| 释义 |
aeroelastic 英eərəʊɪ'læstɪk美eəroʊɪ'læstɪk COCA²¹³⁵⁴⁵BNC²³⁶²¹³⁺¹
基本例句
adj.气动弹性的¹⁰⁰
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。 cnki
Also, spin rate coupling with structural damping ratio and other structural parameters have a significant influence in aeroelastic dynamic instability for spinning rocket.
旋转速率与结构阻尼及其他结构参数对气动弹性动态稳定性影响也比较显著。 dictall
An experimental study of flutter instability of H-shaped slender member with different sizes of slotted web is carried out using both section models and aeroelastic model.
通过节段模型与气弹模型风洞试验，研究了不同腹板开孔率的 H型细长结构的风致颤振失稳特性。 dictall
The experimental investigation on aeroelastic instability and dynamic response of the BF-1 rotors by a transonic axial-flow compressor test rig are presented in this paper.
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和动态响应的实验研究工作。 cnki
The numerical application is performed for robust static divergence and aeroelastic deformation of a large aspect- ratio wing with perturbation on the elastic modulus of its fore- beam.
以一大展弦比长直机翼为例，分析了机翼前梁的材料弹性模态受到一定摄动时的鲁棒静发散稳定性和静气动弹性变形性能。 cnki
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。 dictall
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。 dictall
The wind-induced responses, including displacement, acceleration and angular velocity responses, were measured by an aeroelastic model, and the dynamic wind load was gained.
用气动弹性模型测量风致响应，包括大厦顶部的位移响应、加速度响应和角速度响应，并计算动风荷载。 cnki
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。 dictall
A theory of aeroelastic stability of hingeless rotor blade in hover by using the Galerkin weighted residual finite element method is developed in this paper.
采用伽辽金加权余数有限元素法发展了一种悬停状态下无铰旋翼桨叶气弹稳定性的分析方法。 cnki
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。 dictall
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。 cnki
Based on the characteristics of aerothermoelasticity, the loose coupling method is used to establish the aeroelastic model.
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。 dictall
Flutter and aeroservoelastic instability are dangerous aeroelastic problems and the critical boundary should be predicted by flight test in the terminal stage of the aircraft design.
颤振和气动伺服弹性失稳是危险的气动弹性现象，在飞机设计的最后阶段需要依靠飞行试验来预测气动弹性稳定边界。 cnki
It is very difficult to design and manufacture aeroelastic models of space structures.
空间结构气动弹性模型的设计和制作是非常困难的。 dictall
Missile carrying on the wing tip causes the wing structure design and analysis to face many challenges, such as structural vibration response and aeroelastic response.
飞机机翼挂装翼尖导弹对机翼结构设计和结构分析提出了诸多全新课题，如结构的振动响应和气动弹性动响应。 cnki
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。 cnki
The paper studied the flutter stability of a single-DOF linear aeroelastic system with time- delayed feedback control.
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。 dictall
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。 cnki
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。 cnki
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。 cnki
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。 cnki
Wind tunnel tests of rigid and aeroelastic model were carried out to investigate the influence of windward sudden opening on static and dynamic wind load for flat roof structures.
采用刚性模型和气动弹性模型风洞试验，研究迎风面突然开孔对平屋盖结构静动力风荷载的影响。 dictall |