与扰流振幅相比，调节扰流振荡频率更能改善翼型深失速条件下的气动性能。
The frequency of oscillating excitation has more effect on improving aerodynamic performance of airfoil at large attack…
分析了旋转失速起始条件的机理。
Mechanism for the onset condition of rotating stall is analysed.
本文给出了确定风力透平叶片振动时二元非定常气动力解法，包括在非失速和失速两种条件下的非定常气动力。
This paper presents a method for determining unsteady aerodynamic force on oscillating blade of wind turbine, both stalled and unstalled.
本文给出了确定风力透平叶片振动时二元非定常气动力解法，包括在非失速和失速两种条件下的非定常气动力。
This paper presents a method for determining unsteady aerodynamic force on oscillating blade of wind turbine, both stalled and unstalled.
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