摘要
飞翼布局(FLYING-WING)作为一种非常规气动布局,有着传统气动布局无可比拟的优势,因此成为未来飞行器理想气动布局之一。对飞翼布局的气动特性进行了分析,提出了飞翼布局飞机的气动设计要点,并利用算例对这些设计要点进行了验证,结果表明该设计思路具有一定的可行性。
The flying-wing configuration has becoming one of the ideal aerodynamic configurations for the future aircraft because of its excellent performance. The features of this configuration are analyzed, the shape of an UAV is designed and the essentials while designing are summarized.
出处
《科学技术与工程》
2009年第12期3570-3573,共4页
Science Technology and Engineering
关键词
飞翼
气动设计
欧拉方程
flying-wing configuration aerodynamic design Euler equation
