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    Influence of the Upstream Wakes on the Boundary Layer of a High-Lift Low-Pressure Turbine at Positive Incidence

    Source: Journal of Aerospace Engineering:;2020:;Volume ( 033 ):;issue: 006
    Author:
    Shuang Sun
    ,
    Tianrong Tan
    ,
    Xingshuang Wu
    ,
    Xingen Lu
    ,
    Yanfeng Zhang
    ,
    Junqiang Zhu
    DOI: 10.1061/(ASCE)AS.1943-5525.0001193
    Publisher: ASCE
    Abstract: The wake-induced transition, natural transition, and instability induced by the Klebanoff streaks complicate the transition process. In this paper, the boundary layer on the suction surface of a high-lift low-pressure turbine (LPT) was investigated at the design and +10° incidence with upstream wakes under numerical simulations and experiments. The interactions between the wakes and boundary on the leading edge of the blade at two incidences are mainly discussed. A positive incidence gives rise to an adverse pressure gradient (APG) over the forward suction surface. The adverse pressure gradient enhances the shear sheltering effect and, as a result, reduces penetration. However, strong Klebanoff streaks are amplified by the APG at +10° incidence and experience a weak viscous decay due to the moderately favorable pressure gradient (FPG). Between the wake passing events, weak Klebanoff streaks are also amplified by the APG at +10° incidence but barely amplified at 0° incidence. Klebanoff streaks appear almost in the whole wake passing cycle, resulting in an earlier transition onset and a longer transition process at +10° incidence.
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      Influence of the Upstream Wakes on the Boundary Layer of a High-Lift Low-Pressure Turbine at Positive Incidence

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4268831
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    contributor authorShuang Sun
    contributor authorTianrong Tan
    contributor authorXingshuang Wu
    contributor authorXingen Lu
    contributor authorYanfeng Zhang
    contributor authorJunqiang Zhu
    date accessioned2022-01-30T21:47:00Z
    date available2022-01-30T21:47:00Z
    date issued11/1/2020 12:00:00 AM
    identifier other%28ASCE%29AS.1943-5525.0001193.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4268831
    description abstractThe wake-induced transition, natural transition, and instability induced by the Klebanoff streaks complicate the transition process. In this paper, the boundary layer on the suction surface of a high-lift low-pressure turbine (LPT) was investigated at the design and +10° incidence with upstream wakes under numerical simulations and experiments. The interactions between the wakes and boundary on the leading edge of the blade at two incidences are mainly discussed. A positive incidence gives rise to an adverse pressure gradient (APG) over the forward suction surface. The adverse pressure gradient enhances the shear sheltering effect and, as a result, reduces penetration. However, strong Klebanoff streaks are amplified by the APG at +10° incidence and experience a weak viscous decay due to the moderately favorable pressure gradient (FPG). Between the wake passing events, weak Klebanoff streaks are also amplified by the APG at +10° incidence but barely amplified at 0° incidence. Klebanoff streaks appear almost in the whole wake passing cycle, resulting in an earlier transition onset and a longer transition process at +10° incidence.
    publisherASCE
    titleInfluence of the Upstream Wakes on the Boundary Layer of a High-Lift Low-Pressure Turbine at Positive Incidence
    typeJournal Paper
    journal volume33
    journal issue6
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)AS.1943-5525.0001193
    page13
    treeJournal of Aerospace Engineering:;2020:;Volume ( 033 ):;issue: 006
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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