aeroelastic的意思

aeroelastic中文翻譯：

adj.空氣彈性變形的

相似詞語短語

雙語使用場景

Panel flutter is a typical supersonic aeroelastic phenomenon taking place in high speed aircraft.───壁板顫振是發生在高速飛行器上的一種典型的超音速氣動彈性現象。

problems of uncertainty modeling and model validation of a wing aeroelastic system are investigated.───研究了機翼氣動彈性系統的不確定性建模及其模型確認問題。

show that the new state-space aeroelastic model is one which has higher accuracy and lower order.───表明：本文提出的新的狀態空間氣動彈性模型是一種精度較高而階數較低的模型。

Before the vortex breakdown, the aeroelastic instability presents itself as just a simple flutter.───渦破裂前，氣動彈性失穩表現為單純的顫振問題。

The problems of uncertainty modeling and model validation of a wing aeroelastic system are investigated.───研究了機翼氣動彈性系統的不確定性建模及其模型確認問題。

Aeroelastic analysis at high angles of attack is an attractive and complicated research subject in modern aircraft design.───大迎角氣動彈性分析是現代飛行器設計中非常引人矚目并且復雜的研究課題。

A super high rise buildings aeroelastic model, whose configuration and dynamics can be changed to some extent, has been designed and made.───設計制作了一外形和動力特性在一定范圍內可調的超高層建筑多自由度氣動彈性模型。

The identification technology of unsteady aerodynamic loads shows a high efficient and accuracy approach for transonic aeroelastic solving.───證明非定常氣動力辨識技術可以提供高效的高精度的氣動彈性分析。

The dynamic loads must be extrapolated using aeroelastic scale factors.───動力載荷必須用氣動彈性尺度因子來推算。

英語使用場景

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.