Multi-objective optimization of comprehensive performance in airfoil channel PCHEs using Bezier curves

被引:0
|
作者
Liu, Rui [1 ]
Zhang, Chuanliang [1 ]
Zhao, Bin [2 ]
Chen, Jiaxiang [1 ]
Wang, Ziyi [1 ]
机构
[1] Changsha Univ Sci & Technol, Coll Energy & Power Engn, Changsha 410114, Peoples R China
[2] Changsha Univ Sci & Technol, Sch Elect & Informat Engn, Changsha 410114, Peoples R China
基金
中国国家自然科学基金;
关键词
Airfoil fin PCHE; Be<acute accent>zier curves; Pareto front; Multi-objective genetic algorithm; Comprehensive performance; CIRCUIT HEAT-EXCHANGER; THERMAL-HYDRAULIC PERFORMANCE; COLBURN J FACTOR; FINS; ZIGZAG; STRAIGHT;
D O I
10.1016/j.applthermaleng.2024.125045
中图分类号
O414.1 [热力学];
学科分类号
摘要
The airfoil fin (AFF) Printed circuit heat exchanger (PCHE) has attracted significant attention for its excellent comprehensive performance. This study proposes an optimized design for AFF PCHE to enhance the comprehensive performance by integrating Be<acute accent>zier curves, computational fluid dynamics (CFD), and multi-objective genetic algorithm (MOGA). A set of 12 Be<acute accent>zier curve-based variables is utilized to define and control the airfoil geometry, with optimization targets set on two comprehensive evaluation criteria: the first enhanced ratio (n1) and the third enhanced ratio (n3). The MOGA-generated Pareto front reveals the evolution of AFF structures in relation to n1 and n3. Results show that as the leading and trailing edges of the AFFs become sharper and the thickness decreases, the n1 of the PCHE channel gradually increases, while n3 decreases. Conversely, as the thickness of the AFFs increases and the trailing edge shape transitions from blunt to elliptical and finally to round, n3 significantly increases while n1 decreases. Furthermore, when changes focus mainly on the leading edge of the AFFs, n3 improves without markedly affecting n1. Compared to the traditional airfoil channel, the n1 of the Fin-b channel increases by 3.1%-10.8%, demonstrating its greater suitability under identical flow rate conditions. Similarly, the n3 of the Fin-g channel is 1.4%-11.6% higher than that of the traditional airfoil channel, highlighting its superior performance under identical pumping power conditions. The present work provides a valuable reference for optimizing the design of AFF PCHEs under identical flow rate and pumping power conditions.
引用
收藏
页数:14
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