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Mechanism analysis of the buoyancy effects on heat transfer of supercritical nitrogen in horizontal serpentine tube

机译:水平蛇形管中浮力对超临界氮传热影响的机理分析

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In this paper, the buoyancy effects on heat transfer performance of cryogenic supercritical fluid in the submerged combustion vaporizer (SCV) are studied experimentally and numerically. Supercritical nitrogen is selected to substitute LNG for the safety reason. A three-dimensional model is established to calculate the flow and heat transfer of supercritical nitrogen, and the maximum relative error between the simulation and experiment is 2.78%. Based on the simulation results, a non-uniform circumferential heat transfer coefficient distribution is found in the pseudo-critical region, and the mechanism of the non-uniformity is analyzed. The reason for the phenomenon that the top and bottom generatrices reach the peak value of the heat transfer coefficient at different positions is further revealed by analyzing the average thermo-physical properties in different regions of the boundary layer. The results showed that the secondary flow caused by buoyancy leads to a non-uniform distribution of the thermal boundary layer thickness on the radial section. Under the influence of buoyancy, the temperature of the buffer layer near the top and bottom generatrices reach the large specific heat region successively, leading the peak position of the heat transfer coefficient of them not appear synchronously. Overall, comparing to the no-buoyancy condition, the whole heat transfer coefficient increased, with the heat transfer enhancement at the bottom and side generatrices but deterioration at the top generatrix.
机译:本文通过实验和数值研究了浮力对低温超临界流体在潜水燃烧蒸发器中的传热性能的影响。出于安全原因,选择超临界氮替代LNG。建立了一个三维模型来计算超临界氮的流动和传热,模拟和实验之间的最大相对误差为2.78%。根据仿真结果,在伪临界区发现周向传热系数不均匀,并分析了不均匀的机理。通过分析边界层不同区域的平均热物理性质,进一步揭示了顶部和底部母体在不同位置达到传热系数峰值的现象的原因。结果表明,由浮力引起的二次流动导致热边界层厚度在径向截面上的不均匀分布。在浮力的影响下,上下母线附近的缓冲层温度依次到达较大的比热区,导致它们的传热系数的峰值位置不同步出现。总体而言,与无浮力条件相比,整体传热系数增加,底部和侧面母线的传热增强,而顶部母线的传热恶化。

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