圆管内不同布置的三角小翼涡发生器强化换热

Islam, A. Nurizki, A. Kareem, A. Baba
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引用次数: 0

摘要

人们开发了各种技术来增强传热。涡发生器(VG)是一种能够改变流动特性并最终提高传热性能的被动技术。三角小翼涡发生器可以产生纵向涡和马蹄形涡,这些涡直到下游才衰减,从而以较低的压降增加换热系数。利用该涡发生器,随着摩擦因数的增加,有望获得更高的努塞尔数。因此,本研究是研究桨距比(PR)和攻角(B)对DW涡发生器提高换热器热工性能的影响。四个三角形小翼连接成一个环。这些环将被用来研究不同参数对传热性能的影响。在本研究中,VGs被放置在一个圆形的铜管内,加热线圈缠绕在铜管的外表面,以产生恒定的热流密度条件。实验装置由鼓风机、孔板流量计、流量矫直器、静/流发展段和试验段组成。结果表明,摩擦系数、努塞尔数和热工性能均有显著提高。由于圆管内纵向涡的形成,提高了热工性能。俯仰比和攻角对流动和传热有显著影响。1.6的俯仰比对(f/f0)和(Nu/Nuo)的影响最大,其次是攻角。烟流可视化技术用于研究烟流的流动特性和流动结构。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Heat Transfer Enhancement With Delta Winglets Vortex Generator for Different Arrangement in a Circular Tube
Various technologies have been developed to enhance the heat transfer. Vortex generator (VG) is one of the passive techniques which can change the flow behavior and ultimately enhances the heat transfer performance. Delta winglet (DW) vortex generator can create longitudinal and horseshoe vortices which do not decay until further downstream and consequently increase heat transfer coefficient with comparatively lower pressure drop. With this vortex generator, it is expected to have higher Nusselt number with some increase of friction factor. Therefore, this study is to study the effect of pitch ratio (PR) and attack angle (B) of DW vortex generator to increase the thermal performance of heat exchanger. Four delta winglets are attached into a ring. Those rings attached with VGs will be used to investigate the influence of different parameters to heat transfer performance. In this study VGs were placed inside a circular copper tube and the heating coil was wrapped up around the outer surface of the copper tube to generate a constant heat flux condition. The experimental setup consists of a blower, orifice meter, flow straightener, calm/flow developing section and test section. The results show the friction factor, Nusselt number, and Thermal Performance Enhancement. It increases the thermal performance due to the formation of longitudinal vortex inside the circular tube. Pitch ratio and attack angle seem to have significant impact on the flow and heat transfer. The Pitch ratio of 1.6 have the highest impact on both (f/f0) and (Nu/Nuo) followed by attack angle. Smoke flow visualization technique was used to study flow behavior and flow structures.
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