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飞机结冰风洞试验模拟研究
引用本文:范洁川,于涛.飞机结冰风洞试验模拟研究[J].实验流体力学,2007,21(1):68-72,92.
作者姓名:范洁川  于涛
作者单位:中国航空工业空气动力研究院,黑龙江,哈尔滨,150001
摘    要:论述了飞机结冰风洞试验的必要性;阐述了结冰风洞试验方法;给出了相似准则和模拟参数计算结果及分析;讨论了飞行高度和大尺度水滴模拟问题.

关 键 词:飞机结冰  结冰风洞  结冰试验  模拟参数
文章编号:1672-9897(2007)01-0068-06
收稿时间:2005-01-27
修稿时间:2005-01-272005-05-09

A study of simulation for airplane icing tests in icing wind tunnel
FAN Jie-chuan,YU Tao.A study of simulation for airplane icing tests in icing wind tunnel[J].Experiments and Measur in Fluid Mechanics,2007,21(1):68-72,92.
Authors:FAN Jie-chuan  YU Tao
Institution:Chinese Aerodynamic Research Institute of Aeronautics, Harbin 150001, China
Abstract:In this paper,the necessity of airplane icing tests has been discussed.The testing method in icing wind tunnel has been explained.And the similarity criterion and its computing results as well as analysis have been given.The simulations of flight altitude and super large droplet diameter have been discussed.
Keywords:airplane ice up  icing wind tunnel  icing test  similarity parameters
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