Volume 29 Issue 11
Nov.  2014
Turn off MathJax
Article Contents
WANG Kun, BAI Jun-qiang, XIA Lu, LI Xin, MA Xian-wei. Numerical simulation of aircraft hot air anti-icing system and ice ridge prediction[J]. Journal of Aerospace Power, 2014, 29(11): 2694-2703. doi: 10.13224/j.cnki.jasp.2014.11.021
Citation: WANG Kun, BAI Jun-qiang, XIA Lu, LI Xin, MA Xian-wei. Numerical simulation of aircraft hot air anti-icing system and ice ridge prediction[J]. Journal of Aerospace Power, 2014, 29(11): 2694-2703. doi: 10.13224/j.cnki.jasp.2014.11.021

Numerical simulation of aircraft hot air anti-icing system and ice ridge prediction

doi: 10.13224/j.cnki.jasp.2014.11.021
  • Received Date: 2013-07-12
  • Publish Date: 2014-11-28
  • A numerical simulation method was built based on the conception of fluid-solid coupled heat transfer, and ice prediction under hot air anti-icing system was carried out in associated with ice accretion thermodynamics model. Both the internal and external flow fields were got by solving N-S equation using cell-centered finite volume method. The droplet impingement result was calculated by Euler method based on the external flow field. Three-dimensional heat transfer partial differential equation was solved to get the heat transfer characteristic of the thin-gauge skin. Heat transfer from internal flow to external flow field was accomplished by using interface interpolation method. Three-dimensional ice accretion thermodynamics model was built with which ice ridge was predicted. The result shows that the heated wing surface temperature can get as high as 308 K, and ice ridge is accreted on both the upper and lower surfaces just after the heated zone when the hot air anti-icing system is on. Then, by analyzing the result, it proves that the method is rational and effective.

     

  • loading
  • [1]
    Bragg M B.Aerodynamics of supercooled-large-droplet ice accretion and the effect on aircraft in flight icing[R].DOT/FAA/AR-96/81,1996.
    [2]
    易贤.飞机积冰的数值计算与积冰试验相似准则研究[D].四川 绵阳:中国空气动力研究与发展中心,2007. YI Xian.Numerical computation of aircraft icing and study on icing test scaling law[D].Mianyang Sichuan:China Aerodynamics Research and Development Center,2007.(in Chinese)
    [3]
    Bragg M B.Aircraft aerodynamic effects due to large droplet ice accretions[R].AIAA-96-0932,1996.
    [4]
    Lee S,Bragg M B.Effects of simulated-spanwise ice shapes on airfoils:experimental investigation[R].AIAA-99-0092,1999.
    [5]
    裘燮纲,韩凤华.飞机防冰系统[M].北京:航空专业教材编审组,1985.
    [6]
    Pellissier M,Habashi W G.Optimization via FENSAP-ICE of aircraft hot-air anti-icing systems[J].Journal of Aircraft,2011,48(1):265-276.
    [7]
    HUA Jun,KONG Fanmei,Liu H H T.Unsteady thermodynamic computational computation fluid dynamics simulation of aircraft wing anti-icing operation[J].Journal of Aircraft,2007,44(4):1113-1117.
    [8]
    卜雪琴,郁嘉,林贵平.一种热气防冰系统的数值仿真[J].计算机仿真,2010,27(9):40-43. BU Xueqin,YU Jia,LIN Guiping.Numerical simulation of an airfoil hot-air anti-icing system[J].Computer Simulation,2010,27(9):40-43.(in Chinese)
    [9]
    Hannat R,Morency F.Numerical validation of CHT3D/CFX in anti-/de-icing piccolo system[R].AIAA-2012-2678,2012.
    [10]
    陶文铨.数值传热学[M].西安:西安交通大学出版社,2001.
    [11]
    Petrosino F,Mingione G,Carozza A.Ice accretion model on multi-element airfoil[J]. Jounal of Aircraft,2011,48(6):1913-1920.
    [12]
    张大林,陈维健.飞机机翼表面霜状冰结冰过程的数值模拟[J].航空动力学报,2004,19(1):137-141. ZHANG Dalin,CHEN Weijian.Numerical simulation of rime ice accretion process on airfoil[J].Journal of Aerospace Power,2004,19(1):137-141.(in Chinese)
    [13]
    Fortin G,Ilinca A,Laforte J L,et al.Prediction of 2D ice accretion by bisection method and by rivulets and beads modeling[R].AIAA-2003-1076,2003.
    [14]
    Messinger B L.Equilibrium temperature of an unheated icing surface as a function of airspeed[J].Journal of the Aeronautical Science,1953,20(1):29-42.
    [15]
    常士楠,苏心明,邱义芬.三维机翼结冰模拟[J].航空学报,2011,32(2):212-222. CHANG Shinan,SU Xinming,QIU Yifen.Ice accretion simulation on three dimensional wings[J]. Acta Aeronautica et Astronautica Sinica,2011,32(2):212-222.(in Chinese)
    [16]
    陈科,曹义华,安克文,等.复杂积冰翼型气动性能分析[J].航空动力学报,2007,22(6):986-990. CHEN Ke,CAO Yihua,AN Kewen,et al.Analysis on aerodynamic performance of complex iced airfoils[J].Journal of Aerospace Power,2007,22(6):986-990.(in Chinese)
    [17]
    易贤,桂业伟,朱国林.飞机三维结冰模型及其数值求解方法[J].航空学报,2010,31(11):2152-2158. YI Xian,GUI Yewei,ZHU Guolin.Numerical method of a three-dimensional ice accretion model of aircraft[J].Acta Aeronautica et Astronautica Sinica,2010,31(11):2152-2158.(in Chinese)
    [18]
    张强.飞行器机翼积冰的数值模拟[D].北京:北京航空航天大学,2009. ZHANG Qiang.Numerical simulation of ice accretions on aircraft wings[D].Beijing:Beijing University of Aeronautic and Astronautics,2009.(in Chinese)
    [19]
    Saeed F,Paraschivoiu I.Optimization of a hot-air anti-icing system[R].AIAA-2003-733,2003.
    [20]
    Planquart P.Vanden B G,Buchlin J M.Experimental and numerical optimization of a wing leading edge hot air anti-icing system[R].AIAA-2005-1277,2005.
    [21]
    Papadakis M,Wong S H,Yeong H W,et al.Icing tunnel experiments with a hot air anti-icing system[R].AIAA-2008-444,2008.
    [22]
    Santos L C,Domingos R H,Maria R B,et al.Sensitivity analysis of a bleed air anti-ice thermal model to geometrical and operational parameters[R].AIAA-2008-0445,2008.
  • 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 (1733) PDF downloads(962) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return