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    Improved Accuracy in Jet Impingement Heat Transfer Experiments Considering the Layer Thicknesses of a Triple Thermochromic Liquid Crystal Coating

    Source: Journal of Turbomachinery:;2016:;volume( 138 ):;issue: 002::page 21003
    Author:
    Terzis, Alexandros
    ,
    Bontitsopoulos, Stavros
    ,
    Ott, Peter
    ,
    von Wolfersdorf, Jens
    ,
    Kalfas, Anestis I.
    DOI: 10.1115/1.4031786
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper examines the applicability of a triple layer of thermochromic liquid crystals (TLCs) for the determination of local heat transfer coefficients using the transient liquid crystal (LC) technique. The experiments were carried out in a narrow impingement channel, typically used for turbine blade cooling applications. Three types of narrow bandwidth LCs (1 آ°C range) of 35 آ°C, 38 آ°C, and 41 آ°C were individually painted on the target plate of the cooling cavity and the overall paint thickness was accurately determined with an integral coating thickness gauge. The 1D transient heat conduction equation is then implicitly solved for each individual TLC layer on its realistic depth on the painted surface. Local heat transfer coefficients are therefore calculated three times for the same location in the flow improving the measurement accuracy, especially at regions where the LC detection times are too short (stagnation points) or too long (walljet regions). The results indicate that if multiple LC layers are used and the paint thickness is not considered, the heat transfer coefficients can be significantly underestimated.
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      Improved Accuracy in Jet Impingement Heat Transfer Experiments Considering the Layer Thicknesses of a Triple Thermochromic Liquid Crystal Coating

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    http://yetl.yabesh.ir/yetl1/handle/yetl/162737
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    contributor authorTerzis, Alexandros
    contributor authorBontitsopoulos, Stavros
    contributor authorOtt, Peter
    contributor authorvon Wolfersdorf, Jens
    contributor authorKalfas, Anestis I.
    date accessioned2017-05-09T01:34:01Z
    date available2017-05-09T01:34:01Z
    date issued2016
    identifier issn0889-504X
    identifier otherturbo_138_02_021003.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/162737
    description abstractThis paper examines the applicability of a triple layer of thermochromic liquid crystals (TLCs) for the determination of local heat transfer coefficients using the transient liquid crystal (LC) technique. The experiments were carried out in a narrow impingement channel, typically used for turbine blade cooling applications. Three types of narrow bandwidth LCs (1 آ°C range) of 35 آ°C, 38 آ°C, and 41 آ°C were individually painted on the target plate of the cooling cavity and the overall paint thickness was accurately determined with an integral coating thickness gauge. The 1D transient heat conduction equation is then implicitly solved for each individual TLC layer on its realistic depth on the painted surface. Local heat transfer coefficients are therefore calculated three times for the same location in the flow improving the measurement accuracy, especially at regions where the LC detection times are too short (stagnation points) or too long (walljet regions). The results indicate that if multiple LC layers are used and the paint thickness is not considered, the heat transfer coefficients can be significantly underestimated.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleImproved Accuracy in Jet Impingement Heat Transfer Experiments Considering the Layer Thicknesses of a Triple Thermochromic Liquid Crystal Coating
    typeJournal Paper
    journal volume138
    journal issue2
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.4031786
    journal fristpage21003
    journal lastpage21003
    identifier eissn1528-8900
    treeJournal of Turbomachinery:;2016:;volume( 138 ):;issue: 002
    contenttypeFulltext
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