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    Study of Time Resolved Vortex Structure of In Cylinder Engine Flow Fields Using Proper Orthogonal Decomposition Technique

    Source: Journal of Engineering for Gas Turbines and Power:;2015:;volume( 137 ):;issue: 008::page 82604
    Author:
    Zhuang, Hanyang
    ,
    Hung, David L.S.
    ,
    Chen, Hao
    DOI: 10.1115/1.4029600
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The structure of incylinder flow field makes significant impacts on the processes of fuel injection, air–fuel interactions, and flame development in internal combustion engines. In this study, the implementation of timeresolved particle image velocimetry (PIV) in an optical engine is presented. Flow field PIV images at different crank angles have been taken using a highspeed doublepulsed laser and a highspeed camera with seeding particles mixed with the intake air. This study is focused on measuring the flow fields on the swirl plane at 30 mm below the injector tip under various intake air swirl ratios. A simple algorithm is developed to identify the vortex structure and to track the location and motion of vortex center at different crank angles. Proper orthogonal decomposition (POD) has been used to extract the ensemble and variation information of the vortex structure. Experimental results reveal that strong cycletocycle variations exist in almost all test conditions. The vortex center is difficult to identify since multiple, but small scale, vortices exist during the early stage of the intake stroke. However, during the compression stroke when only one vortex center exists in most cycles, the motion of vortex center is found to be quite similar at different intake swirl ratios and engine speeds. This is due to the dominant driving force exerted by the piston’s upward motion on the incylinder air.
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      Study of Time Resolved Vortex Structure of In Cylinder Engine Flow Fields Using Proper Orthogonal Decomposition Technique

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    http://yetl.yabesh.ir/yetl1/handle/yetl/158020
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    contributor authorZhuang, Hanyang
    contributor authorHung, David L.S.
    contributor authorChen, Hao
    date accessioned2017-05-09T01:18:07Z
    date available2017-05-09T01:18:07Z
    date issued2015
    identifier issn1528-8919
    identifier othergtp_137_08_082604.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/158020
    description abstractThe structure of incylinder flow field makes significant impacts on the processes of fuel injection, air–fuel interactions, and flame development in internal combustion engines. In this study, the implementation of timeresolved particle image velocimetry (PIV) in an optical engine is presented. Flow field PIV images at different crank angles have been taken using a highspeed doublepulsed laser and a highspeed camera with seeding particles mixed with the intake air. This study is focused on measuring the flow fields on the swirl plane at 30 mm below the injector tip under various intake air swirl ratios. A simple algorithm is developed to identify the vortex structure and to track the location and motion of vortex center at different crank angles. Proper orthogonal decomposition (POD) has been used to extract the ensemble and variation information of the vortex structure. Experimental results reveal that strong cycletocycle variations exist in almost all test conditions. The vortex center is difficult to identify since multiple, but small scale, vortices exist during the early stage of the intake stroke. However, during the compression stroke when only one vortex center exists in most cycles, the motion of vortex center is found to be quite similar at different intake swirl ratios and engine speeds. This is due to the dominant driving force exerted by the piston’s upward motion on the incylinder air.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleStudy of Time Resolved Vortex Structure of In Cylinder Engine Flow Fields Using Proper Orthogonal Decomposition Technique
    typeJournal Paper
    journal volume137
    journal issue8
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4029600
    journal fristpage82604
    journal lastpage82604
    identifier eissn0742-4795
    treeJournal of Engineering for Gas Turbines and Power:;2015:;volume( 137 ):;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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