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首页> 外文期刊>Journal of thermal analysis and calorimetry >Second law analysis for nanofluid flow in mini-channel heat sink with finned surface: a study on fin geometries
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Second law analysis for nanofluid flow in mini-channel heat sink with finned surface: a study on fin geometries

机译:粉末表面迷你通道散热器中纳米流体流动的第二法律分析:翅片几何形状研究

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In this numerical work, a second law analysis is carried out for the nanofluid flow and heat transfer in the mini-channel with finned surface. The mini-fins with various geometries, including trapezoidal, square, triangular, and sinusoidal, are located on the bottom surface of the mini-channel. The effects of mini-fins geometry, mini-fins number, Reynolds number, and solid volume fraction of nanoparticles on the temperature and velocity distributions, frictional and thermal irreversibilities, and Bejan number inside the mini-channel are studied. The numerical method is validated with the experimental data. The results show that the sinusoidal, triangular, square, and trapezoidal mini-fins generate up to 66.23%, 61.87%, 59.21%, and 57.80%, respectively, lower thermal irreversibility as compared with the smooth mini-channel. Among mini-fin geometries, the triangular mini-fins generate the maximum frictional irreversibility, while the trapezoidal mini-fins provide the minimum frictional irreversibility. The frictional irreversibility increases about 108.56%, while the thermal irreversibility decreases up to 46.33% as the mini-fin number increases from one to nine. The thermal irreversibility diminishes about 49% by boosting the Reynolds number from 100 to 500. Usage of nanofluid increases both frictional and thermal irreversibilities. Finally, the thermal irreversibility is a dominant term in the total irreversibility and the effects of frictional irreversibility can be ignored.
机译:在该数值工作,第二法分析用于与翅片表面的微通道的纳米流体流动和传热进行。微型翼片与各种几何形状,包括梯形,正方形,三角形,和正弦波,分别位于所述微通道的底表面上。微型翼片的几何形状,微型翼片数,雷诺数,并在温度和速度分布,摩擦和热不可逆性,并且比赞数的微通道内的纳米颗粒的固相体积分数的影响进行了研究。数值方法验证与实验数据。结果表明,正弦,三角形,正方形,梯形和微型翼片分别产生高达66.23%,61.87%,59.21%,57.80和%,降低热不可逆性作为与光滑微通道进行比较。其中微型翼片的几何形状,所述三角形迷你翅片产生的最大摩擦力不可逆性,而梯形迷你翅片提供最小的摩擦不可逆性。约108.56%的摩擦不可逆性增加,而热不可逆性减小到46.33%作为微型翅片数目增加1到9。约49%的热不可逆性减少由升压雷诺数为100〜纳米流体500使用率增加两摩擦和热不可逆性。最后,热不可逆性是总不可逆性一个主项和摩擦不可逆转的影响可以忽略不计。

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