YaBeSH Engineering and Technology Library

    • Journals
    • PaperQuest
    • YSE Standards
    • YaBeSH
    • Login
    View Item 
    •   YE&T Library
    • ASME
    • Journal of Turbomachinery
    • View Item
    •   YE&T Library
    • ASME
    • Journal of Turbomachinery
    • View Item
    • All Fields
    • Source Title
    • Year
    • Publisher
    • Title
    • Subject
    • Author
    • DOI
    • ISBN
    Advanced Search
    JavaScript is disabled for your browser. Some features of this site may not work without it.

    Archive

    Heat Transfer Enhancement Using a Convex-Patterned Surface

    Source: Journal of Turbomachinery:;2003:;volume( 125 ):;issue: 002::page 274
    Author:
    H. K. Moon
    ,
    T. O’Connell
    ,
    R. Sharma
    DOI: 10.1115/1.1556404
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The heat transfer rate from a smooth wall in an internal cooling passage can be significantly enhanced by using a convex patterned surface on the opposite wall of the passage. This design is particularly effective for a design that requires the heat transfer surface to be free of any augmenting features (smooth). Heat transfer coefficients on the smooth wall in a rectangular channel, which had convexities on the opposite wall were experimentally investigated. Friction factors were also measured to assess the thermal performance. Relative clearances (δ/d) between the convexities and the smooth wall of 0, 0.024, and 0.055 were investigated in a Reynolds number (ReHD) range from 15,000 to 35,000. The heat transfer coefficients were measured in the thermally developed region using a transient thermochromic liquid crystal technique. The clearance gap between the convexities and the smooth wall adversely affected the heat transfer enhancement (NuHD). The friction factors (f ), measured in the aerodynamically developed region, were largest for the cases of no clearance (δ/d)=0). The average heat transfer enhancement (NuHD) was also largest for the cases of no clearance (δ/d=0), as high as 3.08 times at a Reynolds number of 11,456 in relative to that (Nuo) of an entirely smooth channel. The normalized Nusselt numbers (NuHD/Nuo), as well as the normalized friction factors (f/fo), for all three cases, decreased with Reynolds numbers. However, the decay rate of the friction factor ratios (f/fo) with Reynolds numbers was lower than that of the normalized Nusselt numbers. For all three cases investigated, the thermal performance ((NuHD/Nuo)/(f/fo)1/3) values were within 5% to each other. The heat transfer enhancement using a convex patterned surface was thermally more effective at a relative low Reynolds numbers (less than 20,000 for δ/d=0) than that of a smooth channel.
    keyword(s): Heat transfer , Channels (Hydraulic engineering) , Reynolds number , Clearances (Engineering) , Heat transfer coefficients , Friction , Flow (Dynamics) AND Cooling ,
    • Download: (606.1Kb)
    • Show Full MetaData Hide Full MetaData
    • Get RIS
    • Item Order
    • Go To Publisher
    • Price: 5000 Rial
    • Statistics

      Heat Transfer Enhancement Using a Convex-Patterned Surface

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/129268
    Collections
    • Journal of Turbomachinery

    Show full item record

    contributor authorH. K. Moon
    contributor authorT. O’Connell
    contributor authorR. Sharma
    date accessioned2017-05-09T00:11:42Z
    date available2017-05-09T00:11:42Z
    date copyrightApril, 2003
    date issued2003
    identifier issn0889-504X
    identifier otherJOTUEI-28702#274_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/129268
    description abstractThe heat transfer rate from a smooth wall in an internal cooling passage can be significantly enhanced by using a convex patterned surface on the opposite wall of the passage. This design is particularly effective for a design that requires the heat transfer surface to be free of any augmenting features (smooth). Heat transfer coefficients on the smooth wall in a rectangular channel, which had convexities on the opposite wall were experimentally investigated. Friction factors were also measured to assess the thermal performance. Relative clearances (δ/d) between the convexities and the smooth wall of 0, 0.024, and 0.055 were investigated in a Reynolds number (ReHD) range from 15,000 to 35,000. The heat transfer coefficients were measured in the thermally developed region using a transient thermochromic liquid crystal technique. The clearance gap between the convexities and the smooth wall adversely affected the heat transfer enhancement (NuHD). The friction factors (f ), measured in the aerodynamically developed region, were largest for the cases of no clearance (δ/d)=0). The average heat transfer enhancement (NuHD) was also largest for the cases of no clearance (δ/d=0), as high as 3.08 times at a Reynolds number of 11,456 in relative to that (Nuo) of an entirely smooth channel. The normalized Nusselt numbers (NuHD/Nuo), as well as the normalized friction factors (f/fo), for all three cases, decreased with Reynolds numbers. However, the decay rate of the friction factor ratios (f/fo) with Reynolds numbers was lower than that of the normalized Nusselt numbers. For all three cases investigated, the thermal performance ((NuHD/Nuo)/(f/fo)1/3) values were within 5% to each other. The heat transfer enhancement using a convex patterned surface was thermally more effective at a relative low Reynolds numbers (less than 20,000 for δ/d=0) than that of a smooth channel.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleHeat Transfer Enhancement Using a Convex-Patterned Surface
    typeJournal Paper
    journal volume125
    journal issue2
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.1556404
    journal fristpage274
    journal lastpage280
    identifier eissn1528-8900
    keywordsHeat transfer
    keywordsChannels (Hydraulic engineering)
    keywordsReynolds number
    keywordsClearances (Engineering)
    keywordsHeat transfer coefficients
    keywordsFriction
    keywordsFlow (Dynamics) AND Cooling
    treeJournal of Turbomachinery:;2003:;volume( 125 ):;issue: 002
    contenttypeFulltext
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian
     
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian