| 柔性飞机非线性气动弹性与飞行动力学耦合静、动态特性 |
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| 引用本文： | 张健,向锦武.柔性飞机非线性气动弹性与飞行动力学耦合静、动态特性[J].航空学报,2011,32(9):1569-1582. |
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| 作者姓名： | 张健 向锦武 |
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| 作者单位： | 北京航空航天大学航空科学与工程学院,北京,100191 |
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| 基金项目： | 国家自然科学基金(90916006)~~ |
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| 摘 要： | 高空长航时(HALE)飞机结构细长、具有柔性,在常规飞行条件下可发生结构大变形、气动失速以及结构低频振动与刚体运动耦合,这些现象显著影响其静、动态特性.基于几何精确完全本征运动梁模型、ONERA动失速气动力模型和六自由度刚体运动模型,建立了考虑几何非线性、动失速和材料各向异性等因素的大展弦比柔性飞机非线性气动弹性与飞行...
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| 关 键 词： | 气动弹性 飞行动力学 柔性飞机 完全本征方程 几何非线性 动失速 刚体运动 高空长航时 |
| 收稿时间： | 2011-01-07; |
Static and Dynamic Characteristics of Coupled Nonlinear Aeroelasticity and Flight Dynamics of Flexible Aircraft |
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| ZHANG Jian,XIANG Jinwu.Static and Dynamic Characteristics of Coupled Nonlinear Aeroelasticity and Flight Dynamics of Flexible Aircraft[J].Acta Aeronautica et Astronautica Sinica,2011,32(9):1569-1582. |
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| Authors: | ZHANG Jian XIANG Jinwu |
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| Institution: | ZHANG Jian,XIANG Jinwu*School of Aeronautic Science and Engineering,Beihang University,Beijing 100191,China |
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| Abstract: | High-altitude long-endurance(HALE) aircraft features slender and flexible structures,which under nominal operation conditions may result in large structural deformation,aerodynamic stall,and coupling between the low-frequency structural vibration and the rigid body motion of the aircraft.These nonlinearities and interactions affect dramatically the static and dynamic behaviors of a HALE flexible aircraft.This paper developed a coupled model of aeroelasticity and flight dynamics for high-aspect-ratio flexibl... |
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| Keywords: | aeroelasticity flight dynamics flexible aircraft fully intrinsic equation geometrical nonlinearity dynamic stall rigid body motion high-altitude long-endurance |
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