南京航空航天大学学报2011，Vol.43Issue(2)：252-256,5.
可变形乘波体气动推进与控制一体化综合设计
Integrated Design on Aerodynamic, Propulsion and Control for Deformable Waverider
摘要
Abstract
Waverider is considered as the main configuration for hypersonic vehicle. If it is designed as a morphing body, the flight envelope can be effectively expanded, and the global stability performance can be ensured. Hence, the integrated design of deformable waverider is researched. Firstly, based on the given referenced waverider shape, the aerodynamics force and thrust are calculated according to the hypersonic aerodynamic theory and the Rayleigh flow formula, and the vehicle model is established. Then the constraint condition of multistage compression is given for the deformable forebody of the vehicle. Furthermore, the coordinated changing relationships among aerodynamic, propulsion and actuator control are discussed. Finally, by simulation,design parameters are obtained for the deformable waverider, and the feasibility of the integrated design is validated.关键词
乘波体/高超声速飞行/变形体/复杂建模/综合设计Key words
waverider/ hypersonic flight/ the deformable body/ complex modeling/ integrated design分类
航空航天引用本文复制引用
刘燕斌,张勇,陆宇平..可变形乘波体气动推进与控制一体化综合设计[J].南京航空航天大学学报,2011,43(2):252-256,5.基金项目
高等学校博士学科点专项科研(20093218120035)资助项目 （20093218120035）
南京航空航天大学基本科研业务费专项科研(NS2010213)资助项目 （NS2010213）
航空科学基金联合(2008ZA52010)资助项目. （2008ZA52010）
