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Heat transfer enhancement of fin-tube heat exchangers using punched triangular ramp vortex generator on the fin surface

机译:在翅片表面上使用冲孔三角斜坡涡流发生器的翅片管热交换器的传热增强

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Existence of the vortices in a flow field strongly affects the heat transfer. In this study, effect of newly proposed punched triangular ramp vortex generator (PRVG) on heat transfer performance for a fin-tube heat exchanger was investigated numerically. Normalized ramp height (H/d=0.196 and 0.161) and ramp angle (α_r=20° and 35°) were examined as the geometric parameter. Numerical computations were carried out under turbulent flow conditions (5000≤Re≤20000). RANS equations were solved using ANSYS Fluent by using SST k-ω) turbulence model. Nusselt (Nu) number, friction factor and Performance Evaluation Criterion (PEC) were comprehensively examined quantitatively. Flow characteristics were also investigated for elucidating the underlying physics of enhancement heat transfer by the PRVG winglet. Results were compared with the flat smooth fin surface (baseline case). Results showed that overall heat transfer on the entire channel wall increases up to 43.66% for Re=5000 by H/d=0.196 and α_r=35°. The influence of ramp angle on thermo-hydraulic performance was more significant compared to ramp height. Furthermore, PEC results showed that the most feasible geometric design of PRVG winglet for the fin-tube heat exchanger is H/d=0.161 and α_r=20°. Furthermore, decreasing flow speed in the channel increases the effectiveness of the vortex generator according to PEC results.
机译:流场中的涡流的存在强烈影响传热。在该研究中,在数值上研究了新提出的冲孔三角形斜坡涡流发生器(PRVG)对翅片管热交换器的传热性能的影响。将归一化斜坡高度(H / D = 0.196和0.161)和斜坡角度(α_R= 20°和35°)作为几何参数进行检查。在湍流条件下进行数值计算(5000≤R≤20000)。使用SST k-ω)湍流模型使用SST k-ω的ansys来解决了Rans方程。全面地定量检查Nusselt(Nu)数,摩擦因子和性能评估标准(PEC)。还研究了流动特性,以阐明PRVG幼锭的增强热传递的潜在物理学。将结果与扁平光滑的翅片表面(基线情况)进行比较。结果表明,通过H / d = 0.196和α_R= 35°,整个通道壁上的总热传递高达43.66%的RE = 5000增加到43.66%。与斜坡高度相比,斜坡角度对热水性能的影响更为显着。此外,PEC结果表明,用于翅片管热交换器的PRVG小翼的最可行的几何设计是H / D = 0.161和α_R= 20°。此外,减小通道中的流速增加了根据PEC结果的涡流发生器的有效性。

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