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带翅片的冲击射流太阳能空气加热器的实验性能评估。

Experimental performance evaluation of an impinging jet with fins type solar air heater.

机构信息

Department of Mechanical Engineering, RKGIT, Ghaziabad, Uttar Pradesh, 201003, India.

Department of Mechanical Engineering, Indian Institute of Technology (Indian School of Mines), Dhanbad, Jharkhand, 826004, India.

出版信息

Environ Sci Pollut Res Int. 2021 Apr;28(16):19944-19957. doi: 10.1007/s11356-020-12193-x. Epub 2021 Jan 6.

Abstract

The current experimental investigation aimed to evaluate performance of a non-cross flow type solar air heater (SAH). The design comprises of an array of continuous longitudinal fins which extends the bottom of absorber surface and alongside to it a jet plate with inline holes has also been encapsulated. The experiments were performed in natural outdoor conditions for a specified range of flow and geometrical parameters, namely, {[Formula: see text], 5700≤ Re  ≤ 11700, 0.046 ≤ D/D ≤ 0.076, and X/D, w/D = 0.23, 0.46}, respectively. The key indices such as temperature rise parameter (TRP) and collector thermal efficiency are chosen to analyze the performance characteristics of collector. The influence of the above listed parameters on these constraints has been investigated in details. As a function of the entire range of geometrical parameters, an increase in the air flow rate degrades the value of TRP. At the same situation, collector thermal efficiency was found to increase. The peak values of TRP were obtained between 12:00 and 01:00 pm. The rise in air temperature corresponding to hourly deviation of solar intensity has been interpreted at different fin spacing ratios. Furthermore, a parametric optimization approach is employed to identify the optimum values of fin and jet plate parameters yielding maximum collector thermal efficiency. The obtained data have been worked out to plot the design curves for fin and jet parameters. The experimental results were validated with similar literature. The comparative analysis reports a maximum enhancement in TRP of 20.5 % at D/D = 0.076. The percentage improvement in collector thermal efficiency of 16.4% at w/D = 0.23 and 9.8% at D/D = 0.076 has also been noted with reference to compared works.

摘要

当前的实验研究旨在评估一种非交叉流型太阳能空气加热器(SAH)的性能。该设计包括一组连续的纵向翅片,这些翅片延伸到吸收器表面的底部,并且在其旁边还封装了一个带有直线孔的射流板。实验在自然户外条件下进行,针对特定的流动和几何参数范围,即[公式:见文本],5700≤Re≤11700,0.046≤D/D≤0.076,以及 X/D,w/D=0.23,0.46。选择关键指标,如温升参数(TRP)和集热器热效率,来分析集热器的性能特征。详细研究了上述参数对这些约束的影响。作为整个几何参数范围的函数,空气流速的增加会降低 TRP 的值。在相同的情况下,集热器热效率被发现增加。在 12:00 到 01:00 之间可以获得 TRP 的峰值。在不同的翅片间距比下,解释了对应于太阳强度每小时偏差的空气温度升高。此外,采用参数优化方法来确定产生最大集热器热效率的翅片和射流板参数的最优值。将获得的数据绘制成翅片和射流参数的设计曲线。实验结果与类似文献进行了验证。比较分析报告称,在 D/D=0.076 时,TRP 最大增强 20.5%。与比较工作相比,w/D=0.23 时集热器热效率提高 16.4%,D/D=0.076 时提高 9.8%。

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