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Performance Evaluation Methods for Multi-stream Plate-Fin Heat Exchanger

机译:多流板翅式换热器性能评估方法

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摘要

Mathematical model of cross type multi-stream plate-fin heat exchanger is established .Meanwhile ,mean square error of accumulative heat load is normalized by dimensionless ,and the equations of temperature-difference uniformity factor are improved .Evaluation factors above and performance of heat exchanger are compared and ana-lyzed by taking aircraft three-stream condenser as an example .The results demonstrate that the mean square error of accumulative heat load is common result of total heat load and excess heat load between passages .So it can be influenced by passage arrangement ,flow inlet parameters as well as flow patterns .Dimensionless parameter of mean square error of accumulative heat load can reflect the influence of passage arrangement to heat exchange per-formance and will not change dramatically with the variation of flow inlet parameters and flow patterns .Tempera-ture-difference uniformity factor is influenced by passage arrangement and flow patterns .It remains basically un-changed under a certain range of flow inlet parameters .
机译:建立了交叉式多流板翅式换热器的数学模型。同时,利用无因次对累积热负荷​​的均方误差进行了归一化,并完善了温差均匀系数方程。以上评价系数及换热器性能以飞机三流冷凝器为例进行比较和分析。结果表明,累积热负荷​​的均方误差是通道间总热负荷和过剩热负荷的共同结果,因此受通道影响蓄热负荷均方误差的无量纲参数可以反映通道布置对换热性能的影响,并且不会随着流入口参数和流型的变化而发生显着变化。温度差均匀性因子受通道排列和流型的影响,它仍然是基础在一定范围内的进水口参数不变。

著录项

  • 来源
    《南京航空航天大学学报(英文版)》 |2017年第5期|553-560|共8页
  • 作者单位

    School of Environmental Science and Engineering,Suzhou University of Science and Technology,Suzhou 215009,P.R.China;

    College of Aerospace Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,P.R.China;

    College of Aerospace Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,P.R.China;

    College of Aerospace Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,P.R.China;

    College of Aerospace Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,P.R.China;

    Aviation Key Laboratory of Science and Technology on Aero Electromechanical System Integration,Nanjing 210016,P.R.China;

  • 收录信息 中国科学引文数据库(CSCD);中国科技论文与引文数据库(CSTPCD);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 一般性问题;
  • 关键词

  • 入库时间 2022-08-18 02:01:17
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