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contributor authorGuan, Yuxi
contributor authorLiu, Shuai
contributor authorZhang, Shengqiu
contributor authorBai, Jie
date accessioned2026-08-20T21:13:12Z
date available2026-08-20T21:13:12Z
date copyright2025/09/10
date issued2025
identifier otherJAEEEZ.ASENG-6202.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4314134
description abstractAbstractA 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 ...
publisherAmerican Society of Civil Engineers
titleInfluence of Fuel-Rich Combustion on the Accuracy of Turbine Speed Prediction in the Event of Shaft Failure
typeJournal Article
journal volume38
journal issue6
journal titleJournal of Aerospace Engineering
identifier doi10.1061/JAEEEZ.ASENG-6202
journal fristpage04025102-1
journal lastpage04025102-17
page17
treeJournal of Aerospace Engineering:;2025:;Volume ( 038 ):;issue: 006
contenttypeFulltext


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