:11-2091/O4
  • 分类号:209-217
摘要
为提高某工程车辆管片式散热器综合性能,以降低空气侧压力损失为前提,选用NACA23021翼型建立散热器换热管代替原有的扁平管,利用fluent对改进前后散热器空气侧换热系数和压力损失进行仿真分析,并对比两者的综合性能评价因子;进一步分析结构参数对翼型管翅片散热器性能的影响,利用正交试验与信噪比相结合分析各结构参数的敏感度。研究结果表明:在入口空气流速2~10 m/s范围内,散热器空气侧换热系数和压力损失的试验与仿真误差值小于5%;在仿真区间内,NACA23021翼型管翅片的综合评价因子较扁平管翅片略高,在入口10m/s时高出约23%;通过信噪比分析,得出换热管的长径对翼型管散热器性能影响最大,为28.88%,管列距、管类型和管排距对其影响次之,分别为23.91%、20.50%和11.18%,翅片间距和翅片厚度对其影响最小,分别为9.63%和5.90%。
        In order to improve the comprehensive performance of tube-fin radiators for construction vehicles, on the premise of reducing pressure loss, the airfoil NACA23021 was used to shape the tube model of the radiator, and the same simulation method was used to obtain the pressure loss and heat transfer coefficient on the air side, then, the comprehensive performance evaluation factor was acquired. The influence of the structural parameters on the performance of the fin tube fin radiator is further analyzed. The sensitivity of each structural parameter is analyzed by orthogonal test and signal-to-noise ratio. The results show that the error between experimental data and simulation results for the airside pressure loss and heat transfer coefficient is less than 5% over the inlet velocity range from 2 to 10 m/s. In the same range, the comprehensive evaluation factor of NACA23021 airfoil fin is about 23% higher than that of flat fin in the entrance 10 m/s. Through the analysis of signal-to-noise ratio, it is concluded that the heat pipe length diameter of finned tube radiator performance impact, 28.88%, tube spacing, tube type and tube spacing on the influence of the times,were 23.91%, 20.50% and 11.18%, fin pitch and fin thickness with minimal impact on the 9.63% and5.90% respectively.
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