常見(jiàn)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)。
• However, this new structure also leads to some problems in strength and aeroelasticity, so some analytical results and suggestions are presented.
  但是這種新型的結(jié)搆也帶來(lái)了強(qiáng)度、氣彈穩(wěn)定性等問(wèn)題，對(duì)此給出了一些分析結(jié)果和建議。
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