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Numerical study on flow and heat transfer of a finned-tube heat exchanger with trapezoid vortex generators in CO_2 lasers

机译:CO_2激光器梯形涡流发生器翅片管热交换器流动和传热的数值研究

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The high pressure loss and low heat transfer efficiency have been plaguing the development of high power fast-axial-flow CO_2 laser. In order to solve this problem, a special longitudinal vortex generator (LVG), which contains two modified right-angled trapezoid wings and interrupt gap(TMRTW), was proposed. The performance of a single trapezoid winglet(STW) and TMRTW was discussed. Numerical study reveals that compared with STW, the TMRTW has better flow and heat transfer characteristics under the same initialization conditions. Further parametric study indicates that the TMRTW generates vortex. The intensity of this vortex is mainly present in central area. The downstream extension of this vortex is better than that of STW. Especially for the developing of boundary layers, this is beneficial. Hence, the performance of heat transfer for TMRTW is enhanced obviously with Re less than 1200. Compared with STW, the heat transfer for TMRTW is enhanced by 16% under the optimized structure size, with the pressure penalty almost the same.
机译:高压损失和低传热效率一直困扰着高功率快速轴流CO_2激光器的开发。为了解决这个问题,提出了一种特殊的纵向涡流发生器(LVG),其包含两个改进的右倾梯翅膀和中断间隙(TMRTW)。讨论了单个梯形小翼(STW)和TMRTW的​​性能。数值研究表明,与STW相比,TMRTW在相同的初始化条件下具有更好的流动和传热特性。进一步的参数研究表明TMRTW产生涡流。该涡旋的强度主要存在于中心地区。该涡流的下游延伸优于STW。特别是对于边界层的发展,这是有益的。因此,TMRTW的​​传热性能明显增强,随着STW,TMRTW的​​热传递在优化的结构尺寸下增强了16%,压力损失几乎相同。

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