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 |