摘要
结合高超声速远程滑翔飞行器在升阻比、容积率和容积等方面的性能需求,对锥导乘波构型底部基线方程的确定方法、构型顶点至基本流场顶点的距离等问题进行研究;采用面元法计算分析了各外形控制变量对飞行器性能的影响规律;总结得出高超声速远程滑翔飞行器各外形设计变量确定的先后顺序及准则。
This paper addressed some problems during wave-rider designing,such as the determination of baseline equation for conic wave-rider,the distance between apex of the vehicle and the basic field,with the consideration of lift-drag ratio,plot ratio and volume for hypersonic glide vehicle（HGV）.The effects of control variables of each configuration on the performance of HGV are analyzed by the method of surface element and the sequence and rules to confirm the design variables for HGV are summarized.
出处
《导弹与航天运载技术》
北大核心
2011年第3期1-5,共5页
Missiles and Space Vehicles
关键词
高超声速飞行器
锥导乘波构型
升阻比
容积率
Hypersonic Vehicle
Conic Derived Wave-rider
Lift-to-drag ratio
Plot ratio
