Surge/ stall study on the compressor of a mini jet engine
A Computational Fluid Dynamics (CFD) framework was established to analyse the flow within the SR-30 mini jet engine compressor. The software utilized in the study were ANSYS ICEM CFD and FLUENT. The simulations adopted the Multiple Reference Frame (MRF) model for steady flow. Preliminary simulati...
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| Format: | Final Year Project (FYP) |
| Language: | English |
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2014
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| Online Access: | http://hdl.handle.net/10356/60082 |