Surge/ stall study on the compressor of a mini jet engine

• المؤلف الرئيسي: Tan, Xiangwei
• مؤلفون آخرون: Tang Hui
• التنسيق: Final Year Project
• اللغة: English
• منشور في: 2014
• الموضوعات: DRNTU::Engineering::Aeronautical engineering::Aerodynamics
• الوصول للمادة أونلاين: http://hdl.handle.net/10356/60082

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...