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    The Effect of Tip Clearance on Fan Aeroelasticity Considering Acoustic Propagation Characteristics

    Source: Journal of Engineering for Gas Turbines and Power:;2025:;volume( 147 ):;issue: 011::page 111009-1
    Author:
    Jia, Xingbiao
    ,
    Dong, Xu
    ,
    Hong, Yansha
    ,
    Zhang, Yanfeng
    ,
    Lu, Xingen
    DOI: 10.1115/1.4068588
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Tip clearance is a critical parameter affecting fan performance and aeroelastic stability. This paper investigates the effect of tip clearance on fan aeroelasticity under different acoustic propagation characteristics through numerical simulations. Focusing on the first bending mode, which is most prone to flutter, the aeroelastic stability under various nodal diameters (ND) is studied using the energy method, with a detailed analysis of the 2 ND mode, which exhibits flutter risk. The study reveals that tip clearance does not alter the position of the most unstable nodal diameter. Under upstream and downstream cutoff mode and upstream cut-on mode, increasing tip clearance enhances aerodynamic damping, whereas under downstream cut-on mode, it reduces aerodynamic damping. The aerodynamic damping of the blade is jointly influenced by the flow field and acoustic propagation characteristics. The impact of the flow field is primarily concentrated near the leading edge of the pressure side at the blade tip, while the acoustic propagation characteristics significantly alter the phase of unsteady pressure, leading to notable changes in energy exchange characteristics. The study concludes that there is no optimal aeroelastic clearance, as the effect of clearance on aeroelasticity is closely related to acoustic propagation characteristics.
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      The Effect of Tip Clearance on Fan Aeroelasticity Considering Acoustic Propagation Characteristics

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4307953
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    contributor authorJia, Xingbiao
    contributor authorDong, Xu
    contributor authorHong, Yansha
    contributor authorZhang, Yanfeng
    contributor authorLu, Xingen
    date accessioned2025-08-20T09:14:07Z
    date available2025-08-20T09:14:07Z
    date copyright5/22/2025 12:00:00 AM
    date issued2025
    identifier issn0742-4795
    identifier othergtp_147_11_111009.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4307953
    description abstractTip clearance is a critical parameter affecting fan performance and aeroelastic stability. This paper investigates the effect of tip clearance on fan aeroelasticity under different acoustic propagation characteristics through numerical simulations. Focusing on the first bending mode, which is most prone to flutter, the aeroelastic stability under various nodal diameters (ND) is studied using the energy method, with a detailed analysis of the 2 ND mode, which exhibits flutter risk. The study reveals that tip clearance does not alter the position of the most unstable nodal diameter. Under upstream and downstream cutoff mode and upstream cut-on mode, increasing tip clearance enhances aerodynamic damping, whereas under downstream cut-on mode, it reduces aerodynamic damping. The aerodynamic damping of the blade is jointly influenced by the flow field and acoustic propagation characteristics. The impact of the flow field is primarily concentrated near the leading edge of the pressure side at the blade tip, while the acoustic propagation characteristics significantly alter the phase of unsteady pressure, leading to notable changes in energy exchange characteristics. The study concludes that there is no optimal aeroelastic clearance, as the effect of clearance on aeroelasticity is closely related to acoustic propagation characteristics.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleThe Effect of Tip Clearance on Fan Aeroelasticity Considering Acoustic Propagation Characteristics
    typeJournal Paper
    journal volume147
    journal issue11
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4068588
    journal fristpage111009-1
    journal lastpage111009-13
    page13
    treeJournal of Engineering for Gas Turbines and Power:;2025:;volume( 147 ):;issue: 011
    contenttypeFulltext
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