Simple and robust framework for coupled aerothermal gas turbine simulation using low-mach and compressible industrial CFD solvers
Efforts are being made to achieve a coupled virtual aero-engine simulation using existing validated solvers. A methodology to easily couple a low-Mach number pressure-based code with a compressible density-based turbomachinery code for industrial application has been developed, based on boundary con...
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| Main Authors: | , , , |
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| Format: | Default Conference proceeding |
| Published: |
2016
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| Subjects: | |
| Online Access: | https://hdl.handle.net/2134/22500 |
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