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    Particle Image Velocimetry Measurements in a Two Pass 90 Degree Ribbed Wall Parallelogram Channel

    Source: Journal of Turbomachinery:;2015:;volume( 137 ):;issue: 004::page 41012
    Author:
    Liou, Tong
    ,
    Chang, Shyy
    ,
    Chan, Shu
    ,
    Liu, Yu
    DOI: 10.1115/1.4028739
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A parallelogram channel has drawn very little or no attention in the open literature although it appears as a crosssectional configuration of some gas turbine rotor blades. Particle image velocimetry (PIV) is presented of local flow structure in a twopass 90 deg ribbedwall parallelogram channel with a 180 deg sharp turn. The channel has a crosssectional equal length, 45.5 mm, of adjacent sides and two pairs of opposite angles are 45 deg and 135 deg. The rib height to channel height ratio is 0.1. All the measurements were performed at a fixed Reynolds number, characterized by channel hydraulic diameter of 32.17 mm and crosssectional bulk mean velocity, of 10,000 and a null rotating number. Results are discussed in terms of the distributions of streamwise and secondaryflow mean velocity vector, turbulent intensity, Reynolds stress, and turbulent kinetic energy of the cooling air. It is found that the flow is not periodically fully developed in pitchwise direction through the inline 90 deg ribbed straight inlet and outlet leg. Pitchwise variation of reattachment length is revealed, and comparison with reported values in square channels is made. Whether the 180 deg sharp turn induced separation bubble exists in the ribbed parallelogram channel is also documented. Moreover, the measured secondary flow results inside the turn are successively used to explain previous heat transfer trends.
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      Particle Image Velocimetry Measurements in a Two Pass 90 Degree Ribbed Wall Parallelogram Channel

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    contributor authorLiou, Tong
    contributor authorChang, Shyy
    contributor authorChan, Shu
    contributor authorLiu, Yu
    date accessioned2017-05-09T01:24:31Z
    date available2017-05-09T01:24:31Z
    date issued2015
    identifier issn0889-504X
    identifier otherturbo_137_04_041012.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/159915
    description abstractA parallelogram channel has drawn very little or no attention in the open literature although it appears as a crosssectional configuration of some gas turbine rotor blades. Particle image velocimetry (PIV) is presented of local flow structure in a twopass 90 deg ribbedwall parallelogram channel with a 180 deg sharp turn. The channel has a crosssectional equal length, 45.5 mm, of adjacent sides and two pairs of opposite angles are 45 deg and 135 deg. The rib height to channel height ratio is 0.1. All the measurements were performed at a fixed Reynolds number, characterized by channel hydraulic diameter of 32.17 mm and crosssectional bulk mean velocity, of 10,000 and a null rotating number. Results are discussed in terms of the distributions of streamwise and secondaryflow mean velocity vector, turbulent intensity, Reynolds stress, and turbulent kinetic energy of the cooling air. It is found that the flow is not periodically fully developed in pitchwise direction through the inline 90 deg ribbed straight inlet and outlet leg. Pitchwise variation of reattachment length is revealed, and comparison with reported values in square channels is made. Whether the 180 deg sharp turn induced separation bubble exists in the ribbed parallelogram channel is also documented. Moreover, the measured secondary flow results inside the turn are successively used to explain previous heat transfer trends.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleParticle Image Velocimetry Measurements in a Two Pass 90 Degree Ribbed Wall Parallelogram Channel
    typeJournal Paper
    journal volume137
    journal issue4
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.4028739
    journal fristpage41012
    journal lastpage41012
    identifier eissn1528-8900
    treeJournal of Turbomachinery:;2015:;volume( 137 ):;issue: 004
    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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