| 微型飞行器优化设计及气动特性分析 |
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| 引用本文： | 何烈堂,曾庆华.微型飞行器优化设计及气动特性分析[J].飞行力学,2003,21(2):31-33,48. |
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| 作者姓名： | 何烈堂 曾庆华 |
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| 作者单位： | 国防科技大学,航天与材料工程学院,湖南,长沙,410073 |
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| 基金项目： | 国家自然科学基金资助项目 (6 0 1 75 0 32 ) |
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| 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。
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| 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 |
| 文章编号： | 1002-0853(2003)02-0031-03 |
Optimium Design of Micro Air Vehicle and It's Aerodynamics Analysis |
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| HE Lie tang,ZENG Qing hua.Optimium Design of Micro Air Vehicle and It''s Aerodynamics Analysis[J].Flight Dynamics,2003,21(2):31-33,48. |
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| Authors: | HE Lie tang ZENG Qing hua |
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| Abstract: | 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. |
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| Keywords: | micro air vehicle aerodynamic configuration lift drag ratio controllability static stability margin |
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