Volume 34 Issue 12
Dec.  2019
Turn off MathJax
Article Contents
XIAO Chunhua, GUI Yewei, YANG Shengke. Ice fracture criterion coupled thermal/mechanical effect based on stress analysis[J]. Journal of Aerospace Power, 2019, 34(12): 2616-2626. doi: 10.13224/j.cnki.jasp.2019.12.010
Citation: XIAO Chunhua, GUI Yewei, YANG Shengke. Ice fracture criterion coupled thermal/mechanical effect based on stress analysis[J]. Journal of Aerospace Power, 2019, 34(12): 2616-2626. doi: 10.13224/j.cnki.jasp.2019.12.010

Ice fracture criterion coupled thermal/mechanical effect based on stress analysis

doi: 10.13224/j.cnki.jasp.2019.12.010
  • Received Date: 2019-05-06
  • Publish Date: 2019-12-28
  • Considering the effect of the external aerodynamic force and skin heating, the computational model of stress inside ice on the leading edge of NACA 0012 airfoil was established according to the thermal de-icing physical process. The finite element method and triangular element were employed to solve the governing equations. The effects of external aerodynamic force and skin heating on the ice adhesion interface stress were obtained. The study showed that, without skin heating, the variation of airflow speed changed the intensity of interfacial stress of ice adhesion interface and the variation of angle of attack changed the distribution of interfacial stress of ice adhesion interface. An approximate linear increasing trend for maximum interfacial shear stress existed along with the increasing airflow speed. But external aerodynamic force contributed little to ice fracture. For skin heating, the coupled stress of ice adhesion interface and principal stress inside ice increased along with the increase of heat flow rate, which can be easily larger than the shear strength of adhesion interface and key factor for ice fracture. The preliminary ice fracture judgement criterion was founded based on the relationship between interfacial stress and adhesion strength related with interfacial temperature. Ice fracture appears when the sum of the interfacial stress generated by the external aerodynamic force and the interfacial thermal stress generated by the skin heating are greater than the shear strength related to the skin surface temperature. The fracture location is the area where the coupled stress exceeds the shear strength.

     

  • loading
  • [1]
    KIND R J,POTAPCZUK M G,FEO A,et al.Experimental and computational simulation of in-flight icing phenomena[J].Progress in Aerospace Sciences,1998,34(5/6):275-345.
    [2]
    KEVIN R P,CAROL D J.A statistical review of aviation airframe icing accidents in the US[R].Washington DC:National Transportation Safety Board,2004.
    [3]
    LYNCH F T,KHODADOUST A.Effects of ice accretions on aircraft aerodynamics[J].Progress in Aerospace Sciences,2001,37(8):669-767.
    [4]
    BRAGG M B,BROEREN A P,BLUMENTHAL L A.Iced-airfoil aerodynamics[J].Progress in Aerospace Sciences,2005,41(5):323-362.
    [5]
    肖春华,桂业伟,易贤,等.结冰翼型表面明冰的压力分布和应力计算[J].航空动力学报,2009,24(7):1457-1463. XIAO Chunhua,GUI Yewei,YI Xian,et al.Pressure distribution and stress calculation of glaze ice on iced airfoil[J].Journal of Aerospace Power,2009,24(7):1457-1463.(in Chinese)
    [6]
    李清英,朱春玲,白天.电脉冲除冰系统的除冰实验与数值模拟[J].航空动力学报,2012,27(2):350-356. LI Qingying,ZHU Chunling,BAI Tian.De-icing experiment and numerical simulation of the electro-impulse de-icing system[J].Journal of Aerospace Power,2012,27(2):350-356.(in Chinese)
    [7]
    SOLTIS J,PALACIOS J,EDEN T,et al.Ice adhesion mechanisms of erosion-resistant coatings[J].AIAA Journal,2015,53(3):1-9.
    [8]
    SOLTIS J,PALACIOS J,WOLFE D E,et al.Evaluation of ice adhesion strength on erosion resistant materials[R].AIAA-2013-1509,2013.
    [9]
    肖春华,林贵平,桂业伟,等.电热除冰的热力耦合特性及其对冰层的影响研究[J].实验流体力学,2012,26(2):23-28. XIAO Chunhua,LIN Guiping,GUI Yewei,et al.Study on coupled thermo-mechanical characteristics and its effects during the process of electrothermal deicing[J].Journal of Experiments in Fluid Mechanics,2012,26(2):23-28.(in Chinese)
    [10]
    LEFFEL K L.A numerical and experimental investigation of electrothermal aircraft deicing[D].Toledo,Ohio:The University of Toledo,1986.
    [11]
    KEITH T G,DEWITT K J,MASIULANIEC K C,et al.Predicted electrothermal deicing of aircraft blades[R].AIAA 84-0110,1984.
    [12]
    常士楠,艾素霄,霍西恒,等.改进的电热除冰系统仿真[J].航空动力学报,2008,23(10):1753-1758. CHANG Shinan,AI Suxiao,HUO Xiheng,et al.Improved simulation of electrothermal de-icing system[J].Journal of Aerospace Power,2008,23(10):1753-1758.(in Chinese)
    [13]
    SAEED F,PARASCHIVOIU I.Optimization of a hot-air anti-icing system[R].AIAA-2003-733,2003.
    [14]
    PAPADAKIS M,WONG S H,YEONG H W,et al.Icing tunnel experimental with a hot air anti-icing system[R].AIAA-2008-444,2008.
    [15]
    卜雪琴,林贵平,郁嘉.三维内外热耦合计算热气防冰系统表面温度[J].航空动力学报,2009,24(11):2495-2500. BU Xueqin,LIN Guiping,YU Jia.Three-dimensional conjugate heat transfer simulation for the surface temperature of wing hot-air anti-icing system[J].Journal of Aerospace Power,2009,24(11):2495-2500.(in Chinese)
    [16]
    SCAVUZZO R J,CHU M L,ANANTHASWAMY V.Influence of aerodynamic forces in ice shedding[J].Journal of Aircraft,1994,31(3):526-530.
    [17]
    SCAVUZZO R J,CHU M L.Structural properties of impact ices accreted on aircraft structures[R].NASA Contractor Report 179580,1987.
    [18]
    WRIGHT W B,DEWITT K J,KEITH T G,Jr.Numerical simulation of icing,deicing,and shedding[R].AIAA 91-0655,1991.
    [19]
    肖春华,林贵平,桂业伟,等.冰脱落对电热除冰传热特性的影响研究[J].空气动力学学报,2012,30(4):551-556. XIAO Chunhua,LIN Guiping,GUI Yewei,et al.Study on effect of ice shedding on heat transfer characteristics of electrothermal aircraft deicing[J].Acta Aerodynamica Sinica,2012,30(4):551-556.(in Chinese)
    [20]
    YASLIK A D,DEWITT K J,KEITH T G.Further developments in three-dimensional numerical simulation of electrothermal deicing systems[R].AIAA 92-0528,1992.
    [21]
    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.
    [22]
    HENRY R.Development of an electrothermal de-icing/anti-icing model[R].AIAA 92-0526,1992.
    [23]
    THWAITES B.Incompressible aerodynamics[M].Oxford,UK:Clarendon Press,1960.
    [24]
    POTAPCZUK M G,BIDWELL C S.Numerical simulation of ice growth on a MS-317 swept wing geometry[R].AIAA 91-0263,1991.
    [25]
    王勖成,邵敏.有限单元法基本原理和数值方法[M].北京:清华大学出版社,1997.
    [26]
    孔祥谦.热应力有限单元法分析[M].上海:上海交通大学出版社,1999.
  • 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 (593) PDF downloads(309) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return