向风弯曲格架结构传热特性的综合研究

IF 5.4 2区 工程技术 Q1 ENGINEERING, AEROSPACE
Xiaohui Bai , Cunliang Liu , Changxian Zhang , Xianlong Meng , Jinbo Li , Xianlong Zhang
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引用次数: 1

摘要

向风弯曲晶格框架结构具有高传热系数和低摩擦系数的特点。WB结构可用于热保护系统,保护加力燃烧室和喷嘴的外壁不受热气热负荷的损坏;用于动力电池模块的风冷系统,散热其充放电过程中产生的热量。本文对迎风弯曲格架结构的传热特性进行了较为全面的研究。通过系统的三维数值模拟研究了WB结构参数(流向和横向节距、迎风弯曲韧带直径和倾角)对其流动阻力和换热增强的影响,并通过比较相同泵送功率下的努塞尔数来评价其增强效果。此外,还充分讨论了一个重要参数,即间隙换热率与端壁换热率之比(RQ)对总换热率的贡献。结果表明,在Nusselt数的取值范围内,纵向为6个单位,横向为2.5个单位,即(nx = 6, nz = 2.5)的情况表现出最好的性能。RQ比值在4.5 ~ 5.0范围内的结构传热性能较好。最后,给出了泵浦功率分别为2500和3000时,用单位数(nx, nz)协调的努塞尔数最优范围的两个彩色轮廓图。图中正确反映了不同nx和nz下结构的Nusselt数的变化,结论与4.2流向和展向单元数的影响、4.3间隙换热率与端壁换热率之比的讨论一致,指导了嵌入WB结构的热防护系统结构参数的合理选择。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
A comprehensive study on the heat transfer characteristics of windward bend lattice frame structure

The windward bend lattice frame structure (WB structure) is characterized by a high heat transfer coefficient and low friction factor. The WB structure can be applied for thermal protection system, protecting outer walls of afterburner and nozzles from being damaged by the heating load of hot gas, for air cooling system of the power battery module, dissipating the heat generated during its charging and discharging. In this paper, the heat transfer characteristics of the windward bend lattice frame structure have been comprehensively studied. A systematic 3D numerical simulation has been conducted to investigate the effects of the structural parameters of the WB structure, including the pitches in both flow direction and transverse direction, the diameter and the inclination angle of windward bend ligament, on its flow resistance and heat transfer enhancement, which has been evaluated by comparing its Nusselt number under an equal pumping power. Furthermore, the contribution of an important parameter, i.e., the ratio of the interstitial heat transfer rate to the end-wall heat transfer rate (RQ), to the overall heat transfer rate has been fully discussed. As a result, the case of 6 units in the longitudinal direction and 2.5 units in the transverse direction, i.e. (nx = 6, nz = 2.5) exhibits the best performance in the light of the value of the Nusselt number. Moreover, the structure with a ratio of RQ ranges in 4.5–5.0 achieves a better heat transfer performance. Finally, two color contour graphs showing an optimal range of Nusselt number coordinated by unit numbers (nx, nz) for pumping powers of 2500 and 3000 have been presented. The graphs correctly reflect the variation of Nusselt numbers of structures with different nx and nz, and the conclusions remain consistent with the discussion in sections 4.2 Effects of the number of units in the streamwise and spanwise directions, 4.3 Ratio of interstitial heat transfer rate to end-wall heat transfer rate, instructing the reasonable selection of structural parameters of a thermal protection system embedded with WB structure.

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来源期刊
CiteScore
7.50
自引率
5.70%
发文量
30
期刊介绍: Propulsion and Power Research is a peer reviewed scientific journal in English established in 2012. The Journals publishes high quality original research articles and general reviews in fundamental research aspects of aeronautics/astronautics propulsion and power engineering, including, but not limited to, system, fluid mechanics, heat transfer, combustion, vibration and acoustics, solid mechanics and dynamics, control and so on. The journal serves as a platform for academic exchange by experts, scholars and researchers in these fields.
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