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    Inviscid-Viscous Coupled Solution for Unsteady Flows Through Vibrating Blades: Part 1—Description of the Method

    Source: Journal of Turbomachinery:;1993:;volume( 115 ):;issue: 001::page 94
    Author:
    L. He
    ,
    J. D. Denton
    DOI: 10.1115/1.2929222
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An efficient coupled approach between inviscid Euler and integral boundary layer solutions has been developed for quasi-3-D unsteady flows induced by vibrating blades. For unsteady laminar and turbulent boundary layers, steady correlations are adopted in a quasi-steady way to close the integral boundary layer model. This quasi-steady adoption of the correlations is assessed by numerical test results using a direct solution of the unsteady momentum integral equation. To conduct the coupling between the inviscid and viscous solutions for strongly interactive flows, the unsteady Euler and integral boundary layer equations are simultaneously time-marched using a multistep Runge–Kutta scheme, and the boundary layer displacement effect is accounted for by a first order transpiration model. This time-resolved coupling method converges at conditions with considerable boundary layer separation.
    keyword(s): Blades , Unsteady flow , Boundary layers , Momentum , Flow (Dynamics) , Separation (Technology) , Boundary layer turbulence , Displacement , Equations , Integral equations AND Transpiration ,
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      Inviscid-Viscous Coupled Solution for Unsteady Flows Through Vibrating Blades: Part 1—Description of the Method

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    http://yetl.yabesh.ir/yetl1/handle/yetl/112852
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    contributor authorL. He
    contributor authorJ. D. Denton
    date accessioned2017-05-08T23:42:55Z
    date available2017-05-08T23:42:55Z
    date copyrightJanuary, 1993
    date issued1993
    identifier issn0889-504X
    identifier otherJOTUEI-28627#94_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/112852
    description abstractAn efficient coupled approach between inviscid Euler and integral boundary layer solutions has been developed for quasi-3-D unsteady flows induced by vibrating blades. For unsteady laminar and turbulent boundary layers, steady correlations are adopted in a quasi-steady way to close the integral boundary layer model. This quasi-steady adoption of the correlations is assessed by numerical test results using a direct solution of the unsteady momentum integral equation. To conduct the coupling between the inviscid and viscous solutions for strongly interactive flows, the unsteady Euler and integral boundary layer equations are simultaneously time-marched using a multistep Runge–Kutta scheme, and the boundary layer displacement effect is accounted for by a first order transpiration model. This time-resolved coupling method converges at conditions with considerable boundary layer separation.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleInviscid-Viscous Coupled Solution for Unsteady Flows Through Vibrating Blades: Part 1—Description of the Method
    typeJournal Paper
    journal volume115
    journal issue1
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2929222
    journal fristpage94
    journal lastpage100
    identifier eissn1528-8900
    keywordsBlades
    keywordsUnsteady flow
    keywordsBoundary layers
    keywordsMomentum
    keywordsFlow (Dynamics)
    keywordsSeparation (Technology)
    keywordsBoundary layer turbulence
    keywordsDisplacement
    keywordsEquations
    keywordsIntegral equations AND Transpiration
    treeJournal of Turbomachinery:;1993:;volume( 115 ):;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
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