| 某战斗机气动隐身分析与改型 |
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| 引用本文： | 邱菊,昂海松.某战斗机气动隐身分析与改型[J].飞机设计,2006(1):15-18,60. |
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| 作者姓名： | 邱菊 昂海松 |
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| 作者单位： | 1. 成都飞机工业(集团)公司,技术中心,四川,成都,610092
2. 南京航空航天大学,江苏,南京,210016 |
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| 摘 要： | 通过对普通翼面飞机和翼身融合飞机的气动隐身分析,得出翼身融合飞机升力系数提高、焦点前移、RCS值明显下降。文章在最后提出了合理的进一步改进措施。
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| 关 键 词： | 气动特性 隐身特性 翼身融合 |
| 文章编号： | 1673-4599（2006）01-0015-04 |
| 收稿时间： | 2005-06-20 |
| 修稿时间： | 2005-06-20 |
An Analytical Study of Two Aerodynamic Configurations For Low RCS for a Fighter Aircraft |
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| QIU Ju,Ang Hai-song.An Analytical Study of Two Aerodynamic Configurations For Low RCS for a Fighter Aircraft[J].Aircraft Design,2006(1):15-18,60. |
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| Authors: | QIU Ju Ang Hai-song |
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| Institution: | 1. Chengdu Aircraft Industry (Group |
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| Abstract: | An analysis of stealth performances for a canard-wing-tailplane configuration and a blended wing-fuselage configuration was conducted.The analysis results showed that the blended wing-fuselage configuration provides a higher lift coefficient,a forward shifted aerodynamic focus,and significantly low RCS.Finally,proposed modifications to the aerodynamic configurations were given. |
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| Keywords: | aerodynamic characteristics stealth performance blended wing-fuselage configuration |
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