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Buoyancy effect on heat transfer in rotating smooth square U-duct at high rotation number

机译:高旋转数下旋转方形U形管道中浮力对传热的影响

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The buoyancy effect on heat transfer in a rotating, two-pass, square channel is experimentally investigated in current work. The classical copper plate technique is performed to measure the regional averaged heat transfer coefficients. In order to perform a fundamental research, all turbulators are removed away. Two approaches of altering Buoyancy numbers are selected: varying rotation number from 0 to 2.08 at Reynolds number ranges of 10000 to 70000, and varying inlet density ratio from 0.07 to 0.16 at Reynolds number of 10000. And thus, Buoyancy numbers range from 0 to 12.9 for both cases. According to the experimental results, the relationships between heat transfer and Buoyancy numbers are in accord with those obtained under different rotation numbers. For both leading and trailing surface, a critical Buoyancy number exists for each X / D location. Before the critical point, the effect of Buoyancy number on heat transfer is limited; but after that, the Nusselt number ratios show different increase rate. Given the same rotation number, higher wall temperature ratios with its corresponding higher Buoyancy numbers substantially enhance heat transfer on both passages. And the critical exceed-point that heat transfer from trailing surface higher than leading surface happens at the same Buoyancy number for different wall temperature ratios in the second passage. Thus, the stronger buoyancy effect promotes heat transfer enhancement at high rotation number condition.
机译:在当前的工作中,通过实验研究了旋转的,两通道,方形通道中浮力对传热的影响。执行经典的铜板技术以测量区域平均传热系数。为了进行基础研究,将所有湍流器都移开了。选择了两种更改浮力数的方法:在10000到70000的雷诺数范围内将旋转数从0更改为2.08,在10000的雷诺数的范围内将入口密度比从0.07更改为0.16。因此,浮力数在0到12.9范围内。对于这两种情况。根据实验结果,传热和浮力数之间的关系与在不同转数下得到的关系一致。对于前导表面和尾随表面,每个X / D位置都存在一个临界浮力值。在临界点之前,浮力数对传热的影响是有限的。但此后,努塞尔特数比率显示出不同的增长率。在给定相同的转数的情况下,较高的壁温比及其相应的较高的浮力数会大大增强两个通道上的传热。对于第二通道中不同的壁温比,从后表面传热到前表面传热的临界超出点发生在相同的浮力数下。因此,较强的浮力作用在高转数条件下促进了传热的增强。

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