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Numerical study of local heat transfer coefficient and fin efficiency of wavy fin-and-tube heat exchangers

机译:波浪形翅片管换热器局部传热系数和翅片效率的数值研究

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Three-dimensional numerical simulations were performed for laminar flow of wavy fin-and-tube heat exchangers by using body-fitted coordinates (BFC) method with fin efficiency effect accounted. The prediction results of average Nusselt number, friction factor and fin efficiency were compared with the related experimental correlations [R. C. Xin, H. Z. Li, H. J. Kang, W. Li, W. Q. Tao, An experimental investigation on heat transfer and pressure drop characteristics of triangular wavy fin-and-tube heat exchanger surfaces, J. Xi'an Jiaotong Univ. 28 (2) (1994) 77-83] and Schmidt approximation [T. E. Schmidt, Heat transfer calculations for extended surfaces, Refrigerating Engineering (April 1949) 351-357]. For Reynolds numbers based on the tube outside diameter ranging from 500 to 4000, the mean deviation is 3.3% for Nusselt number, 1.9% for friction factor and 3.6% for fin efficiency. The distributions of local Nusselt number and fin efficiency on fin surface were studied at wavy angle equal to 0° (plain plate fin), 10° and 20° respectively. The local Nusselt number decreases along the air flow direction, but fin efficiency increases in general. The wavy angle can greatly affect the distributions of local Nusselt number and fin efficiency, and make the distributions present fluctuation along the flow direction. The result also shows that the fin efficiency at the inlet region of wavy fin is larger than that of plain plate fin at the same region. With the increase of Reynolds number, the effects of wavy angle on the distributions of local Nusselt number and fin efficiency are more and more significant.
机译:利用体拟合坐标(BFC)方法对翅片管换热器的层流进行了三维数值模拟,并考虑了翅片效率的影响。将平均Nusselt数,摩擦系数和散热片效率的预测结果与相关的实验相关性进行了比较[R. C. Xin,H.Z. Li,H.J.Kang,W.Li,W.Q.Tao,三角形波浪翅片管换热器表面传热和压降特性的实验研究,西安交通大学。 28(2)(1994)77-83]和施密特逼近[T. E. Schmidt,“扩展表面的传热计算”,制冷工程(1949年4月)351-357]。对于基于管外径(从500到4000)的雷诺数,Nusselt数的平均偏差为3.3%,摩擦因数的平均偏差为1.9%,翅片效率的平均偏差为3.6%。在波浪角分别等于0°(普通平板鳍),10°和20°的波浪角上研究了鳍表面上的局部Nusselt数和鳍效率。局部Nusselt数沿空气流动方向减少,但鳍片效率总体上增加。波浪角会极大地影响局部Nusselt数和翅片效率的分布,并使分布沿流动方向呈现波动。结果还表明,在相同区域,波浪形翅片进口区域的翅片效率要大于平板状翅片。随着雷诺数的增加,波浪角对局部Nusselt数分布和鳍效率的影响越来越显着。

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