| 基于XML技术的结冰后飞机纵向稳定性计算 |
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| 引用本文： | 王起达,王同光.基于XML技术的结冰后飞机纵向稳定性计算[J].飞机设计,2009,29(4):22-25. |
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| 作者姓名： | 王起达 王同光 |
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| 作者单位： | 南京航空航天大学,民航学院,江苏,南京,210016 |
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| 摘 要： | 飞机结冰会使飞机的空气动力学性能恶化,严重影响飞机的稳定性和操纵性.因此,计算飞机稳定性对于保障飞机飞行安全具有重要的意义.本文通过基于XML建模语言技术,建立结冰后飞机气动增量模块计算飞机纵向稳定性.结果表明,用此方法可以方便快捷地计算飞机纵向稳定性.
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| 关 键 词： | 飞机结冰 XML技术 增量模块 纵向稳定性 |
Calculation of the Aircraft Longitudinal Stability with Ice Accretion Basing on XML Technology |
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| WANG Qi-da,WANG Tong-guang.Calculation of the Aircraft Longitudinal Stability with Ice Accretion Basing on XML Technology[J].Aircraft Design,2009,29(4):22-25. |
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| Authors: | WANG Qi-da WANG Tong-guang |
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| Institution: | Civil Aviation College;Nanjing University of Aeronautics and Astronautics;Nanjing 210016;China |
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| Abstract: | Aircraft icing can deteriorate the capability of aerodynamics and badly affect the stability and control of airplanes.Thus it is important for ensuring safe flight to detect airfoil icing.In the paper,the aerodynamic increment model basing on XML technology is established to calculate the aircraft longitudinal stability.The results show that we can conventiontly and fastly calculate the aircraft longitudinal stability. |
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| Keywords: | aircraft icing XML technology increment model longitudinal stability |
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