Laminar-turbulent transition induced by a discrete roughness element in a supersonic boundary layer
The linear instability and breakdown to turbulence induced by an isolated roughness element in a boundary layer at Mach 2:5, over an isothermal flat plate with laminar adiabatic wall temperature, have been analysed by means of direct numerical simulations, aided by spatial BiGlobal and three-dimensi...
| Main Authors: | , , , |
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| Format: | Article |
| Language: | English |
| Published: |
2013-11.
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| Subjects: | |
| Online Access: | Get fulltext |