摘要
微型飞行器 (MAV)气动布局形式是影响其飞行性能指标的关键因素之一。从总体角度出发 ,设计出三种不同气动布局的 MAV,并对其进行了优化设计和气动特性分析。研究结果对 MAV气动布局的设计有一定的指导意义。
The aerodynamic configuration is important to the flight performance of a micro air vehicle(MAV). From the way of comprehensive design, three varied configurations of MAV were designed and optimized in this paper, then their aerodynamic properties were compared and analyzed. Some data and conclusions drew have guidance significance for the design of aerodynamic configuration of MAV.
出处
《飞行力学》
CSCD
2003年第2期31-33,48,共4页
Flight Dynamics
基金
国家自然科学基金资助项目 (6 0 1 75 0 32 )
关键词
微型飞行器
优化设计
气动特性
气动布局
飞行性能
升阻比
操纵性
micro air vehicle
aerodynamic configuration
lift drag ratio
controllability
static stability margin
