摘要
为提高飞行器性能和设计效率,降低设计盲目性和性能冗余度,对高升力、面对称高超声速飞行器气动布局、稳定性和与之相关的飞行控制三者之间的关系进行了论述,最后提出了一种引入稳定性和飞行控制因素的再入飞行器气动布局一体化设计概念,以满足高性能高超声速飞行器气动布局设计需求.
For improving the performance and design efficiency,and decreasing design blindness and performance redundancy,the relationship among aerodynamic configuration,stability and flight control is discussed,and the object is the high lift hypersonic vehicle.An integrated design concept incorporating configuration,stability and flight control is presented to meet the aerodynamic configuration design requirements of the high performance hypersonic vehicle.
出处
《战术导弹技术》
2011年第2期11-14,共4页
Tactical Missile Technology
关键词
高超声速
气动布局
稳定性
飞行控制
hypersonic
aerodynamic configuration
stability
flight control
