基于高温气体效应的磁流体流动控制研究进展1)

罗凯, 汪球, 李逸翔, 李进平, 赵伟

RESEARCH PROGRESS ON MAGNETOHYDRODYNAMIC FLOW CONTROL UNDER TEST CONDITIONS WITH HIGH TEMPERATURE REAL GAS EFFECT1)

Luo Kai, Wang Qiu, Li Yixiang, Li Jinping, Zhao Wei

图7 2019年, Smith等[21]在X2膨胀风洞的激波脱体距离实验结果, 实验气体为氩气, 气流速度5963 m/s

Fig.7 Comparison of shock stand-off distance with/without the magnet in the X2 expansion shock tunnel by Smith et al[21] in 2019.The test gas is argon and velocity of the free stream is 5963 m/s