Bai Manying, Ren Ruoen. Study on the Existence and Uniqueness of G-K System in Multilateral International Comparison[J]. Journal of Beijing University of Aeronautics and Astronautics, 1999, 25(2): 216-220. (in Chinese)
Citation: Li Xiaojuan, Gui Xingmin. Numerical simulation of three dimension viscous flow of fan/compressor with tip clearance[J]. Journal of Beijing University of Aeronautics and Astronautics, 2006, 32(01): 4-7. (in Chinese)

Numerical simulation of three dimension viscous flow of fan/compressor with tip clearance

  • Received Date: 15 Oct 2004
  • Publish Date: 31 Jan 2006
  • A three dimension numerical simulation software named NUMECA(numerical mechanics application) was used to calculate the tip clearance flow of fan/compressor. The flow field performance under design speed condition was obtained. The results show that when back pressure of by-pass duct increases, the intensive blockage area moves upstream and towards the fan pressure surface, and twist of shock become more obvious. The efficiency and the mass flow of the by-pass duct decrease if the back pressure of the by-pass duct increases unceasingly. Atcore duct, the area influenced by tip clearance leakage flow spreads to upstream with the increase of back pressure. In the same way, the efficiency and the mass flow of the core duct decrease if the back pressure of core duct is too great. The comparison between the results and the experiments shows that the numerical simulation results of three dimension viscous flow of fan compressor with tip clearance could actually reflect the influences of leakage flows on the flow structure and parameters.

     

  • [1] 桂幸民,王同庆,于 清,等. 跨音压气机转子叶尖流场试验与 分析[J] 程热物理学报,1998, 19(5):553~558 Gui Xingmin, Wang Tongqing, Yu Qing, et al. Investigation on the tip clearance flow field in a transonic compressor rotor[J] Journal of Engineering Thermophysics, 1998, 19(5):553~558(in Chinese) [2] 桂幸民,聂超群,王同庆,等. 跨音压气机转子叶尖间隙复杂 流动观测[J] 程热物理学报,2000, 21(5):570~572 Gui Xingmin, Nie Chaoqun, Wang Tongqing, et al. Tip clearance flow in a transonic compressor rotor[J] Journal of Engineering Thermophysics, 2000, 21(5):570~572(in Chinese) [3] Copenhaver W W, Mayhew E R, Hah C. The effect of tip clearance on a swept transonic compressor rotor, ASME-94-GT-363,1994 [4] 敬荣强,李泯江,桂幸民. 高负荷跨音压气机叶尖间隙流动的数值分析与比较[J] 空动力学报,2003, 18(6):827~831 Jing Rongqiang, Li Minjiang, Gui Xingmin. A numerical analysis and comparison of the tip-clearance flow of a high-loading transonic compressor[J] Journal of Aerospace Power, 2003, 18(6):827~831(in Chinese)
  • Relative Articles

    [1]HAO D,LIU J X,SU J,et al. Optimization of multilayer thermal insulation structure for high-speed aircraft considering material optimization[J]. Journal of Beijing University of Aeronautics and Astronautics,2025,51(5):1662-1672 (in Chinese). doi: 10.13700/j.bh.1001-5965.2023.0261.
    [2]WANG C S,ZHANG X Y,ZHAN Z X,et al. Analysis of compression stability and load capacity of thick composite plate structures[J]. Journal of Beijing University of Aeronautics and Astronautics,2025,51(1):94-101 (in Chinese). doi: 10.13700/j.bh.1001-5965.2022.0991.
    [3]LI Keyu, YANG Chao, WANG Xiaozhe, WAN Zhiqiang, LI Chang. Aeroelastic optimization of wing structure and material using multiple microstructures[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0178
    [4]LU Ming-yu, ZHANG Ming, WEI Yu-xuan, LI Bo, CUI Zhi-gang, ZHANG Kai-hu. Characteristics and Homogenization Removal Methods of Ultraviolet Femtosecond Laser Processing of Aerospace AFRP Composite Materials[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0096
    [5]DENG J X,CHEN L,LU S T,et al. Damage distribution of composite structures of a certain type aircraft[J]. Journal of Beijing University of Aeronautics and Astronautics,2024,50(3):920-930 (in Chinese). doi: 10.13700/j.bh.1001-5965.2022.0379.
    [6]PIAN Rong, YANG Fan, ZHANG Ling, LIU Feng-rui, WANG Lin-juan, ZHAO Li-bin. Failure mode study of composite laminated plates under compression-shear loading[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0084
    [7]GENG Z T,ZHAO J Q. Design and development of virtual simulation experiment software of composite piezoelectric materials[J]. Journal of Beijing University of Aeronautics and Astronautics,2024,50(11):3377-3381 (in Chinese). doi: 10.13700/j.bh.1001-5965.2022.0826.
    [8]YANG Z G,KE Z S,YANG X W,et al. Analysis of effect of construction process on electrical properties of composite skins[J]. Journal of Beijing University of Aeronautics and Astronautics,2024,50(10):3013-3020 (in Chinese). doi: 10.13700/j.bh.1001-5965.2022.0763.
    [9]WANG Z X,WAN Z Q,WANG X Z,et al. Fast stability analysis method for composite panel with variable angle tow fiber[J]. Journal of Beijing University of Aeronautics and Astronautics,2023,49(2):353-366 (in Chinese). doi: 10.13700/j.bh.1001-5965.2021.0259.
    [10]XU M R,ZENG B Y,XIONG X,et al. Tensile fatigue properties of carbon fiber laminates in hygrothermal environments[J]. Journal of Beijing University of Aeronautics and Astronautics,2023,49(7):1614-1622 (in Chinese). doi: 10.13700/j.bh.1001-5965.2021.0565.
    [11]XIAO Yao, LI Yong, LI Dong-sheng, WANG Lei, JIANG Chao. Influence analysis of curing stress and stress relaxation on profile accuracy of carbon fiber reinforced composites tools[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023-0109
    [12]DONG H M,LI X G,MA X Q,et al. Research progress in mechanically fastened polymer-matrix composite joints with protruding-head bolts[J]. Journal of Beijing University of Aeronautics and Astronautics,2023,49(4):745-760 (in Chinese). doi: 10.13700/j.bh.1001-5965.2022.0682.
    [13]WANG L Y,CHEN W H,JIANG Y S,et al. Measurement of ejection factor of new resin matrix composites[J]. Journal of Beijing University of Aeronautics and Astronautics,2023,49(11):2960-2967 (in Chinese). doi: 10.13700/j.bh.1001-5965.2022.0056.
    [14]YANG Zhan-gang, WEI Yu-hao, SHI Xu-dong. Electrical Properties Analysis of Composite Skin Bonding Structures[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0507
    [15]LI Xing, LI Zeng-shan, DENG Fan-chen, NIE Lei, ZHANG Tian. Sub-model Based Failure Analysis of Composite Hybrid Joint Structure[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0555
    [16]LI T S,WANG S K,WU Q,et al. Interface adjustment of aerospace-grade T800 carbon fiber composite material[J]. Journal of Beijing University of Aeronautics and Astronautics,2023,49(8):2011-2020 (in Chinese). doi: 10.13700/j.bh.1001-5965.2021.0619.
    [17]DONG X X,YUE Z J,WANG Z,et al. Uncertainty lightweight design of sandwich structure of rocket fairing cone[J]. Journal of Beijing University of Aeronautics and Astronautics,2023,49(3):625-635 (in Chinese). doi: 10.13700/j.bh.1001-5965.2021.0267.
    [18]CHEN S Z,LI D C,XIANG J W. Design optimization of tow-steered composite structure targeting on manufacturing cost[J]. Journal of Beijing University of Aeronautics and Astronautics,2023,49(9):2423-2431 (in Chinese). doi: 10.13700/j.bh.1001-5965.2021.0677.
    [19]YANG Zhan-gang, KE Zhong-shu, YANG Xu-wei, BAO Xing-wang. Analysis of the influence of finishing process on the electrical properties of composite skin[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2022-0763
    [20]YANG Hui, FAN Shuoshuo, WANG Yan, LIU Rongqiang, XIAO Hong. Stiffness optimization of M-shaped boom based on radial basis function surrogate model[J]. Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(11): 2121-2129. doi: 10.13700/j.bh.1001-5965.2021.0091
  • 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(2956) PDF downloads(1231) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return