Volume 40 Issue 8
Aug.  2025
Turn off MathJax
Article Contents
LIU Zhiwei, XU Guoqiang, WEN Jie, et al. Analytical method on heat conduction performance of anisotropic pin fins[J]. Journal of Aerospace Power, 2025, 40(8):20240450 doi: 10.13224/j.cnki.jasp.20240450
Citation: LIU Zhiwei, XU Guoqiang, WEN Jie, et al. Analytical method on heat conduction performance of anisotropic pin fins[J]. Journal of Aerospace Power, 2025, 40(8):20240450 doi: 10.13224/j.cnki.jasp.20240450

Analytical method on heat conduction performance of anisotropic pin fins

doi: 10.13224/j.cnki.jasp.20240450
  • Received Date: 2024-07-03
    Available Online: 2025-01-15
  • A mathematical model was constructed to describe the heat conduction problem of anisotropic pin fins. Through dimensionless analyses, the dimensionless criterion numbers were obtained, which affected the heat transfer process of the fins. Variable separation method, Taylor expansion, and integral averaging were applied to solve the differential equation. Analytical correlations for fin efficiency and heat transfer rate were derived and numerically verified. Based on the proposed analytical solutions, the influence of the direction of the heat conductivity principal axis on anisotropic pin fins was analyzed. The results showed that within the range of radial Bi was 0.05—10, axial Bi was 0.005—10, cross Bi was 0.2—10, and length to diameter ratio of fin was 2—20, the relative error of fin efficiency from the proposed correlation was less than 1.06% compared with the numerical results. Due to the circumferential symmetry of the temperature field, when the heat conductivity principal axis was deflected in the rOφ and φOz planes, it was beneficial to enhance the fins’ heat transfer performance by making the axis, which had a higher principal heat conductivity coefficient along the r and z directions. However, when the axis was deflected in the rOz plane, the optimal deflection angle can be calculated to maximize the heat transfer performance of the fins under given boundary conditions, material properties, and length to diameter ratio. And the maximum heat transfer rate was 2.97 times that of α=0. The results provide a theoretical support for the design of anisotropic pin fins in application.

     

  • loading
  • [1]
    杜昆, 陈麒好, 孟宪龙, 等. 陶瓷基复合材料在航空发动机热端部件应用及热分析研究进展[J]. 推进技术, 2022, 43(2): 210380. DU Kun, CHEN Qihao, MENG Xianlong, et al. Advancement in application and thermal analysis of ceramic matrix composites in aeroengine hot components[J]. Journal of Propulsion Technology, 2022, 43(2): 210380. (in Chinese

    DU Kun, CHEN Qihao, MENG Xianlong, et al. Advancement in application and thermal analysis of ceramic matrix composites in aeroengine hot components[J]. Journal of Propulsion Technology, 2022, 43(2): 210380. (in Chinese)
    [2]
    BEHRENS E. Thermal conductivities of composite materials[J]. Journal of Composite Materials, 1968, 2(1): 2-17. doi: 10.1177/002199836800200101
    [3]
    周洲, 刘闯, 朱学忠, 等. 航空第二动力系统技术综述[J]. 航空动力学报, 2024, 39(8): 20220561. ZHOU Zhou, LIU Chuang, ZHU Xuezhong, et al. Review on aircraft secondary power system[J]. Journal of Aerospace Power, 2024, 39(8): 20220561. (in Chinese

    ZHOU Zhou, LIU Chuang, ZHU Xuezhong, et al. Review on aircraft secondary power system[J]. Journal of Aerospace Power, 2024, 39(8): 20220561. (in Chinese)
    [4]
    江华, 毛军逵, 屠泽灿, 等. 基于微结构识别的单向复合材料导热系数预估[J]. 航空动力学报, 2016, 31(11): 2641-2651. JIANG Hua, MAO Junkui, TU Zecan, et al. Thermal conductivity prediction of unidirectional composites based on microstructure identification[J]. Journal of Aerospace Power, 2016, 31(11): 2641-2651. (in Chinese

    JIANG Hua, MAO Junkui, TU Zecan, et al. Thermal conductivity prediction of unidirectional composites based on microstructure identification[J]. Journal of Aerospace Power, 2016, 31(11): 2641-2651. (in Chinese)
    [5]
    李典森, 卢子兴, 刘振国, 等. 三维五向编织复合材料导热性能的有限元分析[J]. 航空动力学报, 2008, 23(8): 1455-1460. LI Diansen, LU Zixing, LIU Zhenguo, et al. Finite element analysis of thermal conductivity of three dimensional and five directional braided composites[J]. Journal of Aerospace Power, 2008, 23(8): 1455-1460. (in Chinese

    LI Diansen, LU Zixing, LIU Zhenguo, et al. Finite element analysis of thermal conductivity of three dimensional and five directional braided composites[J]. Journal of Aerospace Power, 2008, 23(8): 1455-1460. (in Chinese)
    [6]
    陆思达, 高希光, 宋迎东. 基于有限元法的平纹编织C/SiC复合材料等效导热系数预测方法[J]. 航空动力学报, 2014, 29(7): 1574-1582. LU Sida, GAO Xiguang, SONG Yingdong. Prediction method on equivalent thermal conductivity coefficient of plain braided C/SiC composites material based on finite element method[J]. Journal of Aerospace Power, 2014, 29(7): 1574-1582. (in Chinese

    LU Sida, GAO Xiguang, SONG Yingdong. Prediction method on equivalent thermal conductivity coefficient of plain braided C/SiC composites material based on finite element method[J]. Journal of Aerospace Power, 2014, 29(7): 1574-1582. (in Chinese)
    [7]
    ASLIB I, HAMZA H, HANCHI N, et al. Numerical study of transient and steady-state anisotropic cylindrical pin fin thermal behavior[J]. Journal of Thermal Science and Engineering Applications, 2019, 11(3): 031007. doi: 10.1115/1.4042056
    [8]
    AKULA R, BALAJI C. Thermal management of 18650 Li-ion battery using novel fins-PCM-EG composite heat sinks[J]. Applied Energy, 2022, 316: 119048. doi: 10.1016/j.apenergy.2022.119048
    [9]
    侯亚东, 单勇, 李江宁, 等. 各向异性复合材料平板气膜冷却特性实验和数值研究[J]. 航空动力学报, 2017, 32(10): 2384-2393. HOU Yadong, SHAN Yong, LI Jiangning, et al. Experimental and numerical studies on the film cooling characteristics of anisotropic composite plates[J]. Journal of Aerospace Power, 2017, 32(10): 2384-2393. (in Chinese

    HOU Yadong, SHAN Yong, LI Jiangning, et al. Experimental and numerical studies on the film cooling characteristics of anisotropic composite plates[J]. Journal of Aerospace Power, 2017, 32(10): 2384-2393. (in Chinese)
    [10]
    屠泽灿, 毛军逵, 徐瑞, 等. 各向异性陶瓷基复合材料涡轮叶片概率性热分析方法[J]. 航空动力学报, 2017, 32(10): 2427-2437. TU Zecan, MAO Junkui, XU Rui, et al. Probabilistic thermal analysis of ceramic matrix composite turbine vane with anisotropic thermal conductivity[J]. Journal of Aerospace Power, 2017, 32(10): 2427-2437. (in Chinese

    TU Zecan, MAO Junkui, XU Rui, et al. Probabilistic thermal analysis of ceramic matrix composite turbine vane with anisotropic thermal conductivity[J]. Journal of Aerospace Power, 2017, 32(10): 2427-2437. (in Chinese)
    [11]
    于国强, 隋正卿, 陈正扬, 等. 类椭圆形 CMC 火焰筒多斜孔冷却性能数值分析[J]. 航空动力学报, 2025, 40(1): 20230084. YU Guoqiang, SUI Zhengqing, CHEN Zhengyang, et al. Numerical analysis on cooling performance of quasi-elliptic multi inclined holes in CMC combustion liner[J]. Journal of Aerospace Power, 2025, 40(1): 20230084. (in Chinese

    YU Guoqiang, SUI Zhengqing, CHEN Zhengyang, et al. Numerical analysis on cooling performance of quasi-elliptic multi inclined holes in CMC combustion liner[J]. Journal of Aerospace Power, 2025, 40(1): 20230084. (in Chinese)
    [12]
    POWERS J M. On the necessity of positive semi-definite conductivity and Onsager reciprocity in modeling heat conduction in anisotropic media[J]. Journal of Heat Transfer, 2004, 126(5): 670-675. doi: 10.1115/1.1798913
    [13]
    LUNA-ABAD J P, ALHAMA F. Design and optimization of composite rectangular fins using the relative inverse thermal admittance[J]. Journal of Heat Transfer, 2013, 135(8): 084504. doi: 10.1115/1.4024016
    [14]
    ZUBAIR S M, ARIF A F M, SHARQAWY M H. Thermal analysis and optimization of orthotropic pin fins: a closed-form analytical solution[J]. Journal of Heat Transfer, 2010, 132(3): 031301. doi: 10.1115/1.4000059
    [15]
    BAHADUR R, BAR-COHEN A. Orthotropic thermal conductivity effect on cylindrical pin fin heat transfer[J]. International Journal of Heat and Mass Transfer, 2007, 50(5/6): 1155-1162.
    [16]
    HSIEH M H, MA C C. Analytical investigations for heat conduction problems in anisotropic thin-layer media with embedded heat sources[J]. International Journal of Heat and Mass Transfer, 2002, 45(20): 4117-4132. doi: 10.1016/S0017-9310(02)00136-9
    [17]
    CHANG Y P, TSOU R C H. Heat conduction in an anisotropic medium homogeneous in cylindrical regions—steady state[J]. Journal of Heat Transfer, 1977, 99(1): 132-134. doi: 10.1115/1.3450636
    [18]
    NOROUZI M, RAHMANI H, BIRJANDI A K, et al. A general exact analytical solution for anisotropic non-axisymmetric heat conduction in composite cylindrical shells[J]. International Journal of Heat and Mass Transfer, 2016, 93: 41-56. doi: 10.1016/j.ijheatmasstransfer.2015.09.072
    [19]
    KAYHANI M H, NOROUZI M, AMIRI DELOUEI A. A general analytical solution for heat conduction in cylindrical multilayer composite laminates[J]. International Journal of Thermal Sciences, 2012, 52: 73-82. doi: 10.1016/j.ijthermalsci.2011.09.002
    [20]
    HILL R. Elastic properties of reinforced solids: some theoretical principles[J]. Journal of the Mechanics and Physics of Solids, 1963, 11(5): 357-372. doi: 10.1016/0022-5096(63)90036-X
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索

    Article Metrics

    Article views (553) PDF downloads(37) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return