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    45 deg Staggered Rib Heat Transfer Coefficient Measurements in a Square Channel

    Source: Journal of Turbomachinery:;1998:;volume( 120 ):;issue: 003::page 571
    Author:
    M. E. Taslim
    ,
    A. Lengkong
    DOI: 10.1115/1.2841755
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: For high-blockage ribs with large heat transfer areas, commonly used in small gas turbine blades, the rib heat transfer is a significant portion of the overall heat transfer in the cooling passages. Three staggered 45 deg rib geometries corresponding to blockage ratios of 0.133, 0.167, and 0.25 were tested in a square channel for pitch-to-height ratios of 5, 8.5, and 10, and for two distinct thermal boundary conditions of heated and unheated channel walls. Comparisons were made between the surface-averaged heat transfer coefficients and friction factors for 45 deg ribs, and 90 deg ribs reported previously. Heat transfer coefficients of the furthest upstream rib and that of a typical rib located in the middle of the rib-roughened region were also compared. It was concluded that: (a) For the geometries tested, the rib average heat transfer coefficient was much higher than that for the area between the ribs. (b) Except for two cases corresponding to the highest blockage ribs mounted at pitch-to-height ratios of 8.5 and 10 for which the heat transfer results of 45 deg ribs were very close to those of 90 deg ribs, 45 deg ribs produced higher heat transfer coefficients than 90 deg ribs. (c) At pitch-to-height ratios of 8.5 and 10, all 45 deg ribs produced lower friction factors than 90 deg ribs. However, when they were brought closer to each other (S/e = 5), they produced higher friction factors than 90 deg ribs. (d) Heat transfer coefficients for the two smaller rib geometries (e/Dh = 0.133 and 0.167) did not vary significantly with the pitch-to-height ratio in the range tested. However, the heat transfer coefficient for the high blockage rib geometry increased significantly as the ribs were brought closer to each other. (e) Under otherwise identical conditions, ribs in the furthest upstream position produced lower heat transfer coefficients than those in the midstream position. (f) Rib thermal performance decreased with the rib blockage ratio. For both angles of attack, the smallest rib geometry in the midstream position and at a pitch-to-height ratio of 10 had the highest thermal performance, and the highest blockage rib in the furthest upstream position produced the lowest thermal performance.
    keyword(s): Channels (Hydraulic engineering) , Measurement , Heat transfer coefficients , Heat transfer , Friction , Geometry , Cooling , Gas turbines , Blades AND Boundary-value problems ,
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      45 deg Staggered Rib Heat Transfer Coefficient Measurements in a Square Channel

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/121313
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    • Journal of Turbomachinery

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    contributor authorM. E. Taslim
    contributor authorA. Lengkong
    date accessioned2017-05-08T23:58:11Z
    date available2017-05-08T23:58:11Z
    date copyrightJuly, 1998
    date issued1998
    identifier issn0889-504X
    identifier otherJOTUEI-28666#571_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/121313
    description abstractFor high-blockage ribs with large heat transfer areas, commonly used in small gas turbine blades, the rib heat transfer is a significant portion of the overall heat transfer in the cooling passages. Three staggered 45 deg rib geometries corresponding to blockage ratios of 0.133, 0.167, and 0.25 were tested in a square channel for pitch-to-height ratios of 5, 8.5, and 10, and for two distinct thermal boundary conditions of heated and unheated channel walls. Comparisons were made between the surface-averaged heat transfer coefficients and friction factors for 45 deg ribs, and 90 deg ribs reported previously. Heat transfer coefficients of the furthest upstream rib and that of a typical rib located in the middle of the rib-roughened region were also compared. It was concluded that: (a) For the geometries tested, the rib average heat transfer coefficient was much higher than that for the area between the ribs. (b) Except for two cases corresponding to the highest blockage ribs mounted at pitch-to-height ratios of 8.5 and 10 for which the heat transfer results of 45 deg ribs were very close to those of 90 deg ribs, 45 deg ribs produced higher heat transfer coefficients than 90 deg ribs. (c) At pitch-to-height ratios of 8.5 and 10, all 45 deg ribs produced lower friction factors than 90 deg ribs. However, when they were brought closer to each other (S/e = 5), they produced higher friction factors than 90 deg ribs. (d) Heat transfer coefficients for the two smaller rib geometries (e/Dh = 0.133 and 0.167) did not vary significantly with the pitch-to-height ratio in the range tested. However, the heat transfer coefficient for the high blockage rib geometry increased significantly as the ribs were brought closer to each other. (e) Under otherwise identical conditions, ribs in the furthest upstream position produced lower heat transfer coefficients than those in the midstream position. (f) Rib thermal performance decreased with the rib blockage ratio. For both angles of attack, the smallest rib geometry in the midstream position and at a pitch-to-height ratio of 10 had the highest thermal performance, and the highest blockage rib in the furthest upstream position produced the lowest thermal performance.
    publisherThe American Society of Mechanical Engineers (ASME)
    title45 deg Staggered Rib Heat Transfer Coefficient Measurements in a Square Channel
    typeJournal Paper
    journal volume120
    journal issue3
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2841755
    journal fristpage571
    journal lastpage580
    identifier eissn1528-8900
    keywordsChannels (Hydraulic engineering)
    keywordsMeasurement
    keywordsHeat transfer coefficients
    keywordsHeat transfer
    keywordsFriction
    keywordsGeometry
    keywordsCooling
    keywordsGas turbines
    keywordsBlades AND Boundary-value problems
    treeJournal of Turbomachinery:;1998:;volume( 120 ):;issue: 003
    contenttypeFulltext
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