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    Analysis of Three-Dimensional Turbomachinery Flows on C-Type Grids Using an Implicit Euler Solver

    Source: Journal of Turbomachinery:;1990:;volume( 112 ):;issue: 003::page 362
    Author:
    K. F. Weber
    ,
    D. W. Thoe
    ,
    R. A. Delaney
    DOI: 10.1115/1.2927668
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A three-dimensional Euler analysis for turbomachinery flows on a C-type grid is presented. The analysis is based on the Beam and Warming implicit algorithm for solution of the unsteady Euler equations and is derived from the ARC3D code developed by Pulliam at NASA Ames Research Center. Modifications made to convert this code from external flow applications to internal turbomachinery flows are given in detail. These changes include the addition of inflow, outflow, and periodic boundary point calculation procedures. Also presented are the C-grid construction procedures. Finally, results of code experimental verification studies for three-dimensional compressor cascade and rotor flows are presented.
    keyword(s): Flow (Dynamics) , Turbomachinery , Inflow , Outflow , Compressors , Construction , Cascades (Fluid dynamics) , Algorithms , Rotors AND Equations ,
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      Analysis of Three-Dimensional Turbomachinery Flows on C-Type Grids Using an Implicit Euler Solver

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/107720
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    contributor authorK. F. Weber
    contributor authorD. W. Thoe
    contributor authorR. A. Delaney
    date accessioned2017-05-08T23:34:05Z
    date available2017-05-08T23:34:05Z
    date copyrightJuly, 1990
    date issued1990
    identifier issn0889-504X
    identifier otherJOTUEI-28604#362_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/107720
    description abstractA three-dimensional Euler analysis for turbomachinery flows on a C-type grid is presented. The analysis is based on the Beam and Warming implicit algorithm for solution of the unsteady Euler equations and is derived from the ARC3D code developed by Pulliam at NASA Ames Research Center. Modifications made to convert this code from external flow applications to internal turbomachinery flows are given in detail. These changes include the addition of inflow, outflow, and periodic boundary point calculation procedures. Also presented are the C-grid construction procedures. Finally, results of code experimental verification studies for three-dimensional compressor cascade and rotor flows are presented.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleAnalysis of Three-Dimensional Turbomachinery Flows on C-Type Grids Using an Implicit Euler Solver
    typeJournal Paper
    journal volume112
    journal issue3
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2927668
    journal fristpage362
    journal lastpage369
    identifier eissn1528-8900
    keywordsFlow (Dynamics)
    keywordsTurbomachinery
    keywordsInflow
    keywordsOutflow
    keywordsCompressors
    keywordsConstruction
    keywordsCascades (Fluid dynamics)
    keywordsAlgorithms
    keywordsRotors AND Equations
    treeJournal of Turbomachinery:;1990:;volume( 112 ):;issue: 003
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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