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飞机机翼结冰计算方法与风洞试验研究概况
引用本文:罗谨,赵兰萍,杨志刚. 飞机机翼结冰计算方法与风洞试验研究概况[J]. 航空计测技术, 2011, 31(1): 50-53,60
作者姓名:罗谨  赵兰萍  杨志刚
作者单位:罗谨,LUO Jin(同济大学机械工程学院,上海,201804);赵兰萍,ZHAO Lanping(同济大学机械工程学院,上海,201804;上海地面交通工具风洞中心,上海,201804);杨志刚,YANG Zhigang(上海地面交通工具风洞中心,上海,201804)
摘    要:介绍了飞机结冰的数值计算方法,包括绕流流场计算、过冷水滴轨迹方程计算和结冰量计算,并给出冰层增长的两种模型;针对结冰风洞试验,指出液滴粒径和液态水含量的测量是试验的难点和重点,并总结上述两个结冰参数的测量方法;给出两种常规结冰缩比方法,并简单介绍混合缩比模型的设计方法。

关 键 词:飞机结冰  数值模拟  测量方法  缩比方法

General Situation of Calculation Method of Ice Accretion on Airfoil
LUO Jin,ZHAO Lanping,,YANG Zhigang. General Situation of Calculation Method of Ice Accretion on Airfoil[J]. Aviation Metrology & Measurement Technology, 2011, 31(1): 50-53,60
Authors:LUO Jin  ZHAO Lanping    YANG Zhigang
Affiliation:LUO Jin1,ZHAO Lanping1,2,YANG Zhigang2(1.Mechanical Engineering College,Tongji University,Shanghai 201804,China,2.Shanghai Ground Transport Wind Tunnel Center,China)
Abstract:The paper introduces numerical methods for calculation of aircraft icing,including the flow field calculation,equation of supercooled water droplets and icy volume calculation,and presents two models of ice growth.For wind tunnel tests,measurements of droplet diameter and liquid water content are difficult and important.Measurement methods of the two icing parameters mentioned above are summed up.Two conventional icing scaling methods are given,and the design of mixed scaling model is brifely introduced.
Keywords:aircraft icing  numerical simulation  measurement  scaling method  
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