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Optimization research of sextant fan baffle curvature radius in shell and tube heat exchanger

机译:壳管热交换器中六峰扇挡板曲率半径的优化研究

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For a high shell side pressure drop of the conventional segmental baffles in shell and tube heat exchanger, a novel sextant fan baffle was put forward. To research the influence of baffle curvature radius of the sextant fan baffled shell and tube heat exchanger (SFTHX) on the shell side pressure drop, the heat transfer coefficient and the comprehensive heat transfer performance, six different curvature radius baffles were numerically simulated and experimental studied in this paper. Based on the numerically simulation results, under the same inlet flow conditions, a better comprehensive heat transfer performance can be found in SFTHX with the baffle curvature radius of 1 D, which is higher by 0.84-6.85% more than that of the others. Moreover, the experimental investigation data of SFTHX with baffle curvature radius of 1 D indicates that the numerically simulation can well predict the flow and heat transfer characteristics with the experiment.
机译:对于壳和管热交换器中传统节段挡板的高壳侧压降,提出了一种新的塞克兰扇挡板。 为了研究摇晃扇形壳体壳和管热交换器(SFTHX)对壳侧压降的影响,传热系数和综合传热性能,六种不同的曲率半径挡板在数模上模拟和实验研究 在本文中。 基于数值模拟结果,在相同的入口流动条件下,可以在SFTHX中找到更好的综合传热性能,其中挡板曲率半径为1 d,比其他的挡板曲率半径为0.84-6.85%。 此外,具有挡板曲率半径为1d的SFTHX的实验研究数据表明,数值模拟可以通过实验预测流量和传热特性。

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