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Heat transfer performance of cross-fin-tube-type heat exchangers with vortex generators

机译:涡流发电机跨翅管型热交换器的传热性能

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We have studied the influence of winglet-stamping hole positions, inclined β angles (winglet face angle to fin surface) and winglets array to cross-fin-tube type fins on heat transfer performance. Heat transfer performance was measured for proto-type heat exchangers with rectangular-type vortex generators by a transient heat transfer measuring method. Results indicate that the backward-stamping winglets (stamping holes positioned downstream to winglets) were 19% higher than forward-stamping winglets ( stamping holes positioned upstream to winglets) during the heat transfer ; The optimal winglet-inclined angle of β =60° which maxmizes the ratio [j{sub}H ]/[friction factor f] and j{sub}H was achieved The winglet array positioned upstream to the pipes was superior to the winglet array positioned downstream to the pipes during both the hear transfer and the pressure drop These data suggest that the corner vortices by using winglets inclined to an upsrtream position [1] is an effective enhancement method during heat transfer.
机译:我们已经研究了小翼冲压孔位置,倾斜β角度(小翼面角度到翅片表面)和小翼阵列对传热性能的跨翅管型翅片的影响。通过瞬态传热测量方法测量具有矩形涡流发生器的原型热交换器的传热性能。结果表明,在热传递期间,后冲压翼(位于飞行下游的冲压孔)比前冲压翅膀(位于前侧上游的冲压孔)高19%; β= 60°的最佳翅倾斜角度,最大化比率[j {sub} h] / [摩擦系数f]和j {sub} h达到朝向管道上游的小翼阵列优于小翼阵列在听到转移和压力下降期间将下游定位在管道上,这些数据表明,通过使用倾斜于upsrtream位置的翼片的角涡流是一种在传热过程中的有效增强方法。

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