首页> 外文会议>ASME turbo expo >EFFECT OF RIB SPACING ON HEAT TRANSFER IN A TWO-PASS RECTANGULAR CHANNEL (AR=1:4) WITH A SHARP ENTRANCE AT HIGH ROTATION NUMBERS
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EFFECT OF RIB SPACING ON HEAT TRANSFER IN A TWO-PASS RECTANGULAR CHANNEL (AR=1:4) WITH A SHARP ENTRANCE AT HIGH ROTATION NUMBERS

机译:在高旋转数下具有锐利入口的两通道矩形通道(AR = 1:4)中肋间距对传热的影响

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The focus of the current study was to determine the effects of rib spacing on heat transfer in rotating 1:4 AR channels. In the current study, heat transfer experiments were performed in a two-pass, 1:4 aspect ratio channel, with a sharp bend entrance. The channel leading and trailing walls in the first pass and second pass utilized angled rib turbulators (45° to the mainstream flow). The rib height-to-hydraulic diameter ratio (e/Dh) was held constant at 0.078. The channel was oriented 90° to the direction of rotation. Three rib pitch-to-rib height ratios (P/e) were studied: P/e = 2.5, 5, and 10. Each ratio was tested at five Reynolds numbers: 10K, 15K, 20K, 30K and 40K. For each Reynolds number, experiments were conducted at five rotational speeds: 0, 100, 200, 300, and 400 rpm. Results showed that the sharp bend entrance has a significant effect on the first pass heat transfer enhancement. In the second pass, the rib spacing and rotation effect are reduced. The P/e=10 case had the highest heat transfer enhancement based on total area, whereas the P/e=2.5 had the highest heat transfer enhancement based on the projected area. The current study has extended the range of the rotation number (Ro) and local buoyancy parameter (Bo_x) for a ribbed 1:4 aspect ratio channel up to 0.65 and 1.5, respectively. Correlations for predicting heat transfer enhancement, due to rotation, in the ribbed (P/e=2.5, 5, and 10) 1:4 aspect ratio channel, based on the extended range of the rotation number and buoyancy parameter, are presented in the paper.
机译:当前研究的重点是确定肋骨间距对旋转的1:4 AR通道中的热传递的影响。在当前的研究中,传热实验是在长宽比为1:4的两通道通道中进行的,该通道具有急剧的弯曲入口。第一遍和第二遍的通道前壁和后壁使用成角度的肋湍流器(与主流成45度角)。肋骨高度与液压直径之比(e / Dh)保持恒定为0.078。通道与旋转方向成90°角。研究了三个肋距与肋的高度比(P / e):P / e = 2.5、5和10。每个比率都以五个雷诺数测试:10K,15K,20K,30K和40K。对于每个雷诺数,以五种转速进行实验:0、100、200、300和400 rpm。结果表明,急弯入口对首过传热的增强有显着影响。在第二遍中,肋间距和旋转效果减小。 P / e = 10的情况下,基于总面积的传热增强最高,而P / e = 2.5的情况下,基于投影面积的传热增强最高。当前的研究已将带肋的1:4长宽比通道的旋转数(Ro)和局部浮力参数(Bo_x)的范围分别扩展到了0.65和1.5。基于旋转数和浮力参数的扩展范围,在带肋的(P / e = 2.5、5和10)1:4长宽比通道中预测了由于旋转而引起的传热增强的相关性。纸。

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