UNSTEADY SHOCK WAVE – TURBULENT BOUNDARY LAYER INTERACTION IN THE LAVAL NOZZLE
The flow in transonic diffusers and supersonic air intakes often becomes unsteady due to shock wave-boundary layer interaction. Oscillations may be induced by natural separation unsteadiness or forced by boundary conditions. Significant improvements of CFD tools, increased computer resources and th...
| Main Authors: | , , |
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| Format: | Article |
| Language: | English |
| Published: |
Gdańsk University of Technology
2005-01-01
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| Series: | TASK Quarterly |
| Subjects: | |
| Online Access: | https://journal.mostwiedzy.pl/TASKQuarterly/article/view/2150 |