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    Assessment of Computational Fluid Dynamic Modeling of Multi-Jet Impingement Cooling and Validation With the Experiments

    Source: Journal of Turbomachinery:;2023:;volume( 145 ):;issue: 007::page 71005-1
    Author:
    Tabassum, Sadiya
    ,
    Hilfer, Michael
    ,
    Brakmann, Robin G.
    ,
    Morsbach, Christian
    ,
    Willert, Christian
    ,
    Matha, Marcel
    ,
    Schroll, Michael
    DOI: 10.1115/1.4056715
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The current study involves numerical and experimental investigations of circular in-line jets impinging on a heated flat plate. The generic configuration is characterized by nine jets, each with a diameter of D = 0.0152 m. The jets are influenced by a self-generating crossflow and are positioned at a nozzle-to-plate distance (H/D) of 5 and a jet pitch (p/D) of 5. The steady Reynolds-averaged Navier–Stokes (RANS) simulations are performed for turbulent jet Reynolds numbers with the in-house CFD code TRACE. The Menter k–ω shear stress transport (SST) model is applied for turbulence modeling and the turbulent scalar fluxes are modeled based on the Reynolds analogy for a constant turbulent Prandtl number. To gain a closer insight into the impingement jet physics, high-resolution near-wall velocity and thermal fields are obtained through large eddy simulations (LESs) and measurements from particle image velocimetry (PIV). Focus is laid on the comparison of RANS results with the LES data and the experimental data. The results exhibit a qualitative similarity between the simulations and the experiments. Furthermore, correlations of the Nusselt number from the literature are used to validate the simulation results.
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      Assessment of Computational Fluid Dynamic Modeling of Multi-Jet Impingement Cooling and Validation With the Experiments

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4291582
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    • Journal of Turbomachinery

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    contributor authorTabassum, Sadiya
    contributor authorHilfer, Michael
    contributor authorBrakmann, Robin G.
    contributor authorMorsbach, Christian
    contributor authorWillert, Christian
    contributor authorMatha, Marcel
    contributor authorSchroll, Michael
    date accessioned2023-08-16T18:11:19Z
    date available2023-08-16T18:11:19Z
    date copyright2/10/2023 12:00:00 AM
    date issued2023
    identifier issn0889-504X
    identifier otherturbo_145_7_071005.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4291582
    description abstractThe current study involves numerical and experimental investigations of circular in-line jets impinging on a heated flat plate. The generic configuration is characterized by nine jets, each with a diameter of D = 0.0152 m. The jets are influenced by a self-generating crossflow and are positioned at a nozzle-to-plate distance (H/D) of 5 and a jet pitch (p/D) of 5. The steady Reynolds-averaged Navier–Stokes (RANS) simulations are performed for turbulent jet Reynolds numbers with the in-house CFD code TRACE. The Menter k–ω shear stress transport (SST) model is applied for turbulence modeling and the turbulent scalar fluxes are modeled based on the Reynolds analogy for a constant turbulent Prandtl number. To gain a closer insight into the impingement jet physics, high-resolution near-wall velocity and thermal fields are obtained through large eddy simulations (LESs) and measurements from particle image velocimetry (PIV). Focus is laid on the comparison of RANS results with the LES data and the experimental data. The results exhibit a qualitative similarity between the simulations and the experiments. Furthermore, correlations of the Nusselt number from the literature are used to validate the simulation results.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleAssessment of Computational Fluid Dynamic Modeling of Multi-Jet Impingement Cooling and Validation With the Experiments
    typeJournal Paper
    journal volume145
    journal issue7
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.4056715
    journal fristpage71005-1
    journal lastpage71005-11
    page11
    treeJournal of Turbomachinery:;2023:;volume( 145 ):;issue: 007
    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
    yabeshDSpacePersian