The influence on flow structure and aerodynamic of a slender by sweep wing at highAngleofattack was studied.
研究了在大迎角下,后掠翼对细长体绕流结构和气动力特性的影响。
2
The extended linearization of nonlinear systems is used to design flight control systems at highangleofattack.
利用非线性系统的扩展线性化方法设计具有大迎角的非线性飞行控制系统。
3
Dynamic aerodynamics characteristic is one of very important parameters of modern maneuverable aircraft to be scaled at highAngleofattack and high speed.