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11 减缩频率5.01时基准流场结构
Fig.11 Flow field structure of baseline with $k=5.01$