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    Comparison of Film Effectiveness and Cooling Uniformity of Conical and Cylindrical-Shaped Film Hole With Coolant-Exit Temperature Correction

    Source: Journal of Thermal Science and Engineering Applications:;2011:;volume( 003 ):;issue: 003::page 31011
    Author:
    Cuong Q. Nguyen
    ,
    Perry L. Johnson
    ,
    Bryan C. Bernier
    ,
    Son H. Ho
    ,
    Jayanta S. Kapat
    DOI: 10.1115/1.4003886
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Data from conical-shaped film cooling holes are extremely sparse in open literature, especially the cooling uniformity characteristic, an important criterion for evaluating any film cooling design. The authors will compare the performance of conical-shaped holes to cylindrical-shaped holes. Cylindrical-shaped holes are often considered a baseline in terms of film cooling effectiveness and cooling uniformity coefficient. The authors will study two coupons with conical-shaped holes, which have 3° and 6° diffusion angles, named CON3 and CON6, respectively. A conjugate heat transfer computational fluid dynamics model and an experimental wind tunnel will be used to study these coupons. The three configurations: cylindrical baseline, CON3, and CON6, have a single row of holes with an inlet metering diameter of 3 mm, length-to-nominal diameter of 4.3, and an injection angle of 30°. In this study, the authors will also take into account the heat transfer into the coolant flow from the coolant channel. In other words, the coolant temperature at the exit of the coolant hole will be different than that measured at the inlet, and the conjugate heat transfer model will be used to correct for this difference. For the numerical model, the realizable k-ɛ turbulent model will be applied with a second order of discretization and an enhanced wall treatment to provide the highest accuracy available. Grid independent studies for both cylindrical-shaped film cooling holes and conical-shaped holes will be performed, and the results will be compared to data in open literature as well as in-house experimental data. Results show that conical-shaped holes considerably outperform cylindrical-shaped holes in film cooling effectiveness at all blowing ratios. In terms of cooling uniformity, conical-shaped holes perform better than cylindrical-shaped holes for low- and midrange blowing ratios, but not at higher levels.
    keyword(s): Flow (Dynamics) , Temperature , Cooling , Coolants , Turbulence AND Heat transfer ,
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      Comparison of Film Effectiveness and Cooling Uniformity of Conical and Cylindrical-Shaped Film Hole With Coolant-Exit Temperature Correction

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    https://yetl.yabesh.ir/yetl1/handle/yetl/147637
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    contributor authorCuong Q. Nguyen
    contributor authorPerry L. Johnson
    contributor authorBryan C. Bernier
    contributor authorSon H. Ho
    contributor authorJayanta S. Kapat
    date accessioned2017-05-09T00:47:01Z
    date available2017-05-09T00:47:01Z
    date copyrightSeptember, 2011
    date issued2011
    identifier issn1948-5085
    identifier otherJTSEBV-28833#031011_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/147637
    description abstractData from conical-shaped film cooling holes are extremely sparse in open literature, especially the cooling uniformity characteristic, an important criterion for evaluating any film cooling design. The authors will compare the performance of conical-shaped holes to cylindrical-shaped holes. Cylindrical-shaped holes are often considered a baseline in terms of film cooling effectiveness and cooling uniformity coefficient. The authors will study two coupons with conical-shaped holes, which have 3° and 6° diffusion angles, named CON3 and CON6, respectively. A conjugate heat transfer computational fluid dynamics model and an experimental wind tunnel will be used to study these coupons. The three configurations: cylindrical baseline, CON3, and CON6, have a single row of holes with an inlet metering diameter of 3 mm, length-to-nominal diameter of 4.3, and an injection angle of 30°. In this study, the authors will also take into account the heat transfer into the coolant flow from the coolant channel. In other words, the coolant temperature at the exit of the coolant hole will be different than that measured at the inlet, and the conjugate heat transfer model will be used to correct for this difference. For the numerical model, the realizable k-ɛ turbulent model will be applied with a second order of discretization and an enhanced wall treatment to provide the highest accuracy available. Grid independent studies for both cylindrical-shaped film cooling holes and conical-shaped holes will be performed, and the results will be compared to data in open literature as well as in-house experimental data. Results show that conical-shaped holes considerably outperform cylindrical-shaped holes in film cooling effectiveness at all blowing ratios. In terms of cooling uniformity, conical-shaped holes perform better than cylindrical-shaped holes for low- and midrange blowing ratios, but not at higher levels.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleComparison of Film Effectiveness and Cooling Uniformity of Conical and Cylindrical-Shaped Film Hole With Coolant-Exit Temperature Correction
    typeJournal Paper
    journal volume3
    journal issue3
    journal titleJournal of Thermal Science and Engineering Applications
    identifier doi10.1115/1.4003886
    journal fristpage31011
    identifier eissn1948-5093
    keywordsFlow (Dynamics)
    keywordsTemperature
    keywordsCooling
    keywordsCoolants
    keywordsTurbulence AND Heat transfer
    treeJournal of Thermal Science and Engineering Applications:;2011:;volume( 003 ):;issue: 003
    contenttypeFulltext
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