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    Investigation of the Boundary Layer Flow Under Engine-Like Conditions Using Particle Image Velocimetry

    Source: Journal of Engineering for Gas Turbines and Power:;2019:;volume( 141 ):;issue: 008::page 82801
    Author:
    Liu, Daming
    ,
    Wang, Tianyou
    ,
    Jia, Ming
    ,
    Li, Wei
    ,
    Lu, Zhen
    ,
    Zhen, Xudong
    DOI: 10.1115/1.4043444
    Publisher: American Society of Mechanical Engineers (ASME)
    Abstract: The turbulent boundary layer flow in internal combustion (IC) engines has a significant effect on the in-cylinder flow and the wall heat transfer. A detailed analysis of the in-cylinder near-wall flow was carried out on an optical steady flow test bench by using high-resolution particle image velocimetry (PIV) in order to characterize the in-cylinder boundary layer flow in this study. The difference between the in-cylinder boundary layer and the canonical turbulent boundary layer was analyzed. The experimental results show that small-scale vortices with a length scale of about 1–2 mm in the instantaneous flow fields appeared in the wall jet region due to the entrainment of the free jet in the outer region of the wall jet. The viscous sublayer thickness decreased from 0.5 mm to 0.3 mm as the valve lift increased from 2.32 mm to 7.975 mm and the pressure drop from 0.5 kPa to 1 kPa. The dimensionless velocity profile is in good agreement with the law of the wall in the viscous sublayer. However, no obvious logarithmic law distribution region was observed in the logarithmic layer. The distribution of the Reynolds stress and the turbulent kinetic energy is similar to that of the canonical turbulent boundary layer. But the Reynolds stress had a much larger magnitude because the turbulent velocity measured in this boundary layer included not only the turbulence generated by wall shear but also the large-scale turbulent vortices caused by the wall jet.
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      Investigation of the Boundary Layer Flow Under Engine-Like Conditions Using Particle Image Velocimetry

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4259234
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorLiu, Daming
    contributor authorWang, Tianyou
    contributor authorJia, Ming
    contributor authorLi, Wei
    contributor authorLu, Zhen
    contributor authorZhen, Xudong
    date accessioned2019-09-18T09:07:59Z
    date available2019-09-18T09:07:59Z
    date copyright4/25/2019 12:00:00 AM
    date issued2019
    identifier issn0742-4795
    identifier othergtp_141_08_082801
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4259234
    description abstractThe turbulent boundary layer flow in internal combustion (IC) engines has a significant effect on the in-cylinder flow and the wall heat transfer. A detailed analysis of the in-cylinder near-wall flow was carried out on an optical steady flow test bench by using high-resolution particle image velocimetry (PIV) in order to characterize the in-cylinder boundary layer flow in this study. The difference between the in-cylinder boundary layer and the canonical turbulent boundary layer was analyzed. The experimental results show that small-scale vortices with a length scale of about 1–2 mm in the instantaneous flow fields appeared in the wall jet region due to the entrainment of the free jet in the outer region of the wall jet. The viscous sublayer thickness decreased from 0.5 mm to 0.3 mm as the valve lift increased from 2.32 mm to 7.975 mm and the pressure drop from 0.5 kPa to 1 kPa. The dimensionless velocity profile is in good agreement with the law of the wall in the viscous sublayer. However, no obvious logarithmic law distribution region was observed in the logarithmic layer. The distribution of the Reynolds stress and the turbulent kinetic energy is similar to that of the canonical turbulent boundary layer. But the Reynolds stress had a much larger magnitude because the turbulent velocity measured in this boundary layer included not only the turbulence generated by wall shear but also the large-scale turbulent vortices caused by the wall jet.
    publisherAmerican Society of Mechanical Engineers (ASME)
    titleInvestigation of the Boundary Layer Flow Under Engine-Like Conditions Using Particle Image Velocimetry
    typeJournal Paper
    journal volume141
    journal issue8
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4043444
    journal fristpage82801
    journal lastpage082801-16
    treeJournal of Engineering for Gas Turbines and Power:;2019:;volume( 141 ):;issue: 008
    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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