aeroelastic stability发音

意思翻译

气动弹性稳定性，气弹稳定性

相似词语短语

stability───n.稳定性；坚定，恒心

methylal stability───甲缩醛稳定性

stability help───稳定性帮助

gyroscopic stability───[力]陀螺稳定性

flinch stability───畏缩稳定性

postural stability───位置稳定

intact stability───完整稳性（即非破损时的稳定性）；车辆稳定性

dimensional stability───[测][纺][纸]尺寸稳定性；[纺]形稳性；尺寸恒定性，尺寸稳定性，形稳性

intact stability code───完整稳定性代码

双语使用场景

also seen that the transverse shear deformation and warping have effects on the aeroelastic stability of the rotor blade. These effects become larger at the higher thrust level.───同时对悬停时桨叶的气弹稳定性有相当程度的影响，尤其是在高桨距角下这种影响是不能忽略的。

The experimental results verify that the feasible theory can be used to investigate the effects of structural parameters of hingeless rotor on aeroelastic stability.───试验证明该理论可行并能用于研究无铰旋翼结构参数对桨叶气弹稳定性的影响，也能用于直升机旋翼的型号设计。

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。

According to the analysis, dry friction damper can raise the aeroelastic stability of the labyrinth gas seals.───研究表明，干摩擦式阻尼减振器可以有效地提高篦齿封严装置的气动弹性稳定性。

Effects of Wall Admittance Changes on Aeroelastic Stability of Turbomachines .───壁导纳变化对涡轮机气动弹性力学稳定性的影响。

Mathematical model and formulations of a new tilt-rotor aircraft for aeroelastic stability analysis───新型倾转旋翼机气动弹性稳定性分析模型

Aeroelastic Stability for Helicopter Rotor Blades with Consideration of Transverse Shear Deformation and Warping───考虑剪切和翘曲影响的直升机旋翼气弹稳定性分析

Model experiment and damping identification for aeroelastic stability of helicopter rotor with elastomeric lag damper───带粘弹减摆器旋翼系统气弹稳定性试验与阻尼识别

Analysis of Aeroelastic Stability for Helicopter Rotor with Different Elastomeric Lag Damper Connections───不同粘弹减摆器连接形式下的旋翼系统气动弹性稳定性分析

英语使用场景

According to the analysis, dry friction damper can raise the aeroelastic stability of the labyrinth gas seals.

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.

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

The experimental results verify that the feasible theory can be used to investigate the effects of structural parameters of hingeless rotor on aeroelastic stability.