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    Unsteady Flow in Oscillating Turbine Cascades: Part 2—Computational Study

    Source: Journal of Turbomachinery:;1998:;volume( 120 ):;issue: 002::page 269
    Author:
    L. He
    DOI: 10.1115/1.2841402
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Unsteady flow around a linear oscillating turbine cascade has been experimentally and computationally studied, aimed at understanding the bubble type of flow separation and examining the predictive ability of a computational method. It was also intended to check the validity of the linear assumption under an unsteady viscous flow condition. Part 2 of the paper presents a computational study of the experimental turbine cascade that was discussed in Part 1. Numerical calculations were carried out for this case using an unsteady Navier–Stokes solver. The Baldwin–Lomax mixing length model was adopted for turbulence closure. The boundary layers on blade surfaces were either assumed to be fully turbulent or transitional with the unsteady transition subject to a quasi-steady laminar separation bubble model. The comparison between the computations and the experiment was generally quite satisfactory, except in the regions with the flow separation. It was shown that the behavior of the short bubble on the suction surface could be reasonably accounted for by using the quasi-steady bubble transition model. The calculation also showed that there was a more apparent mesh dependence of the results in the regions of flow separation. Two different kinds of numerical test were carried out to check the linearity of the unsteady flow and therefore the validity of the influence coefficient method. First, calculations using the same configurations as in the experiment were performed with different oscillating amplitudes. Second, calculations were performed with a tuned cascade model and the results were compared with those using the influence coefficient method. The present work showed that the nonlinear effect was quite small, even though for the most severe case in which the separated flow region covered about 60 percent of blade pressure surface with a large movement of the reattachment point. It seemed to suggest that the linear assumption about the unsteady flow behavior should be adequately acceptable for situations with bubble-type flow separation similar to the present case.
    keyword(s): Turbines , Unsteady flow , Bubbles , Flow separation , Cascades (Fluid dynamics) , Turbulence , Blades , Computation , Computational methods , Suction , Pressure , Flow (Dynamics) , Separation (Technology) , Viscous flow AND Boundary layers ,
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      Unsteady Flow in Oscillating Turbine Cascades: Part 2—Computational Study

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    http://yetl.yabesh.ir/yetl1/handle/yetl/121327
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    contributor authorL. He
    date accessioned2017-05-08T23:58:12Z
    date available2017-05-08T23:58:12Z
    date copyrightApril, 1998
    date issued1998
    identifier issn0889-504X
    identifier otherJOTUEI-28665#269_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/121327
    description abstractUnsteady flow around a linear oscillating turbine cascade has been experimentally and computationally studied, aimed at understanding the bubble type of flow separation and examining the predictive ability of a computational method. It was also intended to check the validity of the linear assumption under an unsteady viscous flow condition. Part 2 of the paper presents a computational study of the experimental turbine cascade that was discussed in Part 1. Numerical calculations were carried out for this case using an unsteady Navier–Stokes solver. The Baldwin–Lomax mixing length model was adopted for turbulence closure. The boundary layers on blade surfaces were either assumed to be fully turbulent or transitional with the unsteady transition subject to a quasi-steady laminar separation bubble model. The comparison between the computations and the experiment was generally quite satisfactory, except in the regions with the flow separation. It was shown that the behavior of the short bubble on the suction surface could be reasonably accounted for by using the quasi-steady bubble transition model. The calculation also showed that there was a more apparent mesh dependence of the results in the regions of flow separation. Two different kinds of numerical test were carried out to check the linearity of the unsteady flow and therefore the validity of the influence coefficient method. First, calculations using the same configurations as in the experiment were performed with different oscillating amplitudes. Second, calculations were performed with a tuned cascade model and the results were compared with those using the influence coefficient method. The present work showed that the nonlinear effect was quite small, even though for the most severe case in which the separated flow region covered about 60 percent of blade pressure surface with a large movement of the reattachment point. It seemed to suggest that the linear assumption about the unsteady flow behavior should be adequately acceptable for situations with bubble-type flow separation similar to the present case.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleUnsteady Flow in Oscillating Turbine Cascades: Part 2—Computational Study
    typeJournal Paper
    journal volume120
    journal issue2
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2841402
    journal fristpage269
    journal lastpage275
    identifier eissn1528-8900
    keywordsTurbines
    keywordsUnsteady flow
    keywordsBubbles
    keywordsFlow separation
    keywordsCascades (Fluid dynamics)
    keywordsTurbulence
    keywordsBlades
    keywordsComputation
    keywordsComputational methods
    keywordsSuction
    keywordsPressure
    keywordsFlow (Dynamics)
    keywordsSeparation (Technology)
    keywordsViscous flow AND Boundary layers
    treeJournal of Turbomachinery:;1998:;volume( 120 ):;issue: 002
    contenttypeFulltext
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