| 民用飞机气动力模型建模方法研究 |
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| 引用本文： | 李,林、李,佳、郑晓辉.民用飞机气动力模型建模方法研究[J].民用飞机设计与研究,2012(1):42-43,60. |
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| 作者姓名： | 李 林、李 佳、郑晓辉 |
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| 作者单位： | 上海飞机设计研究院,上海,200235 |
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| 摘 要： | 对民机常用的两种气动力建模方法——全机建模法和分部件组合建模法进行了研究,并对两者的优缺点进行了对比分析,进而对两类方法在大型客机气动力建模中的综合运用提出了建议。
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| 关 键 词： | 气动力模型 气动弹性修正 下洗 |
Aerodynamic Model Building Methods for Civil Airplanes |
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| Li Lin Li Jia Zheng Xiaohui.Aerodynamic Model Building Methods for Civil Airplanes[J].Civil Aircraft Design and Research,2012(1):42-43,60. |
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| Authors: | Li Lin Li Jia Zheng Xiaohui |
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| Institution: | Li Lin Li Jia Zheng Xiaohui( Shanghai Aircraft Design andResearch Institute, Shanghai 200235, China) |
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| Abstract: | Two kinds of methods for building the aerodynamic models, the overall method and the part-plus-part method, were studied and compared, and some advices on applying these two methods synthetically to the aerodyminc model of the civil trunkliners were provided. |
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| Keywords: | Aerodynamic Model Aeroelastic Correction Downwash |
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