| 一种低RCS无人飞行器外形的气动特性实验研究 |
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| 引用本文： | 戴全辉,昂海松.一种低RCS无人飞行器外形的气动特性实验研究[J].宇航学报,2002,23(1):60-63. |
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| 作者姓名： | 戴全辉 昂海松 |
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| 作者单位： | 南京航空航天大学,南京,210016 |
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| 摘 要： | 根据气动布局的基本原理,结合低RCS要求,设计了一种鸭式布局、带边条的翼身融合无人飞行器外形,实验结果表明,该外形不仅具有低RCS特征,而且具有良好的气动特性,升阻比达到8左右。
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| 关 键 词： | 无人飞行器 融合外形 气动特性实验 侧向雷达截面 RCS 隐身技术 设计 |
| 文章编号： | 1000-1328(2002)01-0060-04 |
| 修稿时间： | 2001年3月12日 |
Experimental research on the aerodynamic characteristics of a low RCS configuration of UAV |
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| DAI Quan hui,ANG Hai song.Experimental research on the aerodynamic characteristics of a low RCS configuration of UAV[J].Journal of Astronautics,2002,23(1):60-63. |
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| Authors: | DAI Quan hui ANG Hai song |
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| Abstract: | A "canard" configuration with blended fuselage and fringe of unmanned aerial vehicle(UAV)is designed according to the basic theory of aerodynamic layout and the low RCS demand and its aerodynamic characteristics test has been carried out.It is shown that the configuration has good aerodynamic characteristics as well as low Radar Cross Section,and the ratio of lift over drag is about 8. |
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| Keywords: | Unmanned aerial vehicle(UAV) Blending configuration Aerodynamic characteristics |
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