基于高温气体效应的磁流体流动控制研究进展1)
RESEARCH PROGRESS ON MAGNETOHYDRODYNAMIC FLOW CONTROL UNDER TEST CONDITIONS WITH HIGH TEMPERATURE REAL GAS EFFECT1)
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 |
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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11 20 mm球头模型以12.4 km/s速度从75 km近地轨道再入[ |
| Fig.11 Stagnation point heat flux of the R20 mm sphere model along the flight trajectories for different magnet cases, reentry from the height of 75 km with a velocity of 12.4 km/s[ |
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