3D numerical investigation of trans-critical heat transfer enhancement in regeneration cooling channel with crescent rib

被引:34
|
作者
Luo, Wen [1 ,2 ]
Han, Huaizhi [1 ,2 ]
Jiang, Rongpei [3 ]
Yu, Ruitian [1 ,2 ]
Zhu, Quan [1 ,2 ]
机构
[1] Sichuan Univ, Sch Chem Engn, Chengdu 610065, Peoples R China
[2] Sichuan Univ, Minist Educ, Engn Res Ctr Combust & Cooling Aerosp Power, Chengdu 610065, Sichuan, Peoples R China
[3] Beijing Inst Aerosp Testing Technol, Beijing 100074, Peoples R China
基金
中国国家自然科学基金;
关键词
Regenerative cooling; Heat transfer deterioration; Heat transfer enhancement; Crescent rib; Numerical simulation; FRICTION FACTOR CORRELATIONS; SUPERCRITICAL CO2; ABSORBER PLATE; TURBULENT-FLOW; DUCT; ROUGHNESS; AUGMENTATION; PERFORMANCE; SIMULATION; METHANE;
D O I
10.1016/j.ijthermalsci.2021.107287
中图分类号
O414.1 [热力学];
学科分类号
摘要
In this study, a numerical simulation of the trans-critical flow and heat transfer performance of n-decane in a regenerative cooling microrib structure channel is conducted. The shear stress transfer k-omega numerical model is used to compare the heat transfer enhancement mechanism between straight and crescent ribs to improve heat transfer deterioration in a smooth channel. Within the specific dimensions and operative conditions of the test case, the results demonstrate that the average temperature in a channel with crescent ribs was 70 K less than one with rectangular ribs, and the average Nusselt number in a channel with crescent ribs was 50 greater than one with rectangular ribs. When compared with the rectangular rib channel, the thermal performance in the crescent rib channel increased by 59.1%-66.4%, and the overall heat transfer performance increased by 18.3%-25.9%. Saw-tooth distribution was observed along the rib channel, breaking the thermal boundary layer and avoiding heat transfer deterioration. Two spanwise vortices produced by the crescent ribs enhanced the flow mixing and turbulence kinetic energy transport near the sidewall region, which is a significant reason for the superior thermal performance of the crescent rib channel.
引用
收藏
页数:11
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