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    Rib Heat Transfer Coefficient Measurements in a Rib-Roughened Square Passage

    Source: Journal of Turbomachinery:;1998:;volume( 120 ):;issue: 002::page 376
    Author:
    G. J. Korotky
    ,
    M. E. Taslim
    DOI: 10.1115/1.2841416
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Three staggered 90 deg rib geometries corresponding to blockage ratios of 0.133, 0.167, and 0.25 were tested 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 ribs with rounded corners and those with sharp corners, 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 of the passage wall 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. For the sharp-corner ribs, the rib average heat transfer coefficient increased with blockage ratio. However, when the corners were rounded, the trend depended on the level of roundness. (b) High-blockage-ratio (e/Dh = 0.25) ribs were insensitive to the pitch-to-height ratio. For the other two blockage ratios, the pitch-to-height ratio of 5 produced the lowest heat transfer coefficient. Results of the other two pitch-to-height ratios were very close, with the results of S/e = 10 slightly higher than those of S/e = 8.5. (c) Under otherwise identical conditions, ribs in the furthest upstream position produced lower heat transfer coefficients for all cases except that of the smallest blockage ratio with S/e of 5. In that position, for the rib geometries tested, while the sharp-corner rib average heat transfer coefficients increased with the blockage ratio, the trend of the round-corner ribs depended on the level of roundness, r/e. (d) Thermal performance decreased with the blockage ratio. While the smallest rib geometry at a pitch-to-height ratio of 10 had the highest thermal performance, thermal performance of high blockage ribs at a pitch-to-height ratio of 5 was the lowest. (e) The general effects of rounding were a decrease in heat transfer coefficient for the midstream ribs and an increase in heat transfer coefficient for ribs in the furthest upstream position.
    keyword(s): Measurement , Heat transfer coefficients , Corners (Structural elements) , Boundary-value problems , Geometry , Friction AND Channels (Hydraulic engineering) ,
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      Rib Heat Transfer Coefficient Measurements in a Rib-Roughened Square Passage

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/121341
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    • Journal of Turbomachinery

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    contributor authorG. J. Korotky
    contributor authorM. E. Taslim
    date accessioned2017-05-08T23:58:13Z
    date available2017-05-08T23:58:13Z
    date copyrightApril, 1998
    date issued1998
    identifier issn0889-504X
    identifier otherJOTUEI-28665#376_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/121341
    description abstractThree staggered 90 deg rib geometries corresponding to blockage ratios of 0.133, 0.167, and 0.25 were tested 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 ribs with rounded corners and those with sharp corners, 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 of the passage wall 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. For the sharp-corner ribs, the rib average heat transfer coefficient increased with blockage ratio. However, when the corners were rounded, the trend depended on the level of roundness. (b) High-blockage-ratio (e/Dh = 0.25) ribs were insensitive to the pitch-to-height ratio. For the other two blockage ratios, the pitch-to-height ratio of 5 produced the lowest heat transfer coefficient. Results of the other two pitch-to-height ratios were very close, with the results of S/e = 10 slightly higher than those of S/e = 8.5. (c) Under otherwise identical conditions, ribs in the furthest upstream position produced lower heat transfer coefficients for all cases except that of the smallest blockage ratio with S/e of 5. In that position, for the rib geometries tested, while the sharp-corner rib average heat transfer coefficients increased with the blockage ratio, the trend of the round-corner ribs depended on the level of roundness, r/e. (d) Thermal performance decreased with the blockage ratio. While the smallest rib geometry at a pitch-to-height ratio of 10 had the highest thermal performance, thermal performance of high blockage ribs at a pitch-to-height ratio of 5 was the lowest. (e) The general effects of rounding were a decrease in heat transfer coefficient for the midstream ribs and an increase in heat transfer coefficient for ribs in the furthest upstream position.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleRib Heat Transfer Coefficient Measurements in a Rib-Roughened Square Passage
    typeJournal Paper
    journal volume120
    journal issue2
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2841416
    journal fristpage376
    journal lastpage385
    identifier eissn1528-8900
    keywordsMeasurement
    keywordsHeat transfer coefficients
    keywordsCorners (Structural elements)
    keywordsBoundary-value problems
    keywordsGeometry
    keywordsFriction AND Channels (Hydraulic engineering)
    treeJournal of Turbomachinery:;1998:;volume( 120 ):;issue: 002
    contenttypeFulltext
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