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19 后缘DBD控制最大升力系数和平均阻力系数变化率随减缩频率的变化曲线
Fig.19 The rate of max lift coefficient and average drag coefficient change as reduced frequency with plasma at trailing edge