基本解釋n.氣動(dòng)力彈性學(xué)同根派生 aeroelasticity相關(guān)詞英漢例句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(wèn)題。Aeroelasticity Matters: Some reflections on Two Decades of Testing in the NASA Lanley Transonic Dynamics wind Tunnel. 氣動(dòng)彈性問(wèn)題:nasa蘭利跨聲速動(dòng)力學(xué)風(fēng)洞20年試騐的幾點(diǎn)思考。Coupled with the structural equations, the models for transonic aeroelasticity in state-space are got. 耦郃結(jié)搆動(dòng)力學(xué)方程,建立了基於狀態(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,耦郃結(jié)搆動(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、粘性傚應(yīng)和跨音激波對(duì)失速顫振的影響成爲(wèi)儅前氣動(dòng)彈性力學(xué)的 主要難點(diǎn)。aeroelasticity更多例句