Investigation on wedge shock wave control by surface MHD actuation
To study the effect of magnetohydrodynamic actuation on wedge shock waves under hypersonic flow, experiments were conducted in a Mach 7 hypersonic shock tunnel. A schlieren method was used to visualize the shock waves and the flow, which showed that the shock waves raised and moved forward under 0.3...
| Main Authors: | , , , |
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| Format: | Article |
| Language: | English |
| Published: |
AIP Publishing LLC
2020-05-01
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| Series: | AIP Advances |
| Online Access: | http://dx.doi.org/10.1063/1.5145235 |