摘要
通过对普通翼面飞机和翼身融合飞机的气动隐身分析,得出翼身融合飞机升力系数提高、焦点前移、RCS值明显下降。文章在最后提出了合理的进一步改进措施。
An analysis of stealth performances for a canard-wing-tailplane configuration and a blended wing-fuselage configuration was conducted. The analysis results showed that the blended wing-fuselage configuration provides a higher lift coefficient, a forward shifted aerodynamic focus, and significandy low RCS. Finally, proposed modifications to the aerodynamic configurations were given.
出处
《飞机设计》
2006年第1期15-18,60,共5页
Aircraft Design
关键词
气动特性
隐身特性
翼身融合
aerodynamic characteristics
stealth performance
blended wing-fuselage configuration
