Volume 34 Issue 12
Dec.  2019
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XIAO Chunhua, LIN We, YANG Shengke. Preliminary study on influence of icing cloud parameters on ice shear strength on solid wall[J]. Journal of Aerospace Power, 2019, 34(12): 2627-2634. doi: 10.13224/j.cnki.jasp.2019.12.011
Citation: XIAO Chunhua, LIN We, YANG Shengke. Preliminary study on influence of icing cloud parameters on ice shear strength on solid wall[J]. Journal of Aerospace Power, 2019, 34(12): 2627-2634. doi: 10.13224/j.cnki.jasp.2019.12.011

Preliminary study on influence of icing cloud parameters on ice shear strength on solid wall

doi: 10.13224/j.cnki.jasp.2019.12.011
  • Received Date: 2019-05-29
  • Publish Date: 2019-12-28
  • The ice shear strength test equipment was established in the test section of icing wind tunnel, and used to measure the shear strength between ice and solid wall of airplane. The reasonable range of ice shear strength was obtained. The ice shear strength measurement was implemented in test section of 0.3 m×0.2 m icing wind tunnel. The influences of icing cloud parameters on the ice shear strength between ice and solid wall were obtained. Research showed that the maximum value of ice shear strength appeared when the icing environmental temperature was between -15 ℃ and -10 ℃. The higher airflow speed indicated the larger impact force of droplets on solid wall. The gap among droplets was easier to be filled in. Thus, the ice shear strength was increased. The minimum value of ice shear strength happened when the mean volume diameter (MVD) of droplets was near 35 μm. The ice became compact and the gap among droplets was smaller along with the decrease of MVD. And the droplets easily spread out and were difficult to be frozen immediately. The ice shear strength increased due to the filling of gap among droplets.

     

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  • [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]
    LYNCH F T,KHODADOUST A.Effects of ice accretions on aircraft aerodynamics[J].Progress in Aerospace Sciences,2001,37(8):669-767.
    [3]
    KEVIN R P,CAROL D J.A statistical review of aviation airframe icing accidents in the U.S.[R].Washington DC:National Transportation Safety Board,2004.
    [4]
    BRAGG M B,BROEREN A P,BLUMENTHAL LA.Iced-airfoil aerodynamics[J].Progress in Aerospace Sciences,2005,41(5):323-362.
    [5]
    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)
    [6]
    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)
    [7]
    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)
    [8]
    JELLINEK H G.The influence of imperfections on the strength of ice[J].Journal of Applied Physics,1958,27(10):1198-1209.
    [9]
    REICH A D,SCAVUZZO R J,CHU M L.Survey of mechanical properties of impact ice[R].AIAA 94-0712,1994.
    [10]
    SCAVUZZO R J,CHU M L.Structural properties of impact ices accreted on aircraft structures[R].NASA Contractor Report 179580,1987.
    [11]
    SCAVUZZO R J,CHU M L,Ananthaswamy V.Influence of aerodynamic forces in ice shedding[J].Journal of Aircraft,1994,31(3):526-530.
    [12]
    STALLABRASS J R,PRICE R D.On the adhesion of ice to various materials[R].National Research Council,NRC No.6980,1963.
    [13]
    PHAN C L,MCCOMBER P,MANSIANX A.Adhesion of rime and glaze on conductors protected by various materials[J].Transactions of the Canadian Society for Mechanical Engineering (CSME),1976,4(4):204-208.
    [14]
    DRUEZ J,PHAN C L,LAFORTE J L,et al.The adhesion of glaze and rime on aluminum electric conductors[J].Transactions of the Canadian Society for Mechanical Engineering (CSME),1979,5(4):215-220.
    [15]
    REICH A D.Comparison of rime and glaze deformation and failure properties[R].AIAA 91-0446,1991.
    [16]
    ANDERSON D N,REICH A D.Tests of the performance of coating for low ice adhesion[R].AIAA 97-0303,1997.
    [17]
    肖春华,程尧,乔宝英,等.并列双方柱的疏水涂层防冰效果结冰风洞实验评估[J].航空动力学报,2018,33(3):540-548. XIAO Chunhua,CHENG Yao,QIAO Baoying,et al.Icing wind tunnel test evaluation on anti-icing effects of hydrophobic coating on two parallelized square cylinders[J].Journal of Aerospace Power,2018,33(3):540-548.(in Chinese)
    [18]
    VARGAS M,BROUGHTON H,SIMS J J,et al.Local and total density measurements in ice shapes[R].AIAA-2005-657,2005.
    [19]
    LIBBRECHT K G.The physics of snow crystals[J].Reports on Progress in Physics,2005,68(4):855-895.
    [20]
    HOBBS P V.Ice physics[M].Oxford:Oxford University Press,1974.
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