摘要
本文对后掠角为 80°的尖前缘平板三角翼的翼摇滚特性进行了实验研究 ,并与附加前体。
An wind tunnel experimental investigation of wing rock behavior of a slender delta wing was performed. A sharp leading edge, flat plate, delta wing having a sweep angle of 80° was used in this study. The result was compared with several layout which was added forbody or/and vertical tail. In addi tion, Investigation was conducted on the relation between wing rock behavior and roll static stability about several layout.
出处
《空气动力学学报》
EI
CSCD
北大核心
2000年第1期111-114,共4页
Acta Aerodynamica Sinica
关键词
细长机翼
大迎角
非定常流动
摇滚特性
slender wing
large angle of attack
unsteady flow
wing rock behavior
