| 某联接翼飞机外形参数变化对稳定性影响的研究 |
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| 引用本文： | 郭卫刚,贾忠湖,康小伟.某联接翼飞机外形参数变化对稳定性影响的研究[J].飞机设计,2007,27(2):37-40,58. |
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| 作者姓名： | 郭卫刚 贾忠湖 康小伟 |
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| 作者单位： | 海军航空工程学院,飞行器工程系,山东,烟台,264001 |
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| 摘 要： | 确定7个变量参数构造了联接翼飞机的外形布局,应用涡格法分析了这7个外形参数的变化对联接翼飞机俯仰稳定性、滚转稳定性和航向稳定性的影响,为飞机总体设计提供了理论依据。
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| 关 键 词： | 联接翼飞机 外形参数 稳定性 |
| 文章编号： | 1673-4599（2007）02-0037-04 |
| 收稿时间： | 2006-07-26 |
| 修稿时间： | 2006-07-262007-03-19 |
Impacts of Aerodynamic Configuration Parameters on Stabilities of Joined-Wing Aircraft |
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| GUO Wei-gang,JIA Zhong-hu,KANG Xiao-wei.Impacts of Aerodynamic Configuration Parameters on Stabilities of Joined-Wing Aircraft[J].Aircraft Design,2007,27(2):37-40,58. |
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| Authors: | GUO Wei-gang JIA Zhong-hu KANG Xiao-wei |
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| Institution: | Department of aircraft engineering, Naval Aeronautical Engineering Institute, Yantai 264001, China |
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| Abstract: | Seven parameters are defined to construct the aerodynamic configuration of joined-wing aircraft.The vortex lattice method is used to analyze impacts of the seven parameters on pitching,rolling and yawing stabilities.These results would provide a basis for future aircraft designs. |
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| Keywords: | joined-wing aircraft configuration parameter stability |
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