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    A Rapid Blade-to-Blade Solution for Use in Turbomachinery Design

    Source: Journal of Engineering for Gas Turbines and Power:;1984:;volume( 106 ):;issue: 002::page 376
    Author:
    E. R. McFarland
    DOI: 10.1115/1.3239574
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A rapid technique for solving the blade-to-blade turbomachinery flow problem has been developed. Approximate governing flow equations, which include the effects of compressibility, radius change, rotation, and variable stream sheet thickness are solved using an improved panel method. The development and solution of these equations are described. Sample calculations are presented to illustrate the method’s capabilities and accuracy.
    keyword(s): Design , Blades , Turbomachinery , Flow (Dynamics) , Equations , Thickness , Rotation AND Compressibility ,
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      A Rapid Blade-to-Blade Solution for Use in Turbomachinery Design

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    http://yetl.yabesh.ir/yetl1/handle/yetl/98440
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorE. R. McFarland
    date accessioned2017-05-08T23:17:50Z
    date available2017-05-08T23:17:50Z
    date copyrightApril, 1984
    date issued1984
    identifier issn1528-8919
    identifier otherJETPEZ-26604#376_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/98440
    description abstractA rapid technique for solving the blade-to-blade turbomachinery flow problem has been developed. Approximate governing flow equations, which include the effects of compressibility, radius change, rotation, and variable stream sheet thickness are solved using an improved panel method. The development and solution of these equations are described. Sample calculations are presented to illustrate the method’s capabilities and accuracy.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleA Rapid Blade-to-Blade Solution for Use in Turbomachinery Design
    typeJournal Paper
    journal volume106
    journal issue2
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3239574
    journal fristpage376
    journal lastpage382
    identifier eissn0742-4795
    keywordsDesign
    keywordsBlades
    keywordsTurbomachinery
    keywordsFlow (Dynamics)
    keywordsEquations
    keywordsThickness
    keywordsRotation AND Compressibility
    treeJournal of Engineering for Gas Turbines and Power:;1984:;volume( 106 ):;issue: 002
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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