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    Evaluation of Computational Fluid Dynamics and Coupled Fluid Solid Modeling for a Direct Transfer Preswirl System

    Source: Journal of Engineering for Gas Turbines and Power:;2013:;volume( 135 ):;issue: 005::page 51501
    Author:
    Javiya, Umesh
    ,
    Chew, John
    ,
    Hills, Nick
    ,
    Dullenkopf, Klaus
    ,
    Scanlon, Timothy
    DOI: 10.1115/1.4007752
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The prediction of the preswirl cooling air delivery and disk metal temperature are important for the cooling system performance and the rotor disk thermal stresses and life assessment. In this paper, standalone 3D steady and unsteady computation fluid dynamics (CFD), and coupled FECFD calculations are presented for prediction of these temperatures. CFD results are compared with previous measurements from a direct transfer preswirl test rig. The predicted cooling air temperatures agree well with the measurement, but the nozzle discharge coefficients are under predicted. Results from the coupled FECFD analyses are compared directly with thermocouple temperature measurements and with heat transfer coefficients on the rotor disk previously obtained from a rotor disk heat conduction solution. Considering the modeling limitations, the coupled approach predicted the solid metal temperatures well. Heat transfer coefficients on the rotor disk from CFD show some effect of the temperature variations on the heat transfer coefficients. Reasonable agreement is obtained with values deduced from the previous heat conduction solution.
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      Evaluation of Computational Fluid Dynamics and Coupled Fluid Solid Modeling for a Direct Transfer Preswirl System

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    http://yetl.yabesh.ir/yetl1/handle/yetl/151601
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorJaviya, Umesh
    contributor authorChew, John
    contributor authorHills, Nick
    contributor authorDullenkopf, Klaus
    contributor authorScanlon, Timothy
    date accessioned2017-05-09T00:58:13Z
    date available2017-05-09T00:58:13Z
    date issued2013
    identifier issn1528-8919
    identifier othergtp_135_5_051501.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/151601
    description abstractThe prediction of the preswirl cooling air delivery and disk metal temperature are important for the cooling system performance and the rotor disk thermal stresses and life assessment. In this paper, standalone 3D steady and unsteady computation fluid dynamics (CFD), and coupled FECFD calculations are presented for prediction of these temperatures. CFD results are compared with previous measurements from a direct transfer preswirl test rig. The predicted cooling air temperatures agree well with the measurement, but the nozzle discharge coefficients are under predicted. Results from the coupled FECFD analyses are compared directly with thermocouple temperature measurements and with heat transfer coefficients on the rotor disk previously obtained from a rotor disk heat conduction solution. Considering the modeling limitations, the coupled approach predicted the solid metal temperatures well. Heat transfer coefficients on the rotor disk from CFD show some effect of the temperature variations on the heat transfer coefficients. Reasonable agreement is obtained with values deduced from the previous heat conduction solution.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleEvaluation of Computational Fluid Dynamics and Coupled Fluid Solid Modeling for a Direct Transfer Preswirl System
    typeJournal Paper
    journal volume135
    journal issue5
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4007752
    journal fristpage51501
    journal lastpage51501
    identifier eissn0742-4795
    treeJournal of Engineering for Gas Turbines and Power:;2013:;volume( 135 ):;issue: 005
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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