YaBeSH Engineering and Technology Library

    • Journals
    • PaperQuest
    • YSE Standards
    • YaBeSH
    • Login
    View Item 
    •   YE&T Library
    • ASME
    • Journal of Fluids Engineering
    • View Item
    •   YE&T Library
    • ASME
    • Journal of Fluids Engineering
    • 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

    Evaluation of a High Hub/Tip Ratio Centrifugal Compressor

    Source: Journal of Fluids Engineering:;1970:;volume( 092 ):;issue: 003::page 419
    Author:
    F. G. Groh
    ,
    D. P. Kenny
    ,
    G. M. Wood
    ,
    R. S. Kulp
    DOI: 10.1115/1.3425017
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A centrifugal compressor stage with an unusually high inlet hub/tip ratio of 0.87 was designed for a pressure ratio of 2.0 at a corrected mass flow of 2.45 lb per sec. The geometry was selected so that the centrifugal stage could replace several of the last stages of a multistage axial compressor. The stage was tested with two diffuser schemes. One diffuser consisted of a series of drilled conical pipes, whereas the other employed multirow vaned cascades. Sea level aerodynamic tests of the compressor stage with each diffuser showed a peak total-to-total efficiency at design speed of 83.8 percent for the pipe diffuser and 82.9 percent for the vaned cascade diffuser. Additional tests were conducted with a vaneless diffuser to determine effects of impeller discharge tip clearance and inlet prewhirl on impeller performance.
    keyword(s): Compressors , Diffusers , Impellers , Pipes , Geometry , Vaneless diffusers , Seas , Cascades (Fluid dynamics) , Pressure , Flow (Dynamics) , Clearances (Engineering) AND Design ,
    • Download: (1.404Mb)
    • Show Full MetaData Hide Full MetaData
    • Get RIS
    • Item Order
    • Go To Publisher
    • Price: 5000 Rial
    • Statistics

      Evaluation of a High Hub/Tip Ratio Centrifugal Compressor

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/143445
    Collections
    • Journal of Fluids Engineering

    Show full item record

    contributor authorF. G. Groh
    contributor authorD. P. Kenny
    contributor authorG. M. Wood
    contributor authorR. S. Kulp
    date accessioned2017-05-09T00:38:11Z
    date available2017-05-09T00:38:11Z
    date copyrightSeptember, 1970
    date issued1970
    identifier issn0098-2202
    identifier otherJFEGA4-27367#419_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/143445
    description abstractA centrifugal compressor stage with an unusually high inlet hub/tip ratio of 0.87 was designed for a pressure ratio of 2.0 at a corrected mass flow of 2.45 lb per sec. The geometry was selected so that the centrifugal stage could replace several of the last stages of a multistage axial compressor. The stage was tested with two diffuser schemes. One diffuser consisted of a series of drilled conical pipes, whereas the other employed multirow vaned cascades. Sea level aerodynamic tests of the compressor stage with each diffuser showed a peak total-to-total efficiency at design speed of 83.8 percent for the pipe diffuser and 82.9 percent for the vaned cascade diffuser. Additional tests were conducted with a vaneless diffuser to determine effects of impeller discharge tip clearance and inlet prewhirl on impeller performance.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleEvaluation of a High Hub/Tip Ratio Centrifugal Compressor
    typeJournal Paper
    journal volume92
    journal issue3
    journal titleJournal of Fluids Engineering
    identifier doi10.1115/1.3425017
    journal fristpage419
    journal lastpage428
    identifier eissn1528-901X
    keywordsCompressors
    keywordsDiffusers
    keywordsImpellers
    keywordsPipes
    keywordsGeometry
    keywordsVaneless diffusers
    keywordsSeas
    keywordsCascades (Fluid dynamics)
    keywordsPressure
    keywordsFlow (Dynamics)
    keywordsClearances (Engineering) AND Design
    treeJournal of Fluids Engineering:;1970:;volume( 092 ):;issue: 003
    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