| dc.contributor.author | Guan, Yuxi | |
| dc.contributor.author | Liu, Shuai | |
| dc.contributor.author | Zhang, Shengqiu | |
| dc.contributor.author | Bai, Jie | |
| dc.date.accessioned | 2026-08-20T21:13:12Z | |
| dc.date.available | 2026-08-20T21:13:12Z | |
| dc.date.copyright | 2025/09/10 | |
| dc.date.issued | 2025 | |
| dc.identifier.other | JAEEEZ.ASENG-6202.pdf | |
| dc.identifier.uri | http://yetl.yabesh.ir/yetl1/handle/yetl/4314134 | |
| dc.description.abstract | AbstractA physics-based component-level model has been developed to investigate the influence
of fuel-rich combustion on the accuracy of low-pressure turbine speed prediction following
low-pressure shaft failure in a turbofan engine. The model extends ... | |
| dc.publisher | American Society of Civil Engineers | |
| dc.title | Influence of Fuel-Rich Combustion on the Accuracy of Turbine Speed Prediction in the Event of Shaft Failure | |
| 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-6202 | |
| dc.journal.fristpage | 04025102-1 | |
| dc.journal.lastpage | 04025102-17 | |
| dc.page | 17 | |
| dc.tree | Journal of Aerospace Engineering:;2025:;Volume ( 038 ):;issue: 006 | |
| dc.contenttype | Fulltext | |
