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    Local Heat Transfer and Flow Structure on and Above a Dimpled Surface in a Channel

    Source: Journal of Turbomachinery:;2001:;volume( 123 ):;issue: 001::page 115
    Author:
    G. I. Mahmood
    ,
    H.-K. Moon
    ,
    Consulting Engineer
    ,
    B. Glezer
    ,
    Head
    ,
    Turbine Cooling and Heat Transfer Analysis
    ,
    M. L. Hill
    ,
    D. L. Nelson
    ,
    P. M. Ligrani
    ,
    Professor.
    DOI: 10.1115/1.1333694
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Experimental results, measured on and above a dimpled test surface placed on one wall of a channel, are given for Reynolds numbers from 1250 to 61,500 and ratios of air inlet stagnation temperature to surface temperature ranging from 0.68 to 0.94. These include flow visualizations, surveys of time-averaged total pressure and streamwise velocity, and spatially resolved local Nusselt numbers, which are measured using infrared thermography, used in conjunction with energy balances, thermocouples, and in situ calibration procedures. The ratio of channel height to dimple print diameter is 0.5. Flow visualizations show vortical fluid and vortex pairs shed from the dimples, including a large upwash region and packets of fluid emanating from the central regions of each dimple, as well as vortex pairs and vortical fluid that form near dimple diagonals. These vortex structures augment local Nusselt numbers near the downstream rims of each dimple, both slightly within each depression, and especially on the flat surface just downstream of each dimple. Such augmentations are spread over larger surface areas and become more pronounced as the ratio of inlet stagnation temperature to local surface temperature decreases. As a result, local and spatially averaged heat transfer augmentations become larger as this temperature ratio decreases. This is due to the actions of vortical fluid in advecting cool fluid from the central parts of the channel to regions close to the hotter dimpled surface.
    keyword(s): Flow (Dynamics) , Temperature , Heat transfer , Fluids , Channels (Hydraulic engineering) , Reynolds number , Vortices , Flow visualization AND Pressure ,
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      Local Heat Transfer and Flow Structure on and Above a Dimpled Surface in a Channel

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    http://yetl.yabesh.ir/yetl1/handle/yetl/126087
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    contributor authorG. I. Mahmood
    contributor authorH.-K. Moon
    contributor authorConsulting Engineer
    contributor authorB. Glezer
    contributor authorHead
    contributor authorTurbine Cooling and Heat Transfer Analysis
    contributor authorM. L. Hill
    contributor authorD. L. Nelson
    contributor authorP. M. Ligrani
    contributor authorProfessor.
    date accessioned2017-05-09T00:06:20Z
    date available2017-05-09T00:06:20Z
    date copyrightJanuary, 2001
    date issued2001
    identifier issn0889-504X
    identifier otherJOTUEI-28686#115_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/126087
    description abstractExperimental results, measured on and above a dimpled test surface placed on one wall of a channel, are given for Reynolds numbers from 1250 to 61,500 and ratios of air inlet stagnation temperature to surface temperature ranging from 0.68 to 0.94. These include flow visualizations, surveys of time-averaged total pressure and streamwise velocity, and spatially resolved local Nusselt numbers, which are measured using infrared thermography, used in conjunction with energy balances, thermocouples, and in situ calibration procedures. The ratio of channel height to dimple print diameter is 0.5. Flow visualizations show vortical fluid and vortex pairs shed from the dimples, including a large upwash region and packets of fluid emanating from the central regions of each dimple, as well as vortex pairs and vortical fluid that form near dimple diagonals. These vortex structures augment local Nusselt numbers near the downstream rims of each dimple, both slightly within each depression, and especially on the flat surface just downstream of each dimple. Such augmentations are spread over larger surface areas and become more pronounced as the ratio of inlet stagnation temperature to local surface temperature decreases. As a result, local and spatially averaged heat transfer augmentations become larger as this temperature ratio decreases. This is due to the actions of vortical fluid in advecting cool fluid from the central parts of the channel to regions close to the hotter dimpled surface.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleLocal Heat Transfer and Flow Structure on and Above a Dimpled Surface in a Channel
    typeJournal Paper
    journal volume123
    journal issue1
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.1333694
    journal fristpage115
    journal lastpage123
    identifier eissn1528-8900
    keywordsFlow (Dynamics)
    keywordsTemperature
    keywordsHeat transfer
    keywordsFluids
    keywordsChannels (Hydraulic engineering)
    keywordsReynolds number
    keywordsVortices
    keywordsFlow visualization AND Pressure
    treeJournal of Turbomachinery:;2001:;volume( 123 ):;issue: 001
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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