Mohammed Abed Ahmed, Saad M. Hatem, Ibrahim K. Alabdaly
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Results revealed that the Nusselt number $(\\overline{N u})$, pressure drop, and total entropy $\\left(\\bar{S}_{\\text {total }}\\right)$ escalated in accordance with Re and A. Conversely, they diminished with reduced spacing from the stagnation point to B. Notably, a superior heat transfer rate was observed when employing a target plate integrated with wing ribs in contrast to a rib-less configuration. Performance Evaluation Criteria (PEC) values were noted to augment with rib height increment. It is demonstrated that the PEC increases as A increases. Also, the lower value of PEC equals 1.044 at A of 2 mm, B of 10 mm, and Re of 8000, while the higher value of the PEC equals 1.68 at A of 2 mm, B of 10 mm, and Re of 3000. 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Comparisons were drawn between the heat transfer and entropy generation attributes of two wing ribs positioned on the heated impinging target surface and those of a rib-less surface. The influences of variations in the spacing between the stagnation point and the rib (B) of (10-30 mm), ranging from 10 to 30 mm, rib heights (A) between 0.5 to 2 mm, and a Reynolds number of the jet (Re) between 3000 to 8000 on fluid flow, heat transfer, and entropy generation were elucidated. Employing the Finite Volume Method (FVM) managed the continuity, momentum, and energy equations in adherence to the principles of the SIMPLE methodology. Results revealed that the Nusselt number $(\\\\overline{N u})$, pressure drop, and total entropy $\\\\left(\\\\bar{S}_{\\\\text {total }}\\\\right)$ escalated in accordance with Re and A. Conversely, they diminished with reduced spacing from the stagnation point to B. 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引用次数: 0
摘要
本文采用数值模拟方法研究了窄缝射流冲击下的传热和熵产特性。对比了放置在被加热的撞击目标表面上的两个翼肋与放置在无翼肋表面上的翼肋的传热和熵产特性。研究了驻点与肋间距(B) (10 ~ 30 mm) (10 ~ 30 mm)、肋高(A) (0.5 ~ 2 mm)、射流雷诺数(Re)(3000 ~ 8000)变化对流体流动、换热和熵产的影响。采用有限体积法(FVM)在遵循SIMPLE方法的原则下管理连续性,动量和能量方程。结果表明,努塞尔数$(\overline{N u})$、压降和总熵$\left(\bar{S}_{\text {total }}\right)$随着Re和a的增大而增大,相反,它们随着从驻点到b的间距的减小而减小。值得注意的是,与无肋配置相比,采用翼肋集成靶板的传热率更高。性能评价标准(PEC)值随着肋骨高度的增加而增加。结果表明,PEC随A的增大而增大。在A为2 mm, B为10 mm, Re为8000时,PEC的低值为1.044;在A为2 mm, B为10 mm, Re为3000时,PEC的最高值为1.68。研究结果表明,翼肋补充的缝隙射流撞击在提高电子设备的冷却效率方面起着关键作用。
Numerical Examination of Heat Transfer and Entropy Generation in Confined-Slot Jet Impingement Featuring Wing Ribs
In this study, a numerical investigation into heat transfer and entropy generation characteristics using confined-slot jet impingement was conducted. Comparisons were drawn between the heat transfer and entropy generation attributes of two wing ribs positioned on the heated impinging target surface and those of a rib-less surface. The influences of variations in the spacing between the stagnation point and the rib (B) of (10-30 mm), ranging from 10 to 30 mm, rib heights (A) between 0.5 to 2 mm, and a Reynolds number of the jet (Re) between 3000 to 8000 on fluid flow, heat transfer, and entropy generation were elucidated. Employing the Finite Volume Method (FVM) managed the continuity, momentum, and energy equations in adherence to the principles of the SIMPLE methodology. Results revealed that the Nusselt number $(\overline{N u})$, pressure drop, and total entropy $\left(\bar{S}_{\text {total }}\right)$ escalated in accordance with Re and A. Conversely, they diminished with reduced spacing from the stagnation point to B. Notably, a superior heat transfer rate was observed when employing a target plate integrated with wing ribs in contrast to a rib-less configuration. Performance Evaluation Criteria (PEC) values were noted to augment with rib height increment. It is demonstrated that the PEC increases as A increases. Also, the lower value of PEC equals 1.044 at A of 2 mm, B of 10 mm, and Re of 8000, while the higher value of the PEC equals 1.68 at A of 2 mm, B of 10 mm, and Re of 3000. The findings suggest that slot-Jet impingement complemented by wing ribs plays a pivotal role in enhancing the cooling efficiency of electronic devices.