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Inlet flow effects in micro-channels in the laminar and transitional regimes on single-phase heat transfer coefficients and friction factors

机译:层流和过渡状态下微通道中的入口流动对单相传热系数和摩擦系数的影响

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An experimental investigation of heat transfer and pressure drop in rectangular micro-channels was conducted for water in the laminar and transitional regimes for three different inlet configurations. The inlet types under consideration were the sudden contraction, bellmouth, and swirl inlet types, and hydraulic diameters of 0.57, 0.85, and 1.05 mm were covered. It was found that the critical Reynolds number and the transitional behaviour in terms of heat transfer coefficients and friction factors were influenced significantly by the inlet type. For the sudden contraction inlet type, which were investigated for both adiabatic, as well as diabatic cases, adiabatic friction factors were predicted well by the laminar Shah and London correlation, while diabatic friction factors were decreased with an increase in wall heat flux. The sudden contraction inlet critical Reynolds numbers were found to be between 1800 and 2000 for adiabatic cases, while for diabatic cases the transition regime commenced at a Reynolds number of about 2000. The bellmouth and swirl inlet types were mostly investigated for diabatic cases only with swirl inlet tests limited to the 1.05 mm channel. Laminar friction factors were approximately similar to those of the sudden contraction inlet type, however, after the commencement of transition both inlet types exhibited higher friction factors than the sudden contraction inlet. Minor transition occurred as early as at Reynolds numbers of 1200 and 800 for the bellmouth and swirl inlet types respectively while major transition occurred at Reynolds numbers of approximately 1800 and 1500 respectively. Critical Reynolds numbers were found not be significantly influenced by the channel diameter to length ratio considered in this study. Laminar Nusselt numbers were predicted well by conventional macro-channel thermal entry correlations. The swirl inlet type exhibited the highest friction factors and Nusselt numbers in the transitional regime followed by the bellmouth inlet type. During transition while compared with the sudden contraction inlet, both the bellmouth and swirl inlet types exhibited larger enhancement in heat transfer than increases in the friction factor penalty. Based on the experimental data obtained in this study, a set of correlations were developed which describes the relation between the friction factor and Colburn j-factor. Depending on the inlet type, the correlations predicted between 94% and 100% of the results to within 10% of the experimental measurements.
机译:针对三种不同的入口构造,在层流和过渡状态下对矩形水进行了矩形微通道内传热和压降的实验研究。所考虑的入口类型为突然收缩,喇叭形和涡流入口类型,并且覆盖了0.57、0.85和1.05 mm的水力直径。已经发现,临界雷诺数和关于传热系数和摩擦系数的过渡行为受入口类型的影响很大。对于绝热和绝热情况下的突然收缩进气口类型,通过层流Shah和London相关性可以很好地预测绝热摩擦因子,而绝热摩擦因子随着壁热通量的增加而减小。绝热病例的突然收缩入口临界雷诺数在1800至2000之间,而非绝热病例的过渡状态始于约2000的雷诺数。入口测试仅限于1.05毫米通道。层流摩擦系数与突然收缩入口类型的摩擦系数近似相似,但是,过渡开始后,两种入口类型均显示出比突然收缩入口更高的摩擦系数。钟形和旋流进气口类型的雷诺数分别在1200和800时发生次要转变,而雷诺数分别为1800和1500时发生次要转变。发现在该研究中考虑的临界雷诺数不受通道直径与长度之比的显着影响。通过常规的宏通道热进入相关性可以很好地预测层流努塞尔数。涡流入口类型在过渡态中表现出最高的摩擦系数和Nusselt数,其次是喇叭口入口类型。在过渡期间,与突然收缩的进气口相比,喇叭形和涡流进气口类型的传热增强都大于摩擦系数损失的增大。根据这项研究中获得的实验数据,开发了一组相关性,这些相关性描述了摩擦系数和Colburn j系数之间的关系。根据进样口的类型,相关性可预测结果的94%和100%之间,以及实验测量值的10%以内。

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