火力与指挥控制2011，Vol.36Issue(2)：112-114,3.
高超声速巡航飞行器纵向气动特性分析
Longitudinal Aerodynamic Characteristics Analysis of Hypersonic Cruise Vehicle
邢永刚 1唐硕1
作者信息
- 1. 西北工业大学航天学院,西安,710072
- 折叠
摘要
Abstract
The airframe integrated nature of the scramjet engine with airbreathing hypersonic cruise vehicle (HCV) results in a strong couplings between aerodynamics and propulsive system. The couplings have an effect on vehicle aerodynamic performance, stability and control. Aiming at the effects, the model of airframe integrated scramjet engine has been developed and aero-propulsion interface separated. Based on the forgoing work,longitudinal aerodynamic characteristics of HCV inlet open, scramjet engine powered and unpowered have been computed separately. Simulation reveals the couplings between aerodynamics and propulsive system and the effect on vehicle characteristics.关键词
高超声速巡航飞行器/气动-推进界面/气动特性Key words
hypersonic cruise vehicle /aero-propulsion interface /aerodynamic characteristics分类
航空航天引用本文复制引用
邢永刚,唐硕..高超声速巡航飞行器纵向气动特性分析[J].火力与指挥控制,2011,36(2):112-114,3.
