The shape of incident shock wave in steady axisymmetric conical Mach reflection
Abstract For internal flow with supersonic inflow boundary conditions, a complicated oblique shock reflection may occur. Different from the planar shock reflection problem, where the shape of the incident shock can be a straight line, the shape of the incident shock wave in the inward-facing axisymm...
| Main Authors: | , , |
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| Format: | Article |
| Language: | English |
| Published: |
SpringerOpen
2020-10-01
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| Series: | Advances in Aerodynamics |
| Subjects: | |
| Online Access: | http://link.springer.com/article/10.1186/s42774-020-00047-6 |