实验流体力学2011，Vol.25Issue(3)：1-5,5.
低速大迎角张线尾撑系统支架干扰影响研究
Study on the support interference of wire-assistant sting support at high angle of attack in low speed wind tunnel
祝明红 1孙海生 1金玲 2汤伟 2刘志涛2
作者信息
- 1. 西北工业大学航空学院,西安710072
- 2. 中国空气动力研究与发展中心,四川绵阳621000
- 折叠
摘要
Abstract
In order to improve test data accuracy and acquire support interference characteristics, the test study on the support interference of wire-assistant sting support setting in Φ3.2m low speed wind tunnel is introduced. It is shown that, the impact of the beam of wire-assistant sting support on longitudinal aerodynamics characteristics of aircraft is small, and the stinghas great effect on longitudinal aerodynamics characteristics at high angle of attack. The yawing moment coefficients decrease and rolling moment coefficients increase at angle of attack from 0°to 15°with the existence of wire-assistant sting support. With the increase of side slip angle, the interference become bigger; without the vertical tail, the effect of the wire-assistant sting support on the pitching moment becomes small evidently.关键词
大迎角/张线尾撑/支架干扰/尾支杆/风洞实验Key words
Key words: high angles of attack/ wire-assistant sting support/ support interference/ sting/wind tunnel test分类
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祝明红,孙海生,金玲,汤伟,刘志涛..低速大迎角张线尾撑系统支架干扰影响研究[J].实验流体力学,2011,25(3):1-5,5.
