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    Effect of Thermal Barrier Coating and Gas Radiation on Film Cooling of a Corrugated Surface

    Source: Journal of Heat Transfer:;2018:;volume( 140 ):;issue: 009::page 94504
    Author:
    Singh, Kuldeep
    ,
    Premachandran, B.
    ,
    Ravi, M. R.
    DOI: 10.1115/1.4039761
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In this work, a numerical study is conducted to investigate film cooling of a corrugated surface. A conjugate heat transfer analysis is carried out, accounting for the presence of thermal barrier coating (TBC) and gas radiation. The Mach number of mainstream flow is maintained at Ma = 0.6, while cold stream Mach number is varied from 0.3 to 0.58, and density ratio is kept 4. From this study, it is observed that the overall film cooling effectiveness increases by a value ranging from 0.10 to 0.15 with the use of TBC. The hot side metallic wall temperature increases in the range of 100–150 °C when the effect of gas radiation is considered. It is also found that the film cooling effectiveness decreases with decrease in the cold side Mach number.
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      Effect of Thermal Barrier Coating and Gas Radiation on Film Cooling of a Corrugated Surface

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4251843
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    contributor authorSingh, Kuldeep
    contributor authorPremachandran, B.
    contributor authorRavi, M. R.
    date accessioned2019-02-28T11:01:31Z
    date available2019-02-28T11:01:31Z
    date copyright5/25/2018 12:00:00 AM
    date issued2018
    identifier issn0022-1481
    identifier otherht_140_09_094504.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4251843
    description abstractIn this work, a numerical study is conducted to investigate film cooling of a corrugated surface. A conjugate heat transfer analysis is carried out, accounting for the presence of thermal barrier coating (TBC) and gas radiation. The Mach number of mainstream flow is maintained at Ma = 0.6, while cold stream Mach number is varied from 0.3 to 0.58, and density ratio is kept 4. From this study, it is observed that the overall film cooling effectiveness increases by a value ranging from 0.10 to 0.15 with the use of TBC. The hot side metallic wall temperature increases in the range of 100–150 °C when the effect of gas radiation is considered. It is also found that the film cooling effectiveness decreases with decrease in the cold side Mach number.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleEffect of Thermal Barrier Coating and Gas Radiation on Film Cooling of a Corrugated Surface
    typeJournal Paper
    journal volume140
    journal issue9
    journal titleJournal of Heat Transfer
    identifier doi10.1115/1.4039761
    journal fristpage94504
    journal lastpage094504-5
    treeJournal of Heat Transfer:;2018:;volume( 140 ):;issue: 009
    contenttypeFulltext
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