Performance of mini jet engine combustor

• Main Author: Chan, Wai Lek
• Other Authors: Fei Duan
• Format: Final Year Project
• Language: English
• Published: 2015
• Subjects: DRNTU::Engineering::Aeronautical engineering
• Online Access: http://hdl.handle.net/10356/65282
• Institution: Nanyang Technological University

Reverse-flow combustor are normally installed on mini turbojet engines due to its smaller size and space required. A numerical study on a reverse-flow combustor was conducted to investigate its performance using ANSYS Fluent. A mesh independence study was carried out prior to the numerical simulatio...