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抖振是大跨度桥梁易发生的一种风振形式。Buffeting is one of recurring aeroelastic dynamic response of long-span bridge.

这类飞机普遍具有大展弦比机翼的特点，它的非线性气动弹性问题…The aeroelastic problems of the UAV are significant due to its high-aspect -ratio wings.

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介绍了超大跨径缆索承重桥梁极限承载力分析的现状和发展趋势。Modal analysis method of aeroelastic full model of cable-supported bridges is introduced.

壁板颤振是发生在高速飞行器上的一种典型的超音速气动弹性现象。Panel flutter is a typical supersonic aeroelastic phenomenon taking place in high speed aircraft.

涡激振动是柔性结构易发生的气动弹性现象。Vortex-induced vibration is one of recurring aeroelastic dynamic responses of flexible structures.

本文还对结构含有间隙非线性的二维机翼的气弹响应进行了分析。The aeroelastic response of 2d airfoil which has freeplay nonlinearity is also analyzed in this paper.

研究了机翼气动弹性系统的不确定性建模及其模型确认问题。The problems of uncertainty modeling and model validation of a wing aeroelastic system are investigated.

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此通用模型，可用于其它超高层建筑的抗风研究。This general aeroelastic model can be used in wind resistance studies of other super high rise buildings.

研究表明，干摩擦式阻尼减振器可以有效地提高篦齿封严装置的气动弹性稳定性。According to the analysis, dry friction damper can raise the aeroelastic stability of the labyrinth gas seals.

进行了一种用解析方法求气动弹性剪裁中的结构响应值敏度的研究。An analytical approach is proposed to obtain the sensitivity of structural responses in aeroelastic tailoring.

所建模型为进行新型倾转旋翼机大速度飞行时气弹稳定性分析奠定了基础。The model can be used for aeroelastic stability analysis of the new tilt-rotor aircraft in high-speed forward flight.

研究了单自由度线性气动弹性系统在延迟反馈控制作用下的颤振稳定性特性。The paper studied the flutter stability of a single-DOF linear aeroelastic system with time-delayed feedback control.

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研究了气动弹性系统的不确定性建模和鲁棒颤振分析问题。The problems of uncertainty modeling and robust flutter analysis of aeroelastic system are investigated in this paper.

本文为激波振荡导致的气动弹性问题提供了一种有价值的理论方法。This paper has supplied a valuable analytical method to study aeroelastic problems produced by shock wave oscillation.

基于热气动弹性的特点，采用松耦合方法建立气动弹性仿真模型。Based on the characteristics of aerothermoelasticity, the loose coupling method is used to establish the aeroelastic model.

利用复合材料蒙皮结构的弯扭耦合效应可以改善翼面的气动弹性特性。The aeroelastic property of a wing can be improved by using the bending-twisting coupling effect of composite material skin.

通过气弹模型风洞试验，研究了不同间距、风偏角、风攻角及固有频率下，串列主缆间的气动干扰特性。The basic aerodynamic interference of tandem cables was investigated through a series of aeroelastic model wind tunnel tests.

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在定常空气动力的作用下，对含立方非线性刚度的二元机翼颤振系统的极限环颤振进行了研究。Limit cycle flutter of a two-dimensional airfoil in cubic nonlinear aeroelastic system in incompressible flow is investigated.

但对于虚拟操纵面方案，气动弹性效应是有利的，可以使用较小的能量控制较为柔软的机翼达到要求的横滚性能。But in the case of FCS, the aeroelastic effect is advantageous and it means that lower structural stiffness can lead to lower voltage.

设计制作了一外形和动力特性在一定范围内可调的超高层建筑多自由度气动弹性模型。A super high rise buildings aeroelastic model, whose configuration and dynamics can be changed to some extent, has been designed and made.