aeroelasticity发音

意思翻译

n.空气弹性；[航]气动力弹性学

相似词语短语

双语使用场景

data exchange to reflect coupling between fluid and structures is essential to solving static aeroelasticity problems.───静气动弹性问题一大关键是要解决流固数据耦合。

new problems of aeroelasticity which are introduced by the novel concepts and system characteristics in the design process of hypersonic vehicles.───高超声速飞行器设计上的特点带来了一系列的气动弹性新问题。

Coupled with the structural equations, the models for transonic aeroelasticity in state-space are got.───耦合结构动力学方程，建立了基于状态空间的跨声速气动弹性分析模型。

The main difficulty on the study of aeroelasticity lies in the effects of unsteady separation, shock and viscosity to the stall flutter.───振荡叶栅的非定常分离、粘性效应和跨音激波对失速颤振的影响成为当前气动弹性力学的主要难点。

There exist obvious aeroelasticity problem for the large-scaled civil aircraft with high aspect ratio wings.───大型民用飞机普遍具有大展弦比机翼的特点，其气动弹性问题尤为突出。

Investigation of two aeroelasticity problems in transonic flow───两种跨声速气动弹性问题分析研究

Application of Regress Analysis Method to Aeroelasticity Research───回归分析方法在气动弹性研究中的应用

Introduction to Aircraft Aeroelasticity and Dynamic Loads───动力载荷飞行气动弹性力学导论

Discussion on Aeroelasticity of Large Aspect-ratio Wing───大展弦比机翼的气动弹性问题探讨

英语使用场景

In order to eliminate the interaction between aeroelasticity and flight control of vehicles, the positions of mounted sensors must be chosen properly.

In this paper, based on theory of aeroelasticity, the mathematical model of rotor of labyrinth seal flow induced vibration, dynamical behaviors of the rotor system are analyzed.

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There exist obvious aeroelasticity problem for the large-scaled civil aircraft with high aspect ratio wings.

There are many new problems of aeroelasticity which are introduced by the novel concepts and system characteristics in the design process of hypersonic vehicles.

The main difficulty on the study of aeroelasticity lies in the effects of unsteady separation, shock and viscosity to the stall flutter.

Develop an analytical model of the nonlinear aeroelasticity of the high-aspect-ratio wings and give the nonlinear partial equations of wing structure motion based on the Hamilton principle.

Some typical numerical results are presented from application of the model to the static analysis, dynamic analysis, static aeroelasticity and flutter analysis of a wing-box and a wing.

A method of analysis of the effect of aeroelasticity on the stability of elastic vehicles by using a simplified mathematical model of unsteady aerodynamic forces is proposed.