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