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

    Manufacturing Influences on Pressure Losses of Channel Fed Holes

    Source: Journal of Turbomachinery:;2014:;volume( 136 ):;issue: 005::page 51012
    Author:
    Barringer, Michael
    ,
    Thole, Karen A.
    ,
    Krishnan, Vaidyanathan
    ,
    Landrum, Evan
    DOI: 10.1115/1.4025226
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Variations from manufacturing can influence the overall pressure drop and subsequent flow rates through supply holes in such applications as filmcooling, transpiration cooling, and impingement cooling that are supplied by microchannels, pipeflow systems, or secondary air systems. The inability to accurately predict flow rates has profound effects on engine operations. The objective of this study was to investigate the influence of several relevant manufacturing features that might occur for a cooling supply hole being fed by a range of channel configurations. The manufacturing variances included the ratio of the hole diameter to the channel width, the number of channel feeds (segments), the effect of hole overlap with respect to the channel sidewalls, and the channel Reynolds number. The results showed that the friction factors for the typically long channels in this study were independent of the tested inlet and exit hole configurations. The results also showed that the nondimensional pressure loss coefficients for the flow passing through the channel inlet holes and through the channel exit holes were found to be independent of the channel flow Reynolds number over the tested range. The geometric scaling ratio of the hole crosssectional area to the channel crosssectional area collapsed the pressure loss coefficients the best for both one and two flow segments for both the channel inlet and channel exit hole.
    • Download: (4.125Mb)
    • Show Full MetaData Hide Full MetaData
    • Get RIS
    • Item Order
    • Go To Publisher
    • Price: 5000 Rial
    • Statistics

      Manufacturing Influences on Pressure Losses of Channel Fed Holes

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/156594
    Collections
    • Journal of Turbomachinery

    Show full item record

    contributor authorBarringer, Michael
    contributor authorThole, Karen A.
    contributor authorKrishnan, Vaidyanathan
    contributor authorLandrum, Evan
    date accessioned2017-05-09T01:13:34Z
    date available2017-05-09T01:13:34Z
    date issued2014
    identifier issn0889-504X
    identifier otherturbo_136_05_051012.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/156594
    description abstractVariations from manufacturing can influence the overall pressure drop and subsequent flow rates through supply holes in such applications as filmcooling, transpiration cooling, and impingement cooling that are supplied by microchannels, pipeflow systems, or secondary air systems. The inability to accurately predict flow rates has profound effects on engine operations. The objective of this study was to investigate the influence of several relevant manufacturing features that might occur for a cooling supply hole being fed by a range of channel configurations. The manufacturing variances included the ratio of the hole diameter to the channel width, the number of channel feeds (segments), the effect of hole overlap with respect to the channel sidewalls, and the channel Reynolds number. The results showed that the friction factors for the typically long channels in this study were independent of the tested inlet and exit hole configurations. The results also showed that the nondimensional pressure loss coefficients for the flow passing through the channel inlet holes and through the channel exit holes were found to be independent of the channel flow Reynolds number over the tested range. The geometric scaling ratio of the hole crosssectional area to the channel crosssectional area collapsed the pressure loss coefficients the best for both one and two flow segments for both the channel inlet and channel exit hole.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleManufacturing Influences on Pressure Losses of Channel Fed Holes
    typeJournal Paper
    journal volume136
    journal issue5
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.4025226
    journal fristpage51012
    journal lastpage51012
    identifier eissn1528-8900
    treeJournal of Turbomachinery:;2014:;volume( 136 ):;issue: 005
    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