aeroelastics

基本解釋

Aeroelastics should be developed as a decisive role during the period of airplane design.
氣動(dòng)彈性作為一門設(shè)計(jì)學(xué)科應(yīng)在設(shè)計(jì)過(guò)程中發(fā)揮關(guān)鍵性作用。
In the domain of aeroelastics, flutter phenomenen is paid most attention when designing aircraft.
在氣動(dòng)彈性領(lǐng)域中，人們?cè)谠O(shè)計(jì)過(guò)程中最為關(guān)心的是顫振現(xiàn)象。
On this base, the static aeroelastics problems of wing and aircraft are investigated by coupled with structure dynamic equation.
并在此基礎(chǔ)上耦合結(jié)構(gòu)力學(xué)方程研究了三維機(jī)翼以及全機(jī)的靜氣動(dòng)彈性問(wèn)題。
On the base of the numerical simulation of unsteady viscous flows, the characters of the static aeroelastics and flutter for the wings are researched.
在模擬非定常粘性繞流的基礎(chǔ)上，對(duì)涉及機(jī)翼和控制面流固耦合作用的靜氣動(dòng)彈性特性和顫振特性進(jìn)行了研究。
Servo aeroelastics analysis is becoming more and more important in designing modern surface-to-air and air-to-air missiles when high velocity and super maneuverability were needed.
隨著對(duì)飛行速度和機(jī)動(dòng)性能要求的不斷提高,伺服氣動(dòng)彈性問(wèn)題成為新一代地空和空空導(dǎo)彈急需解決的重要技術(shù)問(wèn)題。