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    Investigation of Periodic Boundary Conditions in Multipassage Cascade Flows Using Overset Grids

    Source: Journal of Turbomachinery:;1999:;volume( 121 ):;issue: 002::page 341
    Author:
    I. H. Tuncer
    ,
    S. Weber
    ,
    W. Sanz
    DOI: 10.1115/1.2841320
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A Navier–Stokes solution method with overset grids is applied to unsteady multipassage cascade flows, and the unsteady blade loadings are compared against the single-passage solutions with the direct store interblade boundary condition. In the overset grid solutions, the multipassage domain is discretized with O-type grids around each blade and a rectangular background grid. Blade grids are allowed to move in time relative to the background grid, as prescribed by the oscillatory plunging motion. The overset grid method uses a simple, robust numerical algorithm to localize moving intergrid boundary points and to interpolate solution variables across grids. Computational results are presented for two and four-passage, subsonic and transonic flows through a turbine and a compressor cascade. The overset grid solutions over the multipassage periodic domains agree well with the single-passage solutions and the experimental data. It is concluded that the time linearization error introduced by the direct store approach is negligible in the range of flow conditions studied.
    keyword(s): Flow (Dynamics) , Cascades (Fluid dynamics) , Boundary-value problems , Blades , Errors , Transonic flow , Algorithms , Turbines , Motion AND Compressors ,
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      Investigation of Periodic Boundary Conditions in Multipassage Cascade Flows Using Overset Grids

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/123047
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    contributor authorI. H. Tuncer
    contributor authorS. Weber
    contributor authorW. Sanz
    date accessioned2017-05-09T00:01:19Z
    date available2017-05-09T00:01:19Z
    date copyrightApril, 1999
    date issued1999
    identifier issn0889-504X
    identifier otherJOTUEI-28669#341_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/123047
    description abstractA Navier–Stokes solution method with overset grids is applied to unsteady multipassage cascade flows, and the unsteady blade loadings are compared against the single-passage solutions with the direct store interblade boundary condition. In the overset grid solutions, the multipassage domain is discretized with O-type grids around each blade and a rectangular background grid. Blade grids are allowed to move in time relative to the background grid, as prescribed by the oscillatory plunging motion. The overset grid method uses a simple, robust numerical algorithm to localize moving intergrid boundary points and to interpolate solution variables across grids. Computational results are presented for two and four-passage, subsonic and transonic flows through a turbine and a compressor cascade. The overset grid solutions over the multipassage periodic domains agree well with the single-passage solutions and the experimental data. It is concluded that the time linearization error introduced by the direct store approach is negligible in the range of flow conditions studied.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleInvestigation of Periodic Boundary Conditions in Multipassage Cascade Flows Using Overset Grids
    typeJournal Paper
    journal volume121
    journal issue2
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2841320
    journal fristpage341
    journal lastpage347
    identifier eissn1528-8900
    keywordsFlow (Dynamics)
    keywordsCascades (Fluid dynamics)
    keywordsBoundary-value problems
    keywordsBlades
    keywordsErrors
    keywordsTransonic flow
    keywordsAlgorithms
    keywordsTurbines
    keywordsMotion AND Compressors
    treeJournal of Turbomachinery:;1999:;volume( 121 ):;issue: 002
    contenttypeFulltext
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