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:
| 主要作者: | |
|---|---|
| 其他作者: | |
| 格式: | Final Year Project |
| 語言: | English |
| 出版: |
2015
|
| 主題: | |
| 在線閱讀: | http://hdl.handle.net/10356/65282 |
| 標簽: |
添加標簽
沒有標簽, 成為第一個標記此記錄!
|