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    Through-Flow Analysis of a Multistage Compressor: Part I—Aerodynamic Input

    Source: Journal of Turbomachinery:;1986:;volume( 108 ):;issue: 001::page 17
    Author:
    R. P. Dring
    ,
    H. D. Joslyn
    DOI: 10.1115/1.3262016
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Through-flow theory is at the heart of turbomachinery aerodynamic design in that it provides the incidence and Mach number distributions that are ultimately used to define the rotor and stator airfoil contours. The assumption of axisymmetry plays a major role in the formulation of the theory and the consequences of this assumption have historically necessitated the introduction of “blockage” to account for the nonaxisymmetries in the flow. The present paper provides an assessment of these assumptions and of through-flow theory in general by making detailed comparisons between computed and measured results for a two-stage axial compressor. Part I focuses on the experimental benchmark data base and on how these data were used to fully define all of the aerodynamic input required by a through-flow analysis.
    keyword(s): Compressors , Flow (Dynamics) , Mach number , Design , Rotors , Databases , Stators , Turbomachinery AND Airfoils ,
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      Through-Flow Analysis of a Multistage Compressor: Part I—Aerodynamic Input

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/101849
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    contributor authorR. P. Dring
    contributor authorH. D. Joslyn
    date accessioned2017-05-08T23:23:42Z
    date available2017-05-08T23:23:42Z
    date copyrightJuly, 1986
    date issued1986
    identifier issn0889-504X
    identifier otherJOTUEI-28577#17_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/101849
    description abstractThrough-flow theory is at the heart of turbomachinery aerodynamic design in that it provides the incidence and Mach number distributions that are ultimately used to define the rotor and stator airfoil contours. The assumption of axisymmetry plays a major role in the formulation of the theory and the consequences of this assumption have historically necessitated the introduction of “blockage” to account for the nonaxisymmetries in the flow. The present paper provides an assessment of these assumptions and of through-flow theory in general by making detailed comparisons between computed and measured results for a two-stage axial compressor. Part I focuses on the experimental benchmark data base and on how these data were used to fully define all of the aerodynamic input required by a through-flow analysis.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleThrough-Flow Analysis of a Multistage Compressor: Part I—Aerodynamic Input
    typeJournal Paper
    journal volume108
    journal issue1
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.3262016
    journal fristpage17
    journal lastpage22
    identifier eissn1528-8900
    keywordsCompressors
    keywordsFlow (Dynamics)
    keywordsMach number
    keywordsDesign
    keywordsRotors
    keywordsDatabases
    keywordsStators
    keywordsTurbomachinery AND Airfoils
    treeJournal of Turbomachinery:;1986:;volume( 108 ):;issue: 001
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian