低雷诺数俯仰振荡翼型等离子体流动控制
1)
黄广靖, 戴玉婷, 杨超
PLASMA-BASED FLOW CONTROL ON PITCHING AIRFOIL AT LOW REYNOLDS NUMBER
1)
Huang Guangjing, Dai Yuting, Yang Chao
图21
减缩频率11.82升力系数随时间变化曲线
Fig.21
Lift coefficient as time with $k=11.82$