GAO J Y, ZHANG J, NI Z S, et al. The aerodynamic characteristics of roof-wing combination of a high-speed train[J]. Journal of Experiments in Fluid Mechanics, 2023, 37(1): 29-35. DOI: 10.11729/syltlx20220053
Citation: GAO J Y, ZHANG J, NI Z S, et al. The aerodynamic characteristics of roof-wing combination of a high-speed train[J]. Journal of Experiments in Fluid Mechanics, 2023, 37(1): 29-35. DOI: 10.11729/syltlx20220053

The aerodynamic characteristics of roof-wing combination of a high-speed train

More Information
  • Received Date: June 19, 2022
  • Revised Date: July 24, 2022
  • Accepted Date: August 17, 2022
  • Available Online: October 08, 2022
  • Adding the aeronautic wing to the high-speed train equivalently reduces its weight through the lift force provided by the wing. Hopefully, the energy consumption of the high-speed train can be reduced. This provides a new concept for the high speed train design. The aerodynamic characteristics of the wing directly affect the weight reduction effects. Therefore, it is important to analyze the aerodynamic characteristics of the wing under different conditions for the design of the train lift wing. The kε model was used in this study for numerical simulation. Firstly, the influence of the connection rod between the wing and the train roof on the aerodynamic characteristics of the lift wing was analyzed. On this basis, the effects of design parameters such as the wing-roof height, the incoming flow velocity and the angle of attack on the aerodynamic characteristics of the wing were studied. The results shows that: the influence of the connection rod on the lift and drag of the wing is less than 3.7%. Due to the high-speed airflow induced by the leading edge of the train roof model, the air velocity impacting on the lift wing decreases with the increase of the flying height of the lift wing, and the lift force tends to decrease. Within 3 times of the chord length height, the maximum lift difference of different lift wings does will not exceed 3%. When the velocity of the incoming flow is up to 90 m/s and larger, the lift coefficient and the drag coefficient of the lift wing were close to near 1.62 and 0.61, respectively. As the angle of attack varies within 0° to 22°, the lift coefficients of the wing increase continuously. However, the lift coefficients decrease when the attack angle is above 22°.
  • [1]
    王瑞东, 倪章松, 张军, 等. 高速列车串列升力翼翼型优化设计[J]. 空气动力学学报, 2022, 40(2): 129–137. DOI: 10.7638/kqdlxxb-2021.0203

    WANG R D, NI Z S, ZHANG J, et al. Optimization design of tandem airfoils on high-speed train[J]. Acta Aerody-namica Sinica, 2022, 40(2): 129–137. doi: 10.7638/kqdlxxb-2021.0203
    [2]
    SHELDAHL R E, KLIMAS P C. Aerodynamic characteris-tics of seven symmetrical airfoil sections through 180-degree angle of attack for use in aerodynamic analysis of vertical axis wind turbines[R]. SAND-80-2114, 1981. doi: 10.2172/6548367
    [3]
    McALISTER K W, TAKAHASHI R K. NACA 0015 wing pressure and trailing vortex measurements[R]. NASA-TP-3151, 1991.
    [4]
    JOSLIN R D, BAKER W J, PATERSON E G, et al. Aerodynamic prediction of a NACA0015-flap control con-figuration[C]//Proc of the 40th AIAA Aerospace Sciences Meeting & Exhibit. 2002. doi: 10.2514/6.2002-410
    [5]
    LEE S J, JEONG E C, LIM H C. Numerical study on aerodynamic characteristics of NACA0015[J]. Applied Mechanics and Materials, 2013, 302: 640–645. doi: 10.4028/www.scientific.net/amm.302.640
    [6]
    AHMED M R, TAKASAKI T, KOHAMA Y. Aerodynamics of a NACA4412 airfoil in ground effect[J]. AIAA Journal, 2007, 45(1): 37–47. doi: 10.2514/1.23872
    [7]
    SINGH N. Analysis of aerodynamic characteristics of various airfoils at sonic speed[J]. International Journal of Engineering Research & Technical, 2016, 5(9): 405–411. doi: 10.17577/ijertv5is090321
    [8]
    GERAKOPULOS R, BOUTILIER M S H, YARUSEVYCH S. Aerodynamic characterization of a NACA 0018 airfoil at low Reynolds numbers[C]//Proc of the 40th Fluid Dynamics Conference and Exhibit. 2010: 4629. doi: 10.2514/6.2010-4629
    [9]
    GAO D G, NI F, LIN G B, et al. Aerodynamic analysis of pressure wave of high-speed maglev vehicle crossing: model-ing and calculation[J]. Energies, 2019, 12(19): 3770. doi: 10.3390/en12193770
    [10]
    毕海权, 雷波, 张卫华. TR型磁浮列车气动力特性数值计算研究[J]. 铁道学报, 2004, 26(4): 51–54. DOI: 10.1007/BF02911033

    BI H Q, LEI B, ZHANG W H. Research on numerical calculation for aerodynamic characteristics of the TR maglev train[J]. Journal of the China Railway Society, 2004, 26(4): 51–54. doi: 10.1007/BF02911033
    [11]
    庄礼贤, 尹协远, 马晖扬, 等. 流体力学(第2版)[M]. 合肥: 中国科学技术大学出版社, 2009.
    [12]
    VERSTEEG H K, MALALASEKERA W. An introduction to computational fluid dynamics[M]. 北京: 世界图书出版公司北京公司, 2000.
    [13]
    YAO S B, SUN Z X, GUO D L, et al. Numerical study on wake characteristics of high-speed trains[J]. Acta Mechanica Sinica, 2013, 29(6): 811–822. doi: 10.1007/s10409-013-0077-3
    [14]
    姚曙光, 许平. 国产磁浮列车外形气动性能分析[J]. 铁道机车车辆, 2007, 27(3): 33–34,69. DOI: 10.3969/j.issn.1008-7842.2007.03.012

    YAO S G, XU P. Aerodynamic shape optimization of domestic maglev train[J]. Railway Locomotive & Car, 2007, 27(3): 33–34,69. doi: 10.3969/j.issn.1008-7842.2007.03.012
    [15]
    McGHEE R J, BEASLEY W. Low speed aerodynamic characteristics of a 17 percent thick airfoil section designed for general aviation applications[R]. NASA-TN-D-7428, 1973.
  • Related Articles

    [1]SONG Huazhen, ZHAO Huanyu, ZHU Chengxiang, WANG Zhengzhi, TIAN Wei, LI Haixing, ZHU Chunling. Three-dimensional liquid film flow measurement based on digital image projection technology[J]. Journal of Experiments in Fluid Mechanics, 2021, 35(5): 106-114. DOI: 10.11729/syltlx20200031
    [2]ZHANG Lei, ZHANG Ruoling, XIAO Shide, LIU Yu, XIONG Ying. Experimental investigation on high temperature deformation of regeneratively cooled combustor structure based on non-contact measurement[J]. Journal of Experiments in Fluid Mechanics, 2021, 35(1): 53-59. DOI: 10.11729/syltlx20200051
    [3]Wang Hongwei, Huang Zhan. Research on particle image velocimetry based on optical flow[J]. Journal of Experiments in Fluid Mechanics, 2015, (3): 68-75. DOI: 10.11729/syltlx20140115
    [4]Tao Bo, Wang Sheng, Hu Zhiyun, Zhang Lirong, Zhang Zhenrong, Ye Xisheng. TDLAS 技术二次谐波法测量发动机温度[J]. Journal of Experiments in Fluid Mechanics, 2015, (2): 68-72. DOI: 10.11729/syltlx20140053
    [5]GU Yi, CEN Fei, WEN Yu-chang, LIU Zhi-tao, CHE Bing-hui. Research about continuous scanning test technique based on non-contact measurement technique in low speed wind tunnel[J]. Journal of Experiments in Fluid Mechanics, 2013, 27(5): 98-104. DOI: 10.3969/j.issn.1672-9897.2013.05.019
    [6]XU Ming, WANG Hao-li. Measurement of velocity by micro-PIV technique based on overlap of low density particle images[J]. Journal of Experiments in Fluid Mechanics, 2013, 27(2): 106-112. DOI: 10.3969/j.issn.1672-9897.2013.02.021
    [7]WANG Yuan, YANG Bin, WANG Da-wei. Advances in wind-blown sand flow optical measurement and image processing techniques[J]. Journal of Experiments in Fluid Mechanics, 2010, 24(1): 55-64. DOI: 10.3969/j.issn.1672-9897.2010.01.011
    [8]ZHU Ru-song, KANG Hu. The real-time model angle of attack measurement based on image and it's application in wind tunnel[J]. Journal of Experiments in Fluid Mechanics, 2006, 20(4): 63-68,72. DOI: 10.3969/j.issn.1672-9897.2006.04.012
    [9]Method of measuring cavity's shapes at axially symmetrical bodies[J]. Journal of Experiments in Fluid Mechanics, 2004, 18(1): 67-70. DOI: 10.3969/j.issn.1672-9897.2004.01.015
    [10]XI Hua, ZHANG Xi-wen, HE Feng, XU Yang, XU Hong-qing. The investigation of particle removal efficiency beneath an impinging jet with image processing[J]. Journal of Experiments in Fluid Mechanics, 2000, 14(2): 40-43. DOI: 10.3969/j.issn.1672-9897.2000.02.007
  • Cited by

    Periodical cited type(4)

    1. 张璇,沈雪,田于逵,孙海浪,谢华,张楠. 平板边界层参数水槽测量与仿真分析研究. 实验流体力学. 2017(01): 26-31+46 . 本站查看
    2. 严宇超,姜澄宇,马炳和,薛晓晗,罗剑. 壁面剪应力标定方法研究综述. 实验流体力学. 2017(02): 20-25 . 本站查看
    3. 孙海浪,田于逵,金磊,张璇,谢华. MEMS热膜式壁面剪应力传感器微弱信号检测. 实验流体力学. 2017(02): 39-43 . 本站查看
    4. 田于逵,张璇,沈雪,孙海浪,谢华,张楠. 水下平板壁面剪应力MEMS测量研究进展. 实验流体力学. 2017(03): 82-87 . 本站查看

    Other cited types(5)

Catalog

    Article Metrics

    Article views (3437) PDF downloads (76) Cited by(9)
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return
    x Close Forever Close