Improvement study on aerodynamic characteristics of a fighter configuration with strake-wing

被引：0
|
作者：
Lu, Zhi-Yong [1 ]
Gao, Wei-Ming [1 ]
机构：
[1] Inst. of Fluid Mech., Beijing Univ. of Aero. and Astron., Beijing 100083, China
来源：
Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica | 2002年 / 23卷 / 02期
关键词：
Experiments - Lift - Stability - Wind tunnels;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
An experimental study of the effects of the twin vertical fins position and twist strake wing on a fighter aerodynamic characteristics was performed in the wind tunnel. The result shows that the twist strake wing is able to increase the maximum lift coefficient and incidence range of yawing stability. However, it has no effect on rolling stability. When twin vertical fins are located at the wing surface the maximum lift coefficient could be increased obviously and the incidence range of yawing and rolling stability is extended.
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收藏
页码：170 / 172
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