aeroelasticity的意思

aeroelasticity中文翻譯：

n.空氣彈性；[航]氣動力彈性學

相似詞語短語

雙語使用場景

data exchange to reflect coupling between fluid and structures is essential to solving static aeroelasticity problems.───靜氣動彈性問題一大關鍵是要解決流固數據耦合。

new problems of aeroelasticity which are introduced by the novel concepts and system characteristics in the design process of hypersonic vehicles.───高超聲速飛行器設計上的特點帶來了一系列的氣動彈性新問題。

Coupled with the structural equations, the models for transonic aeroelasticity in state-space are got.───耦合結構動力學方程，建立了基于狀態空間的跨聲速氣動彈性分析模型。

The main difficulty on the study of aeroelasticity lies in the effects of unsteady separation, shock and viscosity to the stall flutter.───振蕩葉柵的非定常分離、粘性效應和跨音激波對失速顫振的影響成為當前氣動彈性力學的主要難點。

There exist obvious aeroelasticity problem for the large-scaled civil aircraft with high aspect ratio wings.───大型民用飛機普遍具有大展弦比機翼的特點，其氣動彈性問題尤為突出。

Investigation of two aeroelasticity problems in transonic flow───兩種跨聲速氣動彈性問題分析研究

Application of Regress Analysis Method to Aeroelasticity Research───回歸分析方法在氣動彈性研究中的應用

Introduction to Aircraft Aeroelasticity and Dynamic Loads───動力載荷飛行氣動彈性力學導論

Discussion on Aeroelasticity of Large Aspect-ratio Wing───大展弦比機翼的氣動彈性問題探討

英語使用場景

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.