Transitional shock-wave/boundary-layer interactions in hypersonic flow
Strong interactions of shock waves with boundary layers lead to flow separations and enhanced heat transfer rates. When the approaching boundary layer is hypersonic and transitional the problem is particularly challenging and more reliable data is required in order to assess changes in the flow and...
| Main Authors: | , , , , |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
2014-07-04.
|
| Subjects: | |
| Online Access: | Get fulltext |