| 某民机尾翼布局对全机稳定性影响分析 |
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| 引用本文： | 李鹏飞,陈雅丽,魏文建,万俊明.某民机尾翼布局对全机稳定性影响分析[J].洪都科技,2014(2):28-32. |
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| 作者姓名： | 李鹏飞 陈雅丽 魏文建 万俊明 |
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| 作者单位： | 中航工业洪都,江西南昌330024 |
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| 摘 要： | 利用CFD手段,对下单翼尾吊布局民机的两种不同尾翼布局形式进行计算,分析两种不同尾翼布局对全机的纵向、航向稳定性的影响,结果表明,对于下单翼尾吊布局的民机,气动上"T"型尾翼布局更具优势。
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| 关 键 词： | 气动设计 尾翼布局 稳定性 |
Analysis of Effect of Empennage Layout of a Certain Civil Aircraft on Aircraft Stability |
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| Li Pengfei,Chen Yali,Wei Wenjian,Wan Junming.Analysis of Effect of Empennage Layout of a Certain Civil Aircraft on Aircraft Stability[J].Hongdu Science and Technology,2014(2):28-32. |
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| Authors: | Li Pengfei Chen Yali Wei Wenjian Wan Junming |
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| Institution: | (AVIC Hongdu Aviation Industry Group, Nanchang, Jiangxi, 330024) |
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| Abstract: | Calculation is done for two different empennage layouts of low wing tail mounted civil aircraft by means of CFD, and effect of two different empennage layouts on vertical and heading stability is analyzed. The result shows that＂T＂ type empennage layout is superior in aerodynamic for low wing tail mounted civil aircraft. |
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| Keywords: | aerodynamic design empennage layout stability |
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