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

    The Determination of End-Wall Blockage in Axial Compressors: A Comparison Between Various Approaches

    Source: Journal of Turbomachinery:;2000:;volume( 122 ):;issue: 002::page 218
    Author:
    J. H. Horlock
    DOI: 10.1115/1.555452
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The end-wall blockage in axial compressors has been the subject of several investigations over a period of many years. This paper reviews and compares various approaches to determining the blockage, particularly in the “repeating” stage, a stage deeply embedded in the compressor where an equilibrium state is reached, the flow through any one stage repeating in the next. These approaches include: (i) correlations of displacement thickness measured in compressor rigs; (ii) a relationship between outlet blockage and the clearance area, based both on an empirical development of a simple model of the flow through the clearance space and full CFD calculations of the flow; (iii) momentum analysis of the flow through the blockage region, developed from the boundary layer analyses of some years ago, but not now relying on boundary layer concepts. [S0889-504X(00)01502-6]
    keyword(s): Pressure , Momentum , Flow (Dynamics) , Compressors , Clearances (Engineering) , Boundary layers , Rotors , Blades , Thickness , Stators , Equilibrium (Physics) AND Displacement ,
    • Download: (130.2Kb)
    • Show Full MetaData Hide Full MetaData
    • Get RIS
    • Item Order
    • Go To Publisher
    • Price: 5000 Rial
    • Statistics

      The Determination of End-Wall Blockage in Axial Compressors: A Comparison Between Various Approaches

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/124481
    Collections
    • Journal of Turbomachinery

    Show full item record

    contributor authorJ. H. Horlock
    date accessioned2017-05-09T00:03:39Z
    date available2017-05-09T00:03:39Z
    date copyrightApril, 2000
    date issued2000
    identifier issn0889-504X
    identifier otherJOTUEI-28676#218_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/124481
    description abstractThe end-wall blockage in axial compressors has been the subject of several investigations over a period of many years. This paper reviews and compares various approaches to determining the blockage, particularly in the “repeating” stage, a stage deeply embedded in the compressor where an equilibrium state is reached, the flow through any one stage repeating in the next. These approaches include: (i) correlations of displacement thickness measured in compressor rigs; (ii) a relationship between outlet blockage and the clearance area, based both on an empirical development of a simple model of the flow through the clearance space and full CFD calculations of the flow; (iii) momentum analysis of the flow through the blockage region, developed from the boundary layer analyses of some years ago, but not now relying on boundary layer concepts. [S0889-504X(00)01502-6]
    publisherThe American Society of Mechanical Engineers (ASME)
    titleThe Determination of End-Wall Blockage in Axial Compressors: A Comparison Between Various Approaches
    typeJournal Paper
    journal volume122
    journal issue2
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.555452
    journal fristpage218
    journal lastpage224
    identifier eissn1528-8900
    keywordsPressure
    keywordsMomentum
    keywordsFlow (Dynamics)
    keywordsCompressors
    keywordsClearances (Engineering)
    keywordsBoundary layers
    keywordsRotors
    keywordsBlades
    keywordsThickness
    keywordsStators
    keywordsEquilibrium (Physics) AND Displacement
    treeJournal of Turbomachinery:;2000:;volume( 122 ):;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