aeroelasticity

基本解釋

Airfoil flutter is one of the important problems in aeroelasticity.
在氣動(dòng)彈性力學(xué)中,機(jī)翼振顫是一個(gè)非常典型的問題。
Aeroelasticity Matters: Some reflections on Two Decades of Testing in the NASA Lanley Transonic Dynamics wind Tunnel.
氣動(dòng)彈性問題：nasa蘭利跨聲速動(dòng)力學(xué)風(fēng)洞20年試驗(yàn)的幾點(diǎn)思考。
Coupled with the structural equations, the models for transonic aeroelasticity in state-space are got.
耦合結(jié)構(gòu)動(dòng)力學(xué)方程,建立了基于狀態(tài)空間的跨聲速氣動(dòng)彈性分析模型。
Using above methods to solve unsteady pressure distribution, coupling structure equations, the supersonic or hypersonic aeroelasticity is simulated in time-domain.
運(yùn)用上述的非定常氣動(dòng)力求解方法，耦合結(jié)構(gòu)動(dòng)力學(xué)方程，實(shí)現(xiàn)超音速、高超音速氣動(dòng)彈性的模擬。
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(yīng)和跨音激波對失速顫振的影響成為當(dāng)前氣動(dòng)彈性力學(xué)的主要難點(diǎn)。