aeroelastic stability的意思

aeroelastic stability中文翻譯：

氣動彈性穩定性，氣彈穩定性

相似詞語短語

stability───n.穩定性；堅定，恒心

methylal stability───甲縮醛穩定性

stability help───穩定性幫助

gyroscopic stability───[力]陀螺穩定性

flinch stability───畏縮穩定性

postural stability───位置穩定

intact stability───完整穩性（即非破損時的穩定性）；車輛穩定性

dimensional stability───[測][紡][紙]尺寸穩定性；[紡]形穩性；尺寸恒定性，尺寸穩定性，形穩性

intact stability code───完整穩定性代碼

雙語使用場景

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.───同時對懸停時槳葉的氣彈穩定性有相當程度的影響，尤其是在高槳距角下這種影響是不能忽略的。

The experimental results verify that the feasible theory can be used to investigate the effects of structural parameters of hingeless rotor on aeroelastic stability.───試驗證明該理論可行并能用于研究無鉸旋翼結構參數對槳葉氣彈穩定性的影響，也能用于直升機旋翼的型號設計。

The model can be used for aeroelastic stability analysis of the new tilt-rotor aircraft in high-speed forward flight.───所建模型為進行新型傾轉旋翼機大速度飛行時氣彈穩定性分析奠定了基礎。

According to the analysis, dry friction damper can raise the aeroelastic stability of the labyrinth gas seals.───研究表明，干摩擦式阻尼減振器可以有效地提高篦齒封嚴裝置的氣動彈性穩定性。

Effects of Wall Admittance Changes on Aeroelastic Stability of Turbomachines .───壁導納變化對渦輪機氣動彈性力學穩定性的影響。

Mathematical model and formulations of a new tilt-rotor aircraft for aeroelastic stability analysis───新型傾轉旋翼機氣動彈性穩定性分析模型

Aeroelastic Stability for Helicopter Rotor Blades with Consideration of Transverse Shear Deformation and Warping───考慮剪切和翹曲影響的直升機旋翼氣彈穩定性分析

Model experiment and damping identification for aeroelastic stability of helicopter rotor with elastomeric lag damper───帶粘彈減擺器旋翼系統氣彈穩定性試驗與阻尼識別

Analysis of Aeroelastic Stability for Helicopter Rotor with Different Elastomeric Lag Damper Connections───不同粘彈減擺器連接形式下的旋翼系統氣動彈性穩定性分析

英語使用場景

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.