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    Scalar Diffusion Equation-Based Model to Predict 2-Dimensional Film Cooling Effectiveness of a Shaped Hole

    Source: Journal of Turbomachinery:;2021:;volume( 143 ):;issue: 004::page 041005-1
    Author:
    Chen, Ziyu
    ,
    Li, Yifei
    ,
    Su, Xinrong
    ,
    Yuan, Xin
    DOI: 10.1115/1.4049782
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: One-dimensional laterally averaged adiabatic film cooling effectiveness η¯lat-based correlations have been widely employed in the cooling design of the modern gas turbine and aero-engine; however, the flow field of the discrete film cooling is fully three dimensional, and thus, the cooling effectiveness distribution on the solid surface is two dimensional. Accurate prediction of the cooling effectiveness distribution in the lateral direction would help to optimize the film cooling design, but few paid attention to this issue in the literature. In this study, a simple yet accurate scalar diffusion equation based model is proposed to extend the one-dimensional correlation into two dimensional. The model is proved to be accurate and efficient. According to the accuracy analysis, the R2 value is larger than 0.95 for the two-dimensional prediction and over 0.93 along the centerline. With given input parameters, the calculation cost for solving a certain case is in the magnitude of 1 × 10−3s in time using the space-marching method. There is only the effective diffusion coefficient left to be modeled in the control equation. It represents the balance between the diffusion and the passive transportation by the main flow. Analyses conducted within the typical experimental range show that κ~eff is only dependent on the velocity ratio and the main-flow turbulence.
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      Scalar Diffusion Equation-Based Model to Predict 2-Dimensional Film Cooling Effectiveness of a Shaped Hole

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4278964
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    contributor authorChen, Ziyu
    contributor authorLi, Yifei
    contributor authorSu, Xinrong
    contributor authorYuan, Xin
    date accessioned2022-02-06T05:52:43Z
    date available2022-02-06T05:52:43Z
    date copyright3/22/2021 12:00:00 AM
    date issued2021
    identifier issn0889-504X
    identifier otherturbo_143_4_041005.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4278964
    description abstractOne-dimensional laterally averaged adiabatic film cooling effectiveness η¯lat-based correlations have been widely employed in the cooling design of the modern gas turbine and aero-engine; however, the flow field of the discrete film cooling is fully three dimensional, and thus, the cooling effectiveness distribution on the solid surface is two dimensional. Accurate prediction of the cooling effectiveness distribution in the lateral direction would help to optimize the film cooling design, but few paid attention to this issue in the literature. In this study, a simple yet accurate scalar diffusion equation based model is proposed to extend the one-dimensional correlation into two dimensional. The model is proved to be accurate and efficient. According to the accuracy analysis, the R2 value is larger than 0.95 for the two-dimensional prediction and over 0.93 along the centerline. With given input parameters, the calculation cost for solving a certain case is in the magnitude of 1 × 10−3s in time using the space-marching method. There is only the effective diffusion coefficient left to be modeled in the control equation. It represents the balance between the diffusion and the passive transportation by the main flow. Analyses conducted within the typical experimental range show that κ~eff is only dependent on the velocity ratio and the main-flow turbulence.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleScalar Diffusion Equation-Based Model to Predict 2-Dimensional Film Cooling Effectiveness of a Shaped Hole
    typeJournal Paper
    journal volume143
    journal issue4
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.4049782
    journal fristpage041005-1
    journal lastpage041005-13
    page13
    treeJournal of Turbomachinery:;2021:;volume( 143 ):;issue: 004
    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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