| contributor author | Shahriari, B. | |
| contributor author | Azizi, M. | |
| contributor author | Farrokhfal, H. | |
| contributor author | Bokaei, H. | |
| date accessioned | 2026-08-20T21:12:35Z | |
| date available | 2026-08-20T21:12:35Z | |
| date copyright | 2025/08/20 | |
| date issued | 2025 | |
| identifier other | JAEEEZ.ASENG-6033.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl1/handle/yetl/4314119 | |
| 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 ... | |
| publisher | American Society of Civil Engineers | |
| title | Optimum Design of Impingement-Effusion Cooling System Using Differential Evolution Algorithm in 2D Vectoring Nozzle of Turbofan Engine | |
| type | Journal Article | |
| journal volume | 38 | |
| journal issue | 6 | |
| journal title | Journal of Aerospace Engineering | |
| identifier doi | 10.1061/JAEEEZ.ASENG-6033 | |
| journal fristpage | 04025089-1 | |
| journal lastpage | 04025089-15 | |
| page | 15 | |
| tree | Journal of Aerospace Engineering:;2025:;Volume ( 038 ):;issue: 006 | |
| contenttype | Fulltext | |
