摘要
针对高空长航时无人机的设计要求和联翼布局在气动、结构、操稳特性等方面的特点,对联翼高空长航时无人机总体布局设计中的一些问题进行了总结和分析,在机翼、控制面、机身-进气道-发动机以及起落架布置等方面提供了设计思路,研究结果可用于相关方案的概念设计。
According to the design requirements of a high-altitude-long-endurance UAV and the aerodynamic, structure, maneuvrability and stability features of a joined-wing, some problems in the conceptual layout design of the Joined-Wing-HALE are summarized and analyzed. The design routes about the layout of wing, control surfaces, body-inlet-engine and landing gears are given. The research results are useful to the correlation conceptual layout design.
出处
《飞行力学》
CSCD
北大核心
2009年第4期1-4,共4页
Flight Dynamics
基金
国家863计划资助项目(2007AA705201)
关键词
联翼
高空长航时无人机
总体布局
一体化设计
joined-wing
high-altitude-long-endurance UAV
conceptual layout
integrated design
