Optimization of Hot Runner Structure for Self-excitedPulsating Heat Transfer of Al2O3 Nanofluid
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摘要:
在对流传热过程中,如何增加边界扰动以改善传热性能,是实现强化传热的关键问题。基于自激振荡腔的脉动效应和纳米流体的高热导率,提出了一种纳米流体无源脉动强化传热机制。采用正交数值试验方法对自激振荡热流道的主要结构参数进行优化研究,利用大涡模拟湍流模型分析了热流道的结构参数对Al2O3纳米流体传热特性的影响规律,并获得了最优结构参数配比。结果表明:腔室长度对热流道中纳米流体的传热性能影响最大,腔室直径影响最小,并观察到无量纲参数L/d1=7、D/d1=11、d2/d0=1.1的自激振荡热流道具有最佳传热性能。 Abstract: In the process of convective heat transfer, how to increase the boundary disturbance to improve the heat transfer performance is the key issue to realize the enhancement of heat transfer. Based on the pulsation effect of the self-excited oscillation chamber and the high thermal conductivity of the nanofluid, a passive pulsation enhanced heat transfer mechanism of the nanofluid is proposed in this study. The orthogonal numerical experiment method was used to optimize the main structural parameters of the self-excited oscillation hot runner. The large eddy simulation turbulence model was used to analyze the influence of the hot runner structural parameters on the heat transfer characteristics of the Al2O3 nanofluid, and the optimal structural parameter ratio was obtained. The orthogonal numerical experiment results show that the length of the chamber has the greatest effect on the heat transfer performance of the nanofluid in the hot runner, and the diameter of the chamber has the least effect. It is also observed that the self-excited oscillating hot runner has the best heat transfer performance when dimensionless parameters L/d1=7, D/d1=11 and d2/d0=1.1. -
表 1 自激振荡热流道初始结构参数
结构参数 尺寸 上流道入口直径d0/mm 12 上流道入口长度l0/mm 15 上流道出口直径d1/mm 6 上流道出口长度l1/mm 5 下流道直径d2 d0 下流道长度l2/mm 150 腔室直径D 10d1 腔室长度L 6d1 收敛角α/(º) 14 碰撞角θ/(º) 120 表 2 Al2O3纳米颗粒和水的热物理性质
物性参数 Al2O3 水 ρ/(kg·m−3) 3 880 998.2 Cp/(J·(kg·K)−1) 773 4 182 μnf /(Pa·s) − 9.98×10−4 k/(W·(m·K)−1) 36 0.597 表 3 热流道主要结构参数因素-水平表
因素水平 A B C 1 10 4 0.8 2 11 5 0.9 3 12 6 1.0 4 13 7 1.1 表 4 正交数值试验方案及试验结果表
编号 A B 空列 C 空列 组合 Nuav 1 10 4 0.8 0.8 0.8 A1B1C1 340.8789 2 10 5 0.9 0.9 0.9 A1B2C2 451.6409 3 10 6 1.0 1.0 1.0 A1B3C3 543.8952 4 10 7 1.1 1.1 1.1 A1B4C4 592.7202 5 11 4 1.0 0.9 1.1 A2B1C2 392.9558 6 11 5 1.1 0.8 1.0 A2B2C1 426.2260 7 11 6 0.8 1.1 0.9 A2B3C4 596.9104 8 11 7 0.9 1.0 0.8 A2B4C3 559.9789 9 12 4 1.1 1.0 0.9 A3B1C3 421.1068 10 12 5 1.0 1.1 0.8 A3B2C4 505.6841 11 12 6 0.9 0.8 1.1 A3B3C1 525.4945 12 12 7 0.8 0.9 1.0 A3B4C2 616.7067 13 13 4 0.9 1.1 1.0 A4B1C4 432.8087 14 13 5 0.8 1.0 1.1 A4B2C3 475.6208 15 13 6 1.1 0.9 0.8 A4B3C2 480.7732 16 13 7 1.0 0.8 0.9 A4B4C1 633.8898 k1 482.2838 396.9375 507.5292 481.6223 471.8288 Tin = 293.15 K
Twall = 343.15 K
Rein = 40000k2 494.0178 464.7929 492.4808 485.5191 525.8870 k3 517.2480 536.7684 519.1062 500.1504 504.9091 k4 505.7731 600.8239 480.2066 532.0309 496.6978 R 34.9642 203.8864 38.8997 50.4086 54.0582 表 5 方差分析表
方差来源 平方和 自由度 F 显著性 A 2721.43 3 0.574 Δ B 93514.66 3 19.741 *** C 6293.28 3 1.328 * e 9474.33 6 − − 总和 112003.69 15 − − 注:Δ不显著;*显著;**较显著;***高度显著。 -
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