Volume 37 Issue 1
Jan.  2022
Turn off MathJax
Article Contents
Article Navigation >  Journal of Aerospace Power  > 2022  >  37(1): 142-151
WANG Qimin, ZHENG Longqian, ZHANG Meihong. Influence of outboard nacelle chine on the low-speed characteristics of civil transport aircraft[J]. Journal of Aerospace Power, 2022, 37(1): 142-151. doi: 10.13224/j.cnki.jasp.20210333
Citation: WANG Qimin, ZHENG Longqian, ZHANG Meihong. Influence of outboard nacelle chine on the low-speed characteristics of civil transport aircraft[J]. Journal of Aerospace Power, 2022, 37(1): 142-151. doi: 10.13224/j.cnki.jasp.20210333
shu

Influence of outboard nacelle chine on the low-speed characteristics of civil transport aircraft

doi: 10.13224/j.cnki.jasp.20210333

  • Shanghai Aircraft Design and Research Institute， Commercial Aircraft Corporation of China，Limited，Shanghai 201210，China

  • Received Date: 2021-06-28
  • Publish Date: 2022-01-28
    Abstract
  • For the purpose of improving the aerodynamic performance of the civil transport aircraft with the high-lift devices deployed at high angle of attack，the numerical simulation method of Reynolds average Navier-Stokes （RANS） turbulence model was used to analyze the stall characteristics of aircraft with the wing-mounted nacelle configuration.The mechanism of the outboard nacelle chine was investigated.Design exploration of the installation position and angle of the outboard nacelle chine was carried out.The vortex from the outboard slat and main wing aggravated the flow separation on the wing upper surface behind the nacelle/pylon.The vortex induced by designed outboard nacelle chine suppressed the flow separation，which increased the maximum lift coefficient.The installation position of the outboard nacelle chine affected the intensity，spanwise position and height of the induced vortex.The installation angle mainly affected the induced vortex intensity.The maximum lift coefficient increased by 2.1% with the outboard nacelle chine.

     

    • FullText(HTML)
  • loading
    • References(19)
  • [1]
    陈迎春，张美红，张淼，等.大型客机气动设计综述[J].航空学报，2019，40（1）：30-46.
    [2]
    RUDOLPH P K C.High-lift systems on commercial subsonic airliners[R].AIAA-2009-2128,2009.
    [3]
    张冬云，张美红，王美黎，等.翼吊布局民机短舱位置气动影响[J].空气动力学学报，2017,35（6）：781-786.
    [4]
    白俊强，刘南，邱亚松，等.民用运输机短舱涡流片设计研究[J].空气动力学学报,2014,32（2）：190-196.
    [5]
    张文升，陈海昕，张宇飞，等.短舱扰流片对运输机增升装置气动特性的影响[J].航空学报,2013,34（1）:76-85.
    [6]
    ELIASSON P,CATALANO P,PAPE L M C,et al.Improved CFD predictions for high lift flows in the European project EUROLIFT Ⅱ[R].AIAA 2007-4303,2007.
    [7]
    GRYR H F,SCHADE N,BURG J W V D,et al.CFD prediction of maximum lift effects on realistic high-lift-commercial-aircraft-configurations within the European project EUROLIFT Ⅱ[R].AIAA-2007-4299,2007.
    [8]
    QUIX H,SCHULZ M,QUEST J,et al.Low speed high lift validation tests within the European project EUROLIFT Ⅱ[R].AIAA-2007-4298,2007.
    [9]
    KATO H,WATANABE S,MURAYAMA M,et al.PIV investigation of nacelle chine effects on high-lift system performance [R].AIAA-2008-240,2008.
    [10]
    KOKLU M,LIN J C,HANNON J A,et al.Mitigation of nacelle/pylon wake on the high-lift common research model using a nacelle chine[R].AIAA-2020-0786,2020.
    [11]
    白俊强，刘南，邱亚松，等.大型民用运输机短舱涡流片增升效率以及参数影响研究[J].西北工业大学学报,2013,31（3）:522-529.
    [12]
    KANAZAKI M,YOKOKAWA Y,MURAYAMA M,et al.Efficient design exploration of nacelle chine installation in wind tunnel testing [R].AIAA-2008-155,2008.
    [13]
    KANAZAKI M,YOKOKAWA Y,MURAYAMA M,et al.Nacelle chine installation based on wind-tunnel test using efficient global optimization[J].Transactions of the Japan Society for Aeronautical and Space Sciences,2008,51（173）:146-150.
    [14]
    邱亚松，白俊强，黄琳，等.翼吊发动机短舱对三维增升装置的影响及改善措施研究[J].空气动力学学报,2012,30（1）:7-13.
    [15]
    钟园，杨小权，刘凯礼，等.民用飞机低速俯仰力矩特性改善研究[J].空气动力学学报,2019,37（4）:569-577.
    [16]
    邱亚松，白俊强，李亚林，等.复杂几何细节对增升装置气动性能影响研究[J].航空学报,2012,33（3）:421-429.
    [17]
    RUMSEY C L,SLOTNICK J P,LONG M,et al.Summary of the first AIAA CFD high-lift prediction workshop[R].Journal of Aircraft,2011,48（6）:2068-2079.
    [18]
    YOKOKAWA Y,MURAYAMA M,ITO T,et al.Experiment and CFD of a high-lift configuration civil transport aircraft model[R].AIAA-2006-3452,2006.
    [19]
    刘凯礼,孙一峰,钟园，等.民用飞机进气道的侧风畸变研究[J].航空动力学报,2015,30（2）:289-296.
    • Relative Articles
    • Supplements(0)
    • Cited By
  • 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
    Get Citation
    PDF(2427.0KB)
    XML

    Article Metrics

    Article views (356) PDF downloads(68) Cited by()
    Proportional views
    Related

    Copyright © 《Journal of Aerospace Power》 All Rights Reserved.

    Supported by: Beijing Renhe Information Technology Co., Ltd.  

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return