Automated multi-code URANS simulation of compressor-combustor components
Currently in an aircraft gas turbine engine, the turbomachinery and combustor components are designed in relative isolation and the effect of the upstream and downstream components on each other’s flow are not fully captured in the design process. The objective of this work is to carry out a multi-c...
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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/2134/22501 |
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