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Effect of fin-enhanced microchannel structures on flow and heat transfer: comparison of triangular ribbed and corrugated designs 翅片增强微通道结构对流动和传热的影响:三角肋和波纹设计的比较
IF 2.6 3区 工程技术 Q2 ENGINEERING, MECHANICAL Pub Date : 2026-03-01 Epub Date: 2025-12-19 DOI: 10.1016/j.ijheatfluidflow.2025.110213
Juhui Chen , Shuxiang Pang , Dan Li , Liwei Chen , Michael Zhurakov , Siarhei Lapatsin , Wenrui Jiang
Conventional microchannels typically exhibit limited heat transfer efficiency and suboptimal flow characteristics. This study investigates two fin-enhanced microchannel geometries, triangular ribbed and corrugated, using a moving-grid method to simulate periodic fin motion. Numerical simulations were conducted over a Reynolds number range of 50–250 at a fin oscillation frequency of 20 Hz. The results show that the triangular ribbed microchannel offers lower flow resistance and improved overall flowability due to its relatively smoother flow path, whereas the corrugated design produces stronger flow disturbances and secondary vortices, leading to enhanced heat transfer, especially at lower Reynolds numbers. However, the intensified flow mixing in the corrugated microchannel also increases flow-path tortuosity, resulting in a larger pressure drop. To evaluate the overall performance, the Performance Evaluation Criterion (PEC) was used. The triangular ribbed channel achieved a maximum PEC of 1.52 at Re = 200, indicating a balanced improvement in both heat transfer and flow resistance. These geometries are relevant for practical thermal management applications, such as compact heat sinks and miniaturized cooling devices, due to their manufacturability and effectiveness in enhancing thermo-fluidic performance.
传统的微通道通常表现出有限的传热效率和次优的流动特性。本研究研究了两种鳍增强微通道几何形状,三角形肋形和波纹形,使用移动网格方法模拟周期性鳍运动。在50 ~ 250雷诺数范围内,在20 Hz的翅片振荡频率下进行了数值模拟。结果表明,三角形肋形微通道由于其相对平滑的流动路径,具有更低的流动阻力和更高的整体流动性,而波纹设计产生更强的流动扰动和二次涡,导致传热增强,特别是在低雷诺数时。然而,波纹微通道内流动混合的加剧也增加了流道扭曲度,导致更大的压降。采用性能评价标准(PEC)对整体性能进行评价。在Re = 200时,三角形肋形通道的最大PEC达到1.52,表明传热和流动阻力的平衡改善。由于其可制造性和提高热流体性能的有效性,这些几何形状与实际热管理应用相关,例如紧凑型散热器和小型化冷却装置。
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引用次数: 0
Parametric investigation of a solid-porous fin design for microchannel thermal performance improvement 改善微通道热性能的固体多孔翅片设计参数化研究
IF 2.6 3区 工程技术 Q2 ENGINEERING, MECHANICAL Pub Date : 2026-03-01 Epub Date: 2025-12-17 DOI: 10.1016/j.ijheatfluidflow.2025.110210
Hanieh Asgharpouri Moghadam , Farid Dolati , Fatemeh Bagherighajari , Morteza Momeni Taromsari
Cooling and thermal management in micro-scale systems are critically important in various applications, as they minimize equipment size and extend its lifespan. Although conventional solid-fin heat sinks have boosted the efficiency of cooling systems, they face a fundamental trade-off between heat dissipation efficiency, energy consumption, and the mechanical power required for pumping. To overcome this, porous fins are applicable; however, their performance is often limited by low effective thermal conductivity and a lack of geometric design refinement. Therefore, this study introduces a novel hybrid porous-solid fin design that strategically combines the high conductivity of solid fins with the superior surface area and flow mixing of porous materials. This numerical investigation analyzes the thermal–hydraulic performance of the hybrid microchannel, focusing on the effects of porous layer thickness (tp), height (hp), Reynolds number (Re), and porosity (ε). Simulations identify that a porous thickness of tp = 0.3 mm yields the best performance, which reduces pressure drop by 21.96 % while simultaneously enhancing heat transfer by 31.21 %, culminating in a 42.51 % improvement in the Performance Evaluation Factor (PEF) compared to conventional solid fins. The analysis further reveals that increasing Re decreases thermal resistance at the expense of a higher pressure drop, while lower porosity enhances heat transfer at the cost of increased flow resistance. Crucially, the favorable porous height for PEF decreases with higher Re, emphasizing the necessity for a flow-condition-specific design to maximize the benefits of this hybrid approach.
微尺度系统的冷却和热管理在各种应用中至关重要,因为它们可以最小化设备尺寸并延长其使用寿命。尽管传统的固体翅片散热器提高了冷却系统的效率,但它们面临着散热效率、能量消耗和泵送所需的机械功率之间的基本权衡。为了克服这个问题,多孔翅片是适用的;然而,它们的性能往往受到低有效导热率和缺乏几何设计精细的限制。因此,本研究引入了一种新型的多孔-固体混合翅片设计,将固体翅片的高导电性与多孔材料的优越表面积和流动混合巧妙地结合在一起。该数值研究分析了混合微通道的热工性能,重点研究了多孔层厚度(tp)、高度(hp)、雷诺数(Re)和孔隙度(ε)对混合微通道热工性能的影响。仿真结果表明,多孔厚度tp = 0.3 mm可获得最佳性能,与传统的固体翅片相比,可将压降降低21.96%,同时传热能力提高31.21%,最终性能评估因子(PEF)提高42.51%。进一步分析表明,增加Re会以增加压降为代价降低热阻,而降低孔隙率会以增加流动阻力为代价增强传热。至关重要的是,PEF的有利孔隙高度随着Re的升高而降低,这强调了针对流动条件进行特定设计的必要性,以最大限度地提高这种混合方法的效益。
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引用次数: 0
Synergistic enhancement of heat transfer in tubular heat exchangers using twisted tape inserts and nanofluids: An integrated numerical and experimental review 使用扭曲带插入和纳米流体的管式换热器中传热的协同增强:综合数值和实验回顾
IF 2.6 3区 工程技术 Q2 ENGINEERING, MECHANICAL Pub Date : 2026-03-01 Epub Date: 2025-12-17 DOI: 10.1016/j.ijheatfluidflow.2025.110180
Deepak Kumar Rathaur, R.M. Sarviya, S.P.S. Rajput
The rising global demand for compact, energy-efficient heat exchangers has driven interest in passive heat transfer enhancement techniques. Among these, the combination of twisted tape inserts with nanofluids is particularly promising, as twisted tapes generate swirl flows that enhance heat transfer, while nanofluids improve thermal conductivity without requiring extra energy. This review systematically synthesizes experimental and numerical studies on single, hybrid, and tri-hybrid nanofluids combined with classical and modified twisted tape inserts, including perforated, wavy, jagged, wing-cut, V-cut, W-cut, and compound designs. Performance is evaluated in terms of Nusselt number, friction factor, and thermal performance factor. Classical twisted tape inserts with single nanofluid enhance heat transfer by 15–40 %, whereas advanced geometries with hybrid nanofluids achieve 50–95 % gains. The maximum reported Nusselt number enhancement is approximately 72% for hybrid nanofluids with modified twisted tape inserts at higher Reynolds numbers, accompanied by a 20–60 % increase in friction factor. Thermal performance factors generally exceed unity, peaking at around 2.5 for a helical coil–twisted tape insert configuration with graphene/water nanofluid. Comparisons indicate that plain twisted tape inserts with Al2O3/water nanofluid improve heat transfer by about 40%, while perforated twisted tape inserts with Al2O3-Cu/water hybrid nanofluids achieve approximately 85%. Overall, geometry modification combined with advanced nanofluids can nearly double heat exchanger performance, although challenges related to pumping power, nanofluid stability, and techno-economic feasibility remain key areas for future research.
全球对紧凑型、高能效热交换器的需求不断增长,推动了人们对被动传热增强技术的兴趣。其中,扭曲带与纳米流体的结合尤其有前景,因为扭曲带产生漩涡流动,加强传热,而纳米流体在不需要额外能量的情况下提高导热性。本文系统地综合了单一、混合和三混合纳米流体与经典和改进的扭曲带插入物结合的实验和数值研究,包括穿孔、波浪、锯齿、翼形切割、v形切割、w形切割和复合设计。性能是根据努塞尔数、摩擦系数和热性能系数来评估的。传统的扭曲带插入与单一纳米流体提高传热15 - 40%,而先进的几何形状与混合纳米流体实现50 - 95%的增益。据报道,在较高雷诺数下,混合纳米流体的最大努塞尔数增强约为72%,同时摩擦系数增加20 - 60%。热性能系数通常超过1,对于带有石墨烯/水纳米流体的螺旋线圈扭曲带插入配置,热性能系数在2.5左右达到峰值。对比表明,普通的扭曲带插入Al2O3/水纳米流体可以提高约40%的换热率,而穿孔扭曲带插入Al2O3- cu /水混合纳米流体可以提高约85%的换热率。总体而言,尽管泵送功率、纳米流体稳定性和技术经济可行性仍是未来研究的关键领域,但与先进纳米流体相结合的几何形状改变可以使热交换器的性能几乎翻倍。
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引用次数: 0
Insight into effect of internal heating on natural convection of Rivlin–Ericksen fluid with highly permeable porous medium: Dynamical system approach 内部加热对高渗透多孔介质Rivlin-Ericksen流体自然对流影响的研究:动力系统方法
IF 2.6 3区 工程技术 Q2 ENGINEERING, MECHANICAL Pub Date : 2026-03-01 Epub Date: 2025-12-22 DOI: 10.1016/j.ijheatfluidflow.2025.110212
Anupama Singh , Anand Kumar , Vinod K. Gupta
The current article explores the structure of chaotic convection and the rate of heat transfer in a Rivlin–Ericksen fluid layer with an internal heat source flowing through a highly permeable porous medium that is heated from below. The truncated Galerkin approximation has produced a low-dimensional system similar to the Lorenz model. To compute the numerical simulation for a Lorenz-like equation framework, we implemented the fourth-order Runge–Kutta method. We utilized MATHEMATICA software for quantitative analysis and MATLAB software for visualization. The influence of an internal heat content on chaotic convection has been investigated. Additionally, when comparing only the elasticity effect, we found that the Rayleigh number decreases by 8.09%. This indicates that the chaotic behavior predominates over the instability of the system. We discovered that both the level of internal heat and the elastic parameter enhance chaotic convection. We propose that the level of internal heat influences the transition from steady to chaotic convection.
本文探讨了具有内部热源的Rivlin-Ericksen流体层中混沌对流的结构和传热速率,该流体层流经从下方加热的高渗透性多孔介质。截断的伽辽金近似产生了一个类似于洛伦兹模型的低维系统。为了计算类洛伦兹方程框架的数值模拟,我们实现了四阶龙格-库塔方法。采用MATHEMATICA软件进行定量分析,MATLAB软件进行可视化分析。研究了内部热含量对混沌对流的影响。此外,当仅比较弹性效应时,我们发现瑞利数降低了8.09%。这表明混沌行为在系统的不稳定性中占主导地位。我们发现内热水平和弹性参数都增强了混沌对流。我们提出内部热的水平影响从稳定对流到混沌对流的转变。
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引用次数: 0
Optimization of the cooling performance of ribbed channels by combining neural networks and genetic algorithms 结合神经网络和遗传算法优化肋形通道的冷却性能
IF 2.6 3区 工程技术 Q2 ENGINEERING, MECHANICAL Pub Date : 2026-03-01 Epub Date: 2025-12-24 DOI: 10.1016/j.ijheatfluidflow.2025.110224
Shao-Fei Zheng , Jia-Xing Meng , Hua-Dong Shi , Yi-Feng Wang , Shu-Rong Gao , Yan-Ru Yang , Bo Gao , Xiao-Dong Wang
In gas turbine engines, efficient heat transfer following less friction loss is extremely preferable for the cooling of turbine blades, because of the limited supply of the cooling air. To maximize the cooling effect of the commonly utilized ribbed channel, the back propagation neural network (BPNN) model and the genetic algorithm (GA) are combined to construct an optimization tool by exactly modeling the complex nonlinear relationship between the influencing factors and cooling performance. The coupling influences of the channel aspect ratio (W/H = 0.5 ∼ 4.0), the pitch ratio of ribs (P/e = 20 ∼ 5), and the Reynolds number (Re = 20, 000 ∼ 100, 000) are comprehensively analyzed using the Nusselt number and overall performance factor as the target function. The results state that using the Nusselt number as the target function, the relatively large aspect ratio and small pitch ratio are recommended due to the heat transfer enhancement of the flow impingement effect with the rib-induced flow separation. Considering both the heat transfer enhancement and the increased friction loss, the overall performance factor presents a highly nonlinear relationship with those influencing parameters, and the relatively small aspect ratio and large pitch ratio are suggested to improve the comprehensive cooling performance. Using the GA-BPNN optimization method, a great increase of 16.98 %∼30.67 % is achieved for the overall performance factor in the current operating conditions. Finally, the GA-BPNN method is demonstrated as powerful and efficient for improving the ribbed cooling channel.
在燃气涡轮发动机中,由于冷却空气的供应有限,在摩擦损失较小的情况下,高效的传热对于涡轮叶片的冷却是极其可取的。为了使常用的肋形通道冷却效果最大化,将反向传播神经网络(BPNN)模型与遗传算法(GA)相结合,通过精确建模影响因素与冷却性能之间复杂的非线性关系,构建了优化工具。耦合通道宽高比的影响(0.5 W / H =  ∼ 4.0),肋骨的螺距比(P / e = 20 ∼ 5),和雷诺数(Re = 000 ∼ 100年,000年)进行了全面分析使用努塞尔特数和整体性能因素作为目标函数。结果表明,以Nusselt数为目标函数,由于肋诱导流动分离强化了流动冲击效应的传热,建议采用较大的展弦比和较小的节距比。考虑到传热增强和摩擦损失的增加,综合性能因子与这些影响参数呈高度非线性关系,建议采用较小的展弦比和较大的节距比来提高综合冷却性能。使用GA-BPNN优化方法,在当前运行条件下,总体性能因子实现了16.98 % ~ 30.67 %的大幅提高。最后,验证了GA-BPNN方法对肋形冷却通道的改进效果。
{"title":"Optimization of the cooling performance of ribbed channels by combining neural networks and genetic algorithms","authors":"Shao-Fei Zheng ,&nbsp;Jia-Xing Meng ,&nbsp;Hua-Dong Shi ,&nbsp;Yi-Feng Wang ,&nbsp;Shu-Rong Gao ,&nbsp;Yan-Ru Yang ,&nbsp;Bo Gao ,&nbsp;Xiao-Dong Wang","doi":"10.1016/j.ijheatfluidflow.2025.110224","DOIUrl":"10.1016/j.ijheatfluidflow.2025.110224","url":null,"abstract":"<div><div>In gas turbine engines, efficient heat transfer following less friction loss is extremely preferable for the cooling of turbine blades, because of the limited supply of the cooling air. To maximize the cooling effect of the commonly utilized ribbed channel, the back propagation neural network (BPNN) model and the genetic algorithm (GA) are combined to construct an optimization tool by exactly modeling the complex nonlinear relationship between the influencing factors and cooling performance. The coupling influences of the channel aspect ratio (<em>W</em>/<em>H</em> = 0.5 ∼ 4.0), the pitch ratio of ribs (<em>P</em>/<em>e</em> = 20 ∼ 5), and the Reynolds number (<em>Re</em> = 20, 000 ∼ 100, 000) are comprehensively analyzed using the Nusselt number and overall performance factor as the target function. The results state that using the Nusselt number as the target function, the relatively large aspect ratio and small pitch ratio are recommended due to the heat transfer enhancement of the flow impingement effect with the rib-induced flow separation. Considering both the heat transfer enhancement and the increased friction loss, the overall performance factor presents a highly nonlinear relationship with those influencing parameters, and the relatively small aspect ratio and large pitch ratio are suggested to improve the comprehensive cooling performance. Using the GA-BPNN optimization method, a great increase of 16.98 %∼30.67 % is achieved for the overall performance factor in the current operating conditions. Finally, the GA-BPNN method is demonstrated as powerful and efficient for improving the ribbed cooling channel.</div></div>","PeriodicalId":335,"journal":{"name":"International Journal of Heat and Fluid Flow","volume":"118 ","pages":"Article 110224"},"PeriodicalIF":2.6,"publicationDate":"2026-03-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"145836939","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":3,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
Enhanced cooling performance in turbine blade tip U-channel using protrusion-V-rib composite structure 采用凸型- v型肋复合结构增强涡轮叶片u型通道冷却性能
IF 2.6 3区 工程技术 Q2 ENGINEERING, MECHANICAL Pub Date : 2026-03-01 Epub Date: 2025-12-20 DOI: 10.1016/j.ijheatfluidflow.2025.110218
Zhen Xiang , Qilong Liu , Shaohua Han , Shizhen Qi , Tianyi Huo , Runsheng Zhang , Leping Zhou , Li Li , Hui Zhang , Xiaoze Du
Improving the cooling effectiveness of turbine blade squealer tip regions under high thermal loads remains a challenge in designing of gas turbines. This study numerically investigates the cooling performance of a novel protrusion-V-rib composite structure applied to the internal U-channel near the blade squealer tip. Eight configurations, including holed/hole free designs and combinations of V-ribs, protrusions and vanes, are evaluated at Re = 10,000–50,000. Key findings show that holed structures enhance heat transfer near holes due to accelerated fluid velocity and increased turbulence, resulting in higher Nusselt number. However, hole free configurations exhibit superior downstream heat transfer (up to 4.14 % improvement) by maintaining coolant mass flow. Complex geometries, particularly the V-Convex design, significantly suppress flow separation and reduce vortex size by promoting fluid disturbance and turbulence. The V-convex structure exhibits the highest Nusselt number and comprehensive thermal performance factor under both constant temperature and constant heat flux boundary conditions, confirming its robustness. The results highlight the trade-off between local heat transfer enhancement (holed structures) and downstream cooling effectiveness (hole-free designs), emphasizing the importance of geometric optimization for blade squealer tip cooling. This work helps understand the composite cooling structures and provides insights for efficient thermal management in applications of high-temperature turbines.
在高热负荷条件下,如何提高涡轮叶片尖尖区域的冷却效率一直是燃气轮机设计中的难题。本文对一种新型的凸型- v型肋复合结构应用于靠近叶片尖部的u型通道内的冷却性能进行了数值研究。在Re = 10,000-50,000的条件下,对8种结构进行了评估,包括有孔/无孔设计以及v型肋、凸点和叶片的组合。关键发现表明,由于流体速度加快和湍流增加,孔结构增强了孔附近的传热,从而导致更高的努塞尔数。然而,通过保持冷却剂质量流量,无孔结构表现出优越的下游传热(提高4.14%)。复杂的几何形状,特别是v -凸设计,通过促进流体扰动和湍流,显著抑制了流动分离,减小了旋涡尺寸。在恒温和恒热流边界条件下,v -凸结构的Nusselt数和综合热性能因子均最高,证实了其鲁棒性。结果强调了局部传热增强(孔结构)和下游冷却效率(无孔设计)之间的权衡,强调了几何优化对叶片尖叫器尖端冷却的重要性。这项工作有助于了解复合冷却结构,并为高温涡轮机应用中的有效热管理提供见解。
{"title":"Enhanced cooling performance in turbine blade tip U-channel using protrusion-V-rib composite structure","authors":"Zhen Xiang ,&nbsp;Qilong Liu ,&nbsp;Shaohua Han ,&nbsp;Shizhen Qi ,&nbsp;Tianyi Huo ,&nbsp;Runsheng Zhang ,&nbsp;Leping Zhou ,&nbsp;Li Li ,&nbsp;Hui Zhang ,&nbsp;Xiaoze Du","doi":"10.1016/j.ijheatfluidflow.2025.110218","DOIUrl":"10.1016/j.ijheatfluidflow.2025.110218","url":null,"abstract":"<div><div>Improving the cooling effectiveness of turbine blade squealer tip regions under high thermal loads remains a challenge in designing of gas turbines. This study numerically investigates the cooling performance of a novel protrusion-V-rib composite structure applied to the internal U-channel near the blade squealer tip. Eight configurations, including holed/hole free designs and combinations of V-ribs, protrusions and vanes, are evaluated at Re = 10,000–50,000. Key findings show that holed structures enhance heat transfer near holes due to accelerated fluid velocity and increased turbulence, resulting in higher Nusselt number. However, hole free configurations exhibit superior downstream heat transfer (up to 4.14 % improvement) by maintaining coolant mass flow. Complex geometries, particularly the V-Convex design, significantly suppress flow separation and reduce vortex size by promoting fluid disturbance and turbulence. The V-convex structure exhibits the highest Nusselt number and comprehensive thermal performance factor under both constant temperature and constant heat flux boundary conditions, confirming its robustness. The results highlight the trade-off between local heat transfer enhancement (holed structures) and downstream cooling effectiveness (hole-free designs), emphasizing the importance of geometric optimization for blade squealer tip cooling. This work helps understand the composite cooling structures and provides insights for efficient thermal management in applications of high-temperature turbines.</div></div>","PeriodicalId":335,"journal":{"name":"International Journal of Heat and Fluid Flow","volume":"118 ","pages":"Article 110218"},"PeriodicalIF":2.6,"publicationDate":"2026-03-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"145836941","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":3,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
Numerical analysis of rib shape effects on entransy and field synergy in a ribbed sinusoidal wavy microchannel 肋形对肋形正弦波微通道中能量和场协同效应影响的数值分析
IF 2.6 3区 工程技术 Q2 ENGINEERING, MECHANICAL Pub Date : 2026-03-01 Epub Date: 2025-12-30 DOI: 10.1016/j.ijheatfluidflow.2025.110222
Qifeng Zhu, He Zhao, Jingwei Zeng, Sen Zhang, Wenqiang He, Haoxin Deng, Zezhong Wang
Previous research has demonstrated that symmetric sinusoidal wavy (SSW) microchannel heat sinks with rectangular ribs enhance heat transfer compared to ribless SSW channels. To further clarify the role of rib geometry, we conduct numerical simulations to analyze the effects of rib cross-sectional shape on flow and heat transfer characteristics in SSW channels using entransy dissipation and field synergy theory. The channels are equipped with internal ribs of six cross-sectional shapes (airfoil, backward triangle, diamond, ellipse, forward triangle and rectangle). The results show that the addition of ribs significantly improved the heat transfer, with the rectangular rib configuration (SSW-RR) achieving the highest overall performance factor of 1.227 at Re = 600. Ribs reduce entransy dissipation in channel troughs while generating high dissipation near flow detachment points, and this effect intensifies at higher Reynolds numbers. SSW-RR exhibits the lowest entransy dissipation values (1.20 × 1010 to 6.76 × 109), indicating optimal heat transfer performance. Flow field analysis reveals that reverse vortices and large-angle fluid deflection enhance heat transfer, with the forward triangular rib configuration (SSW-FTR) showing the best field synergy (83.58 at Re = 300).
先前的研究表明,与无肋的对称正弦波(SSW)微通道散热器相比,矩形肋的对称正弦波(SSW)微通道散热器的传热效果更好。为了进一步阐明肋形几何的作用,我们利用能量耗散和场协同理论进行数值模拟,分析肋形截面形状对SSW通道内流动和换热特性的影响。通道配备六种截面形状的内肋(翼型,后三角形,菱形,椭圆形,前三角形和矩形)。结果表明,肋板的加入显著改善了换热性能,其中矩形肋板构型(SSW-RR)在Re = 600时获得了最高的综合性能因子1.227。肋板减少了通道槽内的能量耗散,同时在流动分离点附近产生了高耗散,这种效应在高雷诺数时增强。SSW-RR具有最低的能量耗散值(1.20 × 1010 ~ 6.76 × 109),传热性能最佳。流场分析表明,反向涡和大角度流体偏转增强了换热,其中前三角肋结构(SSW-FTR)的场协同效果最好(Re = 300时为83.58)。
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引用次数: 0
Taguchi analysis on convective heat transfer of a Prandtl-Eyring hybrid nanofluid over a Riga plate: Entropy optimization Prandtl-Eyring混合纳米流体在Riga板上对流换热的田口分析:熵优化
IF 2.6 3区 工程技术 Q2 ENGINEERING, MECHANICAL Pub Date : 2026-03-01 Epub Date: 2025-12-15 DOI: 10.1016/j.ijheatfluidflow.2025.110203
Mohanaphriya US, Tanmoy Chakraborty
<div><div>This objective of this study is to investigate the influence of nanoparticles (NPs) shapes — spherical, cylindrical, brick-like, and platelet — on stagnation-point flow and heat transfer in a Prandtl–Eyring hybrid nanofluid over a vertical Riga plate. Prandtl–Eyring fluid is considered as engine oil, with the suspension of <span><math><mrow><mi>C</mi><mi>u</mi></mrow></math></span> and <span><math><mrow><mi>Z</mi><mi>r</mi><msub><mrow><mi>O</mi></mrow><mrow><mn>2</mn></mrow></msub></mrow></math></span> nanoparticles. The analysis includes generalized Fourier heat conduction using the Cattaneo–Christov model along with solar radiation, and convective boundary conditions. Numerical solutions are obtained using the MATLAB’s stiff ordinary differential equation solver ode15s and optimized using the Matlab trust-region reflective algorithm. Results reveal that the Prandtl–Eyring parameters reduce the velocity but enhance temperature, while platelet-shaped nanoparticles yield the highest skin friction and heat transfer performance. A marginal 0.027% rise in the skin friction and up to 20.84% reduction in the rate of heat transportation are perceived across all the shapes within the relaxation time parameter (<span><math><mi>ξ</mi></math></span>) ranging between <span><math><mrow><mn>0</mn><mo>.</mo><mn>0</mn><mo>≤</mo><mi>ξ</mi><mo>≤</mo><mn>0</mn><mo>.</mo><mn>2</mn></mrow></math></span>. Furthermore, Entropy generation could be minimized by lowering the unsteadiness parameter and modified Hartmann number. Statistical analysis shows that the solar radiation parameter (<span><math><mi>R</mi></math></span>) has the most significant impact (70.35%) on the heat transfer, while the Prandtl–Eyring parameter 1 (<span><math><msup><mrow><mi>α</mi></mrow><mrow><mo>∗</mo></mrow></msup></math></span>) has the least (0.002%) impact. Based on the Taguchi optimization, the optimal parameter levels for maximizing heat transfer for the spherically shaped nanoparticles are: <span><math><msup><mrow><mi>α</mi></mrow><mrow><mo>∗</mo></mrow></msup></math></span> (Prandtl–Eyring parameter 1) <span><math><mrow><mo>=</mo><mn>1</mn><mo>.</mo><mn>2</mn></mrow></math></span>, <span><math><msup><mrow><mi>β</mi></mrow><mrow><mo>∗</mo></mrow></msup></math></span> (Prandtl–Eyring parameter 2) <span><math><mrow><mo>=</mo><mn>0</mn><mo>.</mo><mn>2</mn></mrow></math></span>, <span><math><mi>Z</mi></math></span> (modified Hartmann number) <span><math><mrow><mo>=</mo><mn>1</mn><mo>.</mo><mn>5</mn></mrow></math></span>, <span><math><mi>ξ</mi></math></span> (relaxation time parameter) <span><math><mrow><mo>=</mo><mn>0</mn><mo>.</mo><mn>2</mn></mrow></math></span>, <span><math><mi>R</mi></math></span> (Solar Radiation parameter) <span><math><mrow><mo>=</mo><mn>1</mn><mo>.</mo><mn>0</mn></mrow></math></span>, <span><math><mi>γ</mi></math></span> (surface convection parameter) <span><math><mrow><mo>=</mo><mn>15</mn></mrow></math></span>. Under these conditions, the maximum heat tran
本研究的目的是研究纳米颗粒(NPs)形状(球形、圆柱形、砖状和血小板状)对垂直Riga板上Prandtl-Eyring混合纳米流体中停滞点流动和传热的影响。将Prandtl-Eyring流体视为发动机润滑油,其中悬浮着Cu和ZrO2纳米颗粒。分析包括使用Cattaneo-Christov模型的广义傅里叶热传导以及太阳辐射和对流边界条件。利用MATLAB的刚性常微分方程求解器ode15s获得了数值解,并利用MATLAB的信任域反射算法进行了优化。结果表明,Prandtl-Eyring参数降低了速度,但提高了温度,而血小板形状的纳米颗粒具有最高的皮肤摩擦和传热性能。在松弛时间参数(ξ)范围在0.0≤ξ≤0.2之间的所有形状中,表面摩擦边际增加0.027%,热传递率减少20.84%。此外,通过降低非定常参数和修正哈特曼数,可以最大限度地减少熵的产生。统计分析表明,太阳辐射参数(R)对换热的影响最大(70.35%),Prandtl-Eyring参数1 (α∗)的影响最小(0.002%)。基于田口优化,使球形纳米颗粒传热最大化的最佳参数水平为:α∗(Prandtl-Eyring参数1)=1.2,β∗(Prandtl-Eyring参数2)=0.2,Z(修正哈特曼数)=1.5,ξ(松弛时间参数)=0.2,R(太阳辐射参数)=1.0,γ(表面对流参数)=15。在此条件下,得到的最大换热率为0.910954 W。
{"title":"Taguchi analysis on convective heat transfer of a Prandtl-Eyring hybrid nanofluid over a Riga plate: Entropy optimization","authors":"Mohanaphriya US,&nbsp;Tanmoy Chakraborty","doi":"10.1016/j.ijheatfluidflow.2025.110203","DOIUrl":"10.1016/j.ijheatfluidflow.2025.110203","url":null,"abstract":"&lt;div&gt;&lt;div&gt;This objective of this study is to investigate the influence of nanoparticles (NPs) shapes — spherical, cylindrical, brick-like, and platelet — on stagnation-point flow and heat transfer in a Prandtl–Eyring hybrid nanofluid over a vertical Riga plate. Prandtl–Eyring fluid is considered as engine oil, with the suspension of &lt;span&gt;&lt;math&gt;&lt;mrow&gt;&lt;mi&gt;C&lt;/mi&gt;&lt;mi&gt;u&lt;/mi&gt;&lt;/mrow&gt;&lt;/math&gt;&lt;/span&gt; and &lt;span&gt;&lt;math&gt;&lt;mrow&gt;&lt;mi&gt;Z&lt;/mi&gt;&lt;mi&gt;r&lt;/mi&gt;&lt;msub&gt;&lt;mrow&gt;&lt;mi&gt;O&lt;/mi&gt;&lt;/mrow&gt;&lt;mrow&gt;&lt;mn&gt;2&lt;/mn&gt;&lt;/mrow&gt;&lt;/msub&gt;&lt;/mrow&gt;&lt;/math&gt;&lt;/span&gt; nanoparticles. The analysis includes generalized Fourier heat conduction using the Cattaneo–Christov model along with solar radiation, and convective boundary conditions. Numerical solutions are obtained using the MATLAB’s stiff ordinary differential equation solver ode15s and optimized using the Matlab trust-region reflective algorithm. Results reveal that the Prandtl–Eyring parameters reduce the velocity but enhance temperature, while platelet-shaped nanoparticles yield the highest skin friction and heat transfer performance. A marginal 0.027% rise in the skin friction and up to 20.84% reduction in the rate of heat transportation are perceived across all the shapes within the relaxation time parameter (&lt;span&gt;&lt;math&gt;&lt;mi&gt;ξ&lt;/mi&gt;&lt;/math&gt;&lt;/span&gt;) ranging between &lt;span&gt;&lt;math&gt;&lt;mrow&gt;&lt;mn&gt;0&lt;/mn&gt;&lt;mo&gt;.&lt;/mo&gt;&lt;mn&gt;0&lt;/mn&gt;&lt;mo&gt;≤&lt;/mo&gt;&lt;mi&gt;ξ&lt;/mi&gt;&lt;mo&gt;≤&lt;/mo&gt;&lt;mn&gt;0&lt;/mn&gt;&lt;mo&gt;.&lt;/mo&gt;&lt;mn&gt;2&lt;/mn&gt;&lt;/mrow&gt;&lt;/math&gt;&lt;/span&gt;. Furthermore, Entropy generation could be minimized by lowering the unsteadiness parameter and modified Hartmann number. Statistical analysis shows that the solar radiation parameter (&lt;span&gt;&lt;math&gt;&lt;mi&gt;R&lt;/mi&gt;&lt;/math&gt;&lt;/span&gt;) has the most significant impact (70.35%) on the heat transfer, while the Prandtl–Eyring parameter 1 (&lt;span&gt;&lt;math&gt;&lt;msup&gt;&lt;mrow&gt;&lt;mi&gt;α&lt;/mi&gt;&lt;/mrow&gt;&lt;mrow&gt;&lt;mo&gt;∗&lt;/mo&gt;&lt;/mrow&gt;&lt;/msup&gt;&lt;/math&gt;&lt;/span&gt;) has the least (0.002%) impact. Based on the Taguchi optimization, the optimal parameter levels for maximizing heat transfer for the spherically shaped nanoparticles are: &lt;span&gt;&lt;math&gt;&lt;msup&gt;&lt;mrow&gt;&lt;mi&gt;α&lt;/mi&gt;&lt;/mrow&gt;&lt;mrow&gt;&lt;mo&gt;∗&lt;/mo&gt;&lt;/mrow&gt;&lt;/msup&gt;&lt;/math&gt;&lt;/span&gt; (Prandtl–Eyring parameter 1) &lt;span&gt;&lt;math&gt;&lt;mrow&gt;&lt;mo&gt;=&lt;/mo&gt;&lt;mn&gt;1&lt;/mn&gt;&lt;mo&gt;.&lt;/mo&gt;&lt;mn&gt;2&lt;/mn&gt;&lt;/mrow&gt;&lt;/math&gt;&lt;/span&gt;, &lt;span&gt;&lt;math&gt;&lt;msup&gt;&lt;mrow&gt;&lt;mi&gt;β&lt;/mi&gt;&lt;/mrow&gt;&lt;mrow&gt;&lt;mo&gt;∗&lt;/mo&gt;&lt;/mrow&gt;&lt;/msup&gt;&lt;/math&gt;&lt;/span&gt; (Prandtl–Eyring parameter 2) &lt;span&gt;&lt;math&gt;&lt;mrow&gt;&lt;mo&gt;=&lt;/mo&gt;&lt;mn&gt;0&lt;/mn&gt;&lt;mo&gt;.&lt;/mo&gt;&lt;mn&gt;2&lt;/mn&gt;&lt;/mrow&gt;&lt;/math&gt;&lt;/span&gt;, &lt;span&gt;&lt;math&gt;&lt;mi&gt;Z&lt;/mi&gt;&lt;/math&gt;&lt;/span&gt; (modified Hartmann number) &lt;span&gt;&lt;math&gt;&lt;mrow&gt;&lt;mo&gt;=&lt;/mo&gt;&lt;mn&gt;1&lt;/mn&gt;&lt;mo&gt;.&lt;/mo&gt;&lt;mn&gt;5&lt;/mn&gt;&lt;/mrow&gt;&lt;/math&gt;&lt;/span&gt;, &lt;span&gt;&lt;math&gt;&lt;mi&gt;ξ&lt;/mi&gt;&lt;/math&gt;&lt;/span&gt; (relaxation time parameter) &lt;span&gt;&lt;math&gt;&lt;mrow&gt;&lt;mo&gt;=&lt;/mo&gt;&lt;mn&gt;0&lt;/mn&gt;&lt;mo&gt;.&lt;/mo&gt;&lt;mn&gt;2&lt;/mn&gt;&lt;/mrow&gt;&lt;/math&gt;&lt;/span&gt;, &lt;span&gt;&lt;math&gt;&lt;mi&gt;R&lt;/mi&gt;&lt;/math&gt;&lt;/span&gt; (Solar Radiation parameter) &lt;span&gt;&lt;math&gt;&lt;mrow&gt;&lt;mo&gt;=&lt;/mo&gt;&lt;mn&gt;1&lt;/mn&gt;&lt;mo&gt;.&lt;/mo&gt;&lt;mn&gt;0&lt;/mn&gt;&lt;/mrow&gt;&lt;/math&gt;&lt;/span&gt;, &lt;span&gt;&lt;math&gt;&lt;mi&gt;γ&lt;/mi&gt;&lt;/math&gt;&lt;/span&gt; (surface convection parameter) &lt;span&gt;&lt;math&gt;&lt;mrow&gt;&lt;mo&gt;=&lt;/mo&gt;&lt;mn&gt;15&lt;/mn&gt;&lt;/mrow&gt;&lt;/math&gt;&lt;/span&gt;. Under these conditions, the maximum heat tran","PeriodicalId":335,"journal":{"name":"International Journal of Heat and Fluid Flow","volume":"118 ","pages":"Article 110203"},"PeriodicalIF":2.6,"publicationDate":"2026-03-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"145797337","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":3,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
A review on the asymmetry, steady instability and bistability in the wake of industrial ground vehicles 工业地面车辆尾迹的不对称性、稳态不稳定性和双稳定性研究进展
IF 2.6 3区 工程技术 Q2 ENGINEERING, MECHANICAL Pub Date : 2026-03-01 Epub Date: 2025-12-19 DOI: 10.1016/j.ijheatfluidflow.2025.110208
Olivier Cadot
Since the first observation of steady symmetry breaking in the turbulent wakes of a square-back Ahmed body by Grandemange et al. (2012), there have been reports of similar effects with ground vehicles of more complex geometries with square-back style, including real vehicles. The article reviews these cases of industrial flows, either at small or full scale in wind tunnels or numerical simulations with and without road effects. A clear consensus appears of asymmetric recirculating flows in the vertical direction that can, with well chosen parametric variations, reverse to the opposite asymmetry and sometimes lead to spectacular vertical bistable dynamics. These global changes of the base flow impact the body drag and lift. The underlying universal property of these wakes is likely the same steady instability as that of the square-back Ahmed body.
自从Grandemange等人(2012)首次观察到方形后置Ahmed体湍流尾迹中的稳定对称性破坏以来,已经有报道称,具有方形后置风格的更复杂几何形状的地面车辆(包括真实车辆)也有类似的效果。本文回顾了这些工业流动的案例,无论是在风洞中的小尺度或全尺度,还是在有或没有道路影响的情况下的数值模拟。一个明确的共识是,在垂直方向上的非对称再循环流动,可以通过精心选择的参数变化,逆转到相反的不对称,有时会导致壮观的垂直双稳态动力学。这些基流的整体变化影响了机体的阻力和升力。这些尾迹潜在的普遍特性很可能与阿迈德的方背体一样具有稳定的不稳定性。
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引用次数: 0
Design and performance optimization of liquid immersion cooling system for prismatic lithium-ion battery modules 棱镜型锂离子电池模块液浸冷却系统设计及性能优化
IF 2.6 3区 工程技术 Q2 ENGINEERING, MECHANICAL Pub Date : 2026-03-01 Epub Date: 2025-12-08 DOI: 10.1016/j.ijheatfluidflow.2025.110181
Luyao Zhao, Jiafeng Wang, Minxue Zheng, Mingyi Chen
Optimal thermal regulation in battery modules is critical for maintaining the efficient and reliable operation of battery packs. This study designed an active immersion cooling system for prismatic lithium-ion battery modules, demonstrating maximum temperature reductions of 34 % and 47.7 % relative to static submersion cooling and free convection methods, respectively. The impacts of coolant flow rate, flow direction, and module arrangement patterns on forced-flow immersion cooling performance were numerically investigated. Results indicate that parallel battery arrangements show superior cooling performance compared to staggered configurations. Among the five flow patterns (top to bottom, bottom to top, top to top, bottom to bottom, and center to center), the top to bottom layout exhibits the optimal cooling efficiency. As the inlet flow rate increases, both the maximum battery temperature and the temperature difference across the battery pack first drop sharply and then slowly after the flow rate reaches 0.023 kg/s. Power consumption demonstrates a positive relationship with inlet velocity, whereas the cooling index shows an inverse relationship. As the horizontal spacing between batteries varies from 1 to 6 mm, the maximum temperature of the battery and temperature difference show a “U” shaped trend, the power consumption decreases monotonically, while the cooling index shows a “И” shaped variation trend. Similarly, with the increase of longitudinal distance between batteries, Both the peak battery temperature and temperature differential present a “U” shaped variation trend, and the power dissipation decreases monotonically. Conversely, the cooling index increases monotonously. Finally, a 4-mm horizontal and 5-mm longitudinal spacing were identified as the optimal configuration. This study addressed both operational safety and thermal management efficiency for prismatic lithium-ion batteries, and established design guidelines for high-performance immersion cooling systems.
电池模块的最佳热调节对于保持电池组的高效可靠运行至关重要。该研究为棱柱形锂离子电池模块设计了一种主动浸没冷却系统,与静态浸没冷却和自由对流冷却方法相比,最大温度分别降低了34%和47.7%。研究了冷却剂流量、流动方向和模块布置方式对强制浸没冷却性能的影响。结果表明,与交错配置相比,并联电池配置具有更好的冷却性能。在5种流动模式(从上到下、从下到上、从上到上、从下到下、从中心到中心)中,从上到下的布局具有最佳的冷却效率。随着进口流量的增加,在流量达到0.023 kg/s后,电池最高温度和电池组温差均先急剧下降,然后缓慢下降。功率消耗与进口速度呈正相关,而冷却指数呈反比关系。当电池水平间距在1 ~ 6mm范围内变化时,电池最高温度和温差呈“U”型变化趋势,功耗单调下降,冷却指数呈“И”型变化趋势。同样,随着电池间纵向距离的增加,电池峰值温度和温差均呈“U”型变化趋势,且功耗单调减小。反之,冷却指数单调增加。最后,确定水平间距为4 mm,纵向间距为5 mm为最优配置。该研究解决了棱柱形锂离子电池的操作安全性和热管理效率,并建立了高性能浸入式冷却系统的设计指南。
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引用次数: 0
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International Journal of Heat and Fluid Flow
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