n.氣動(dòng)力彈性學(xué)
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。
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(duì)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)。
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)構(gòu)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。