首页> 外文会议>ASME Turbo Expo vol.3 pt.A; 20050606-09; Reno-Tahoe,NV(US) >Buoyancy Effects on Heat Transfer in Five Different Aspect-Ratio Rectangular Channels with Smooth Walls and 45-Degree Ribbed Walls
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Buoyancy Effects on Heat Transfer in Five Different Aspect-Ratio Rectangular Channels with Smooth Walls and 45-Degree Ribbed Walls

机译:五个不同纵横比矩形通道的光滑壁和45度肋壁的浮力对传热的影响

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This paper experimentally studies the effects of the buoyancy force and channel aspect ratio on heat transfer in two-pass rotating rectangular channels with smooth walls and 45° ribbed walls. The channel aspect ratios include 4:1, 2:1, 1:1, 1:2 and 1:4. Four Reynolds numbers are studied: 5000, 10000, 25000 and 40000. The rotation speed is fixed at 550 rpm for all tests, and for each channel, two channel orientations are studied: 90° and 45° or 135°, with respect to the plane of rotation. Rib turbulators are placed on the leading and trailing walls of the channels at an angle of 45° to the flow direction. The ribs have a 1.59 by 1.59 mm square cross section, and the rib pitch-to-height ratio (P/e) is 10 for all tests. The effects of the local buoyancy parameter and channel aspect ratio on the regional Nusselt number ratio are presented. The results show that increasing the local buoyancy parameter increases the Nusselt number ratio on the trailing surface and decreases the Nusselt number ratio on the leading surface in the first pass for all channels. However, the trend of the Nusselt number ratio in the second pass is more complicated due to the strong effect of the 180° turn. Results are also presented for this critical turn region of the two-pass channels. In addition to these regions, the channel averaged heat transfer, friction factor, and thermal performance are determined for each channel. With the channels having comparable Nusselt number ratios, the 1:4 channel has the superior thermal performance because it incurs the least pressure penalty.
机译:本文通过实验研究了浮力和通道纵横比对光滑壁面和45°带肋壁的两遍旋转矩形通道中传热的影响。通道宽高比包括4:1、2:1、1:1、1:2和1:4。研究了四个雷诺数:5000、10000、25000和40000。所有测试的转速固定为550 rpm,对于每个通道,研究了两个通道方向:相对于90°和45°或135°。旋转平面。肋湍流器以与流动方向成45°的角度放置在通道的前壁和后壁上。肋条的横截面为1.59 x 1.59 mm的正方形,所有测试的肋条螺距与高度之比(P / e)为10。提出了局部浮力参数和通道长宽比对区域努塞尔特数比的影响。结果表明,对于所有通道,在第一遍中,增加局部浮力参数会增加尾部表面上的Nusselt数比,并减小尾部表面上的Nusselt数比。然而,由于180°转弯的强烈影响,第二遍中的努塞尔特数比的趋势更加复杂。还给出了两通通道的关键转弯区域的结果。除了这些区域之外,还确定了每个通道的通道平均传热,摩擦系数和热性能。在通道具有可比较的努塞尔数比的情况下,1:4通道具有出色的热性能,因为它产生的压力损失最小。

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