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某型温度传感器防冰结构防冰效果的仿真分析 被引量:2

Simulation and analysis of anti-icing effect of an anti-icing structure of temperature sensor
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摘要 基于计算液体动力学(CFD)计算仿真软件STAR-CCM+11.06,对某型温度传感器的防冰结构进行了防冰效果的数值模拟分析,获得防冰结构绕流流场,过冷水滴运动方式,防冰结构表面过冷水滴的收集情况、冰层增长情况及冰层形状。计算结果表明:来流马赫数Ma大于等于0.1的情况下,防冰结构能够实现较好的防冰效果,随着来流马赫数的减小,防冰效果变差;冰层持续增长会导致管路封冻,防冰结构不具备自我清洁的能力。 Numerical simulation and analysis on anti-icing effect of an anti-icing structure of temperature sensor is carried out,based on STAR-CCM + 11. 06,a computational fluid dynamics( CFD) computation and simulation software. Flow field around anti-icing structure,movement mode of overcooled water droplets,the over cooled water droplets collection of anti-icing structure surface and ice layer growth and shape of icing layer. The result shows that the anti-icing structure can get good effect when the mach number Ma is above 0. 1,and the effect will get worse for lower mach number; sustainable growth will cause pipe freezing,anti-icing structure not having the ability of self-cleaning.
作者 张进 姜志恒 李瑜 温铁钝 ZHANG Jin;JIANG Zhi-heng;LI Yu;WEN Tie-dun(Sensing System Engineering Department,Aero Engine Control System Institute,Wuxi 214063,China)
出处 《传感器与微系统》 CSCD 2018年第10期54-56,59,共4页 Transducer and Microsystem Technologies
关键词 计算流体动力学 防冰结构 绕流流场 过冷水滴 冰层增长 computational fluid dynamics (CFD) anti-icing structure flow field around overcooled water droplets ice accretion
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  • 1赵鸿铎,姚祖康,张长安,刘春晨.飞机除冰液对停机坪水泥混凝土的影响[J].交通运输工程学报,2004,4(2):1-5. 被引量:15
  • 2蒋胜矩,李凤蔚.基于N-S方程的翼型结冰数值模拟[J].西北工业大学学报,2004,22(5):559-562. 被引量:23
  • 3陈维建,张大林.飞机机翼结冰过程的数值模拟[J].航空动力学报,2005,20(6):1010-1017. 被引量:25
  • 4常士楠,刘达经,袁修干.直升机旋翼桨叶防/除冰系统防护范围研究[J].航空动力学报,2007,22(3):360-364. 被引量:10
  • 5James J Chung, Harold E Addy, Jr. A numerical evaluation of icing effects on a natural laminar flow airfoil [ R ]. AIAA - 2000 - 0096,2000.
  • 6X Chi,B Zhu,T I-P Shih,et al. CFD analysis of the aerodynamics of a business- jet airfoil with leading- edge ice accretion [ R ]. AIAA - 2004 - 0560,2004.
  • 7Messinger B. Equilibrium temperature of an unheated icing surface as a function of air speed [ J ]. Journal of Aeron Sciences, 1953,20( 1 ).
  • 8Mark G. Potapczuk, Kamel M. Al- Khalil, Matthew T. Velazquez. Ice accretion and performance degradation calculations with LEWICE/NS [ R ]. AIAA - 93 - 0173,1993.
  • 9Harold E. Addy, Jr. Ice accretions and icing effects for modern airfoils [ R ]. NASA/TP - 2000 - 210031,2000.
  • 10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..

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