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27 最大升力系数和平均阻力系数变化率随雷诺数的变化曲线
Fig.27 Rate of max lift coefficient and average drag coefficient change as Reynold numbers