微型飞行器优化设计及气动特性分析  

Optimium Design of Micro Air Vehicle and Its Aerodynamics Analysis

作　　者：何烈堂[1] 曾庆华[1] 

机构地区：[1]国防科技大学航天与材料工程学院,湖南长沙410073

出　　处：《飞行力学》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 )

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.

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 

分 类 号：V212.1[航空宇航科学与技术—航空宇航推进理论与工程]