| dc.contributor.author | Shahriari, B. | |
| dc.contributor.author | Azizi, M. | |
| dc.contributor.author | Farrokhfal, H. | |
| dc.contributor.author | Bokaei, H. | |
| dc.date.accessioned | 2026-08-20T21:12:35Z | |
| dc.date.available | 2026-08-20T21:12:35Z | |
| dc.date.copyright | 2025/08/20 | |
| dc.date.issued | 2025 | |
| dc.identifier.other | JAEEEZ.ASENG-6033.pdf | |
| dc.identifier.uri | http://yetl.yabesh.ir/yetl1/handle/yetl/4314119 | |
| dc.description.abstract | AbstractThe turbine engine nozzle inlet temperature is one of the most influential parameters
in thrust increases, necessitating efficient techniques to safeguard the nozzle wall.
The objective of the present study is to optimize impingement-effusion ... | |
| dc.publisher | American Society of Civil Engineers | |
| dc.title | Optimum Design of Impingement-Effusion Cooling System Using Differential Evolution Algorithm in 2D Vectoring Nozzle of Turbofan Engine | |
| dc.type | Journal Article | |
| dc.journal.volume | 38 | |
| dc.journal.issue | 6 | |
| dc.journal.title | Journal of Aerospace Engineering | |
| dc.identifier.doi | 10.1061/JAEEEZ.ASENG-6033 | |
| dc.journal.fristpage | 04025089-1 | |
| dc.journal.lastpage | 04025089-15 | |
| dc.page | 15 | |
| dc.tree | Journal of Aerospace Engineering:;2025:;Volume ( 038 ):;issue: 006 | |
| dc.contenttype | Fulltext | |
