Performance of mini jet engine combustor
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...
Saved in:
| Main Author: | |
|---|---|
| Other Authors: | |
| Format: | Final Year Project |
| Language: | English |
| Published: |
2015
|
| Subjects: | |
| Online Access: | http://hdl.handle.net/10356/65282 |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
| Institution: | Nanyang Technological University |
| Language: | English |