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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Main Author: | Tan, Xiangwei |
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Other Authors: | Tang Hui |
Format: | Final Year Project |
Language: | English |
Published: |
2014
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Subjects: | |
Online Access: | http://hdl.handle.net/10356/60082 |
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Institution: | Nanyang Technological University |
Language: | English |
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