YaBeSH Engineering and Technology Library

    • Journals
    • PaperQuest
    • YSE Standards
    • YaBeSH
    • Login
    View Item 
    •   YE&T Library
    • ASCE
    • Journal of Aerospace Engineering
    • View Item
    •   YE&T Library
    • ASCE
    • Journal of Aerospace Engineering
    • View Item
    • All Fields
    • Source Title
    • Year
    • Publisher
    • Title
    • Subject
    • Author
    • DOI
    • ISBN
    Advanced Search
    JavaScript is disabled for your browser. Some features of this site may not work without it.

    Archive

    Influence of Fuel-Rich Combustion on the Accuracy of Turbine Speed Prediction in the Event of Shaft Failure

    Source: Journal of Aerospace Engineering:;2025:;Volume ( 038 ):;issue: 006::page 04025102-1
    Author:
    Guan, Yuxi
    ,
    Liu, Shuai
    ,
    Zhang, Shengqiu
    ,
    Bai, Jie
    DOI: 10.1061/JAEEEZ.ASENG-6202
    Publisher: American Society of Civil Engineers
    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 ...
    • Download: (2.190Mb)
    • Show Full MetaData Hide Full MetaData
    • Get RIS
    • Item Order
    • Go To Publisher
    • Statistics

      Influence of Fuel-Rich Combustion on the Accuracy of Turbine Speed Prediction in the Event of Shaft Failure

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/4314134
    Collections
    • Journal of Aerospace Engineering

    Show full item record

    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
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian
     
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian