aeroelastic发音

意思翻译

adj.空气弹性变形的

相似词语短语

双语使用场景

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。

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。

show that the new state-space aeroelastic model is one which has higher accuracy and lower order.───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。

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。

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。

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。

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。

英语使用场景

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.

An aeroelastic model for a UHV power transmission tower and its conductors was designed according to the law of similarity and tested in an atmospheric boundary layer wind tunnel.

Finally for all the above aeroelastic problems, distributed parallel computation is accomplished.

In the design of aeroelastic model of long-span concrete-filled steel tube arch bridge, the method of using an equivalent mandril to simulate the stiffness of whole arch rib is mainly used at present.

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.

Inertia relief theory and static aeroelastic method based on CFD/CSD are introduced in this paper. Three force equilibrium methods of static aeroelasticity are compared with.

Finally aeroelastic tailoring technique of composite laminate is applied to forward - wing structure to improve divergence speed.

The aeroelastic phenomena may be subdivided under the heading static and dynamic.

Aeroelastic model is developed to analyze aeroelastic stability of helicopter rotor blade with swept tips.