The dynamic loads must be extrapolated using aeroelastic scale factors.
动力载荷必须用气动弹性尺度因子来推算。
The aeroelastic phenomena may be subdivided under the heading static and dynamic.
气动弹性现象可以再分为静态和动态两个专题。
The aeroelastic problems of the UAV are significant due to its high-aspect -ratio wings .
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…
Panel flutter is a typical supersonic aeroelastic phenomenon taking place in high speed aircraft.
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。
Before the vortex breakdown, the aeroelastic instability presents itself as just a simple flutter.
涡破裂前，气动弹性失稳表现为单纯的颤振问题。
The problems of uncertainty modeling and model validation of a wing aeroelastic system are investigated.
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。
This general aeroelastic model can be used in wind resistance studies of other super high rise buildings.
此通用模型，可用于其它超高层建筑的抗风研究。
The results show that the new state-space aeroelastic model is one which has higher accuracy and lower order.
算例表明：本文提出的新的状态空间气动弹性模型是一种精度较高而阶数较低的模型。
An analytical approach is proposed to obtain the sensitivity of structural responses in aeroelastic tailoring.
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。
A refined aeroelastic model of a helicopter rotor blade with swept tips is established based on model matching.
以动力学模型和气动模型相匹配为原则，建立了后掠桨尖旋翼的细致气弹模型。
The bifurcation and complex response of the nonlinear aeroelastic systems are the research hotspot in this area.
气动弹性颤振的抑制、系统的分岔、复杂响应等是该领域目前研究的热点。
The model can be used for aeroelastic stability analysis of the new tilt-rotor aircraft in high-speed forward flight.
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 problems of uncertainty modeling and robust flutter analysis of aeroelastic system are investigated in this paper.
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。
This paper has supplied a valuable analytical method to study aeroelastic problems produced by shock wave oscillation.
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。
Aeroelastic tailoring technique involves mechanics of composite materials, aeroelastic dynamics and optimization methods.
复合材料气动弹性剪裁技术涉及复合材料力学、气动弹性力学和优化方法。
Aeroelastic analysis at high angles of attack is an attractive and complicated research subject in modern aircraft design.
大迎角气动弹性分析是现代飞行器设计中非常引人瞩目并且复杂的研究课题。
The basic aerodynamic interference of tandem cables was investigated through a series of aeroelastic model wind tunnel tests.
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。
A super high rise buildings aeroelastic model, whose configuration and dynamics can be changed to some extent, has been designed and made.
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。
The identification technology of unsteady aerodynamic loads shows a high efficient and accuracy approach for transonic aeroelastic solving.
证明非定常气动力辨识技术可以提供高效的高精度的气动弹性分析。
With improvement of aircraft performance, the aeroelastic problem becomes serious, so the aeroelastic analysis becomes more and more important.
随着飞机性能的提高，气动弹性问题日益突出，使得气动弹性分析在飞机设计中的作用越来越重要。
This paper comprehensively introduces a survey and a theory foundation concerning the aeroelastic tailoring for the present composite aircraft.
本文综合介绍了当前复合材料的飞机结构在气动弹性剪裁方面的概况及其理论基础。
This paper describes the initial experimental results of aeroelastic instability of BF-1 rotors on a transonic axial compressor facility at BIAA.
本文介绍了在跨音压气机试验台上对BF - 1系列转子开展气动弹性失稳的实验研究工作。
Vortex-induced vibration of the bridge is an important aeroelastic phenomena, it is easy for long-span bridges to occur Vortex-induced vibration.
桥梁涡激振动是大跨度桥梁在低风速下很容易出现的一种重要的气动弹性现象。
The transfer of the elastic axes is very remarkable with the symmetrical ply and this characteristic is worthy of attention in aeroelastic control.
对称铺设方式下铺设角对结构刚轴移动的影响非常明显，在气动弹性控制中应着重关注。
In this paper, basic design information is first described, followed by briefly introduction to section model and full aeroelastic model wind tunnel tests.
介绍了该桥的设计基本情况、三汊矶大桥节段模型和全桥模型风洞试验情况。
An aeroelastic wind tunnel test was carried out to study the rational wind resistant design method for high-voltage transmission tower-line coupling system.
为研究高压输电塔线体系的合理化抗风设计，进行了气动弹性模型风洞试验。
Years followed, current research has turned toward the application of Computational Fluid Dynamics(CFD) models to the solution of these aeroelastic problems.
近些年来，人们开始应用计算流体动力学（CFD）来求解气动弹性问题。
The mechanisms of aeroelastic tailoring are explained emphatically, which are the basic principles on which the realization of aeroelastic tailoring depends.
着重阐述了气动弹性剪裁的机理，即气动弹性剪裁赖以实现的基本原理。
The mechanisms of aeroelastic tailoring are explained emphatically, which are the basic principles on which the realization of aeroelastic tailoring depends.
着重阐述了气动弹性剪裁的机理，即气动弹性剪裁赖以实现的基本原理。
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