| L8和N5A飞机防颤振设计 |
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| 引用本文： | 陈奎林.L8和N5A飞机防颤振设计[J].洪都科技,1995(3):4-9. |
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| 作者姓名： | 陈奎林 |
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| 作者单位： | 650所!中国航空学会 |
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| 摘 要： | 结合Ｌ８和Ｎ５Ａ飞机的设计特点，对操纵面颤振规律，全复合材料垂尾颤振特性，风洞试验模型的动相似反设计等气动弹性技术作了研究。介绍了这些技术在Ｌ８和Ｎ５Ａ飞机设计中的应用情况。
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| 关 键 词： | 防颤振 复合材料 垂直尾翼 动相似反设计 飞机 |
ANTI-FLUTTER DESIGN OF L8 AND N5A AIRCRAFT |
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| Chen Kuilin.ANTI-FLUTTER DESIGN OF L8 AND N5A AIRCRAFT[J].Hongdu Science and Technology,1995(3):4-9. |
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| Authors: | Chen Kuilin |
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| Institution: | NO. 650 Institute |
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| Abstract: | This paper researches on aeroelasticity technique such as flutter law of control surfaces, flutter behaviour of all-composite vertical tail and dynamic similarity updating design of wind-tunnel model in the light of L8 and N5A aircraft design characteristics. It introduces application of these technique in design of L8 and N5A aircraft. |
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| Keywords: | Anti-flutter design All-composite vertical tail Dynamic similarity updating design |
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