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    Numerical Analysis of Sealing Flows in Gas Turbines Using RANS and Large Eddy Simulation Approaches

    Source: Journal of Turbomachinery:;2026:;volume( 148 ):;issue:007::page 1016
    Author:
    Di Geronimo, A.
    ,
    Orsini, L.
    ,
    Andreini, A.
    ,
    Bonini, A.
    DOI: 10.1115/1.4070936
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Abstract. The flow field developing inside the stator–rotor disc cavities of gas turbines is characterized by highly complex and unsteady behavior driven by strong vortical structures and transient interactions. These features pose significant challenges for accurate prediction using standard computational fluid dynamics models. In particular, the inherent unsteadiness of the flow field has a considerable impact on the sealing performance of the rim, especially when predicted by steady Reynolds-averaged Navier–Stokes (RANS) methods, which tend to overestimate the sealing effectiveness by more than an order of magnitude. In this study, a series of numerical simulations were conducted using RANS, unsteady RANS (URANS), and large eddy simulation (LES) approaches to gain insight into the behavior of the rim seal flow. The main objective was to compare the numerical results with experimental data obtained from the test rig at the University of Florence, to validate the accuracy of different numerical approaches. The RANS, URANS, and LES demonstrated satisfactory agreement in terms of steady-state measurements of pressure coefficients and velocity fields, offering valuable insight into the time-averaged behavior of the flow. However, the Reynolds-averaged models failed to effectively capture the turbulent fluctuations between the main flow and the secondary flow. In contrast, LES accurately captured the development of vortices and replicated more realistic flow conditions, resulting in a closer match with experimental data. Therefore, the resolution of these fluctuations, which is nowadays considered to be one of the fundamental factors driving the ingestion of mainstream flow into the cavity, appeared to be crucial to accurately understand the unsteady interaction between mainstream and secondary flows. Although the high computational cost and long transient phases required to reach periodic convergence make LES a resource-intensive approach, it demonstrates great potential for accurately predicting this interaction and providing valuable insights into the complex flow dynamics of rim seal flows.
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      Numerical Analysis of Sealing Flows in Gas Turbines Using RANS and Large Eddy Simulation Approaches

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    https://yetl.yabesh.ir/yetl1/handle/yetl/4314915
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    contributor authorDi Geronimo, A.
    contributor authorOrsini, L.
    contributor authorAndreini, A.
    contributor authorBonini, A.
    date accessioned2026-08-23T07:18:19Z
    date available2026-08-23T07:18:19Z
    date copyright2026/07/01
    date issued2026
    identifier issn0889-504X
    identifier otherturbo-25-1202.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4314915
    description abstractAbstract. The flow field developing inside the stator–rotor disc cavities of gas turbines is characterized by highly complex and unsteady behavior driven by strong vortical structures and transient interactions. These features pose significant challenges for accurate prediction using standard computational fluid dynamics models. In particular, the inherent unsteadiness of the flow field has a considerable impact on the sealing performance of the rim, especially when predicted by steady Reynolds-averaged Navier–Stokes (RANS) methods, which tend to overestimate the sealing effectiveness by more than an order of magnitude. In this study, a series of numerical simulations were conducted using RANS, unsteady RANS (URANS), and large eddy simulation (LES) approaches to gain insight into the behavior of the rim seal flow. The main objective was to compare the numerical results with experimental data obtained from the test rig at the University of Florence, to validate the accuracy of different numerical approaches. The RANS, URANS, and LES demonstrated satisfactory agreement in terms of steady-state measurements of pressure coefficients and velocity fields, offering valuable insight into the time-averaged behavior of the flow. However, the Reynolds-averaged models failed to effectively capture the turbulent fluctuations between the main flow and the secondary flow. In contrast, LES accurately captured the development of vortices and replicated more realistic flow conditions, resulting in a closer match with experimental data. Therefore, the resolution of these fluctuations, which is nowadays considered to be one of the fundamental factors driving the ingestion of mainstream flow into the cavity, appeared to be crucial to accurately understand the unsteady interaction between mainstream and secondary flows. Although the high computational cost and long transient phases required to reach periodic convergence make LES a resource-intensive approach, it demonstrates great potential for accurately predicting this interaction and providing valuable insights into the complex flow dynamics of rim seal flows.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleNumerical Analysis of Sealing Flows in Gas Turbines Using RANS and Large Eddy Simulation Approaches
    typeJournal Paper
    journal volume148
    journal issue7
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.4070936
    journal fristpage1016
    journal lastpage1031
    page16
    treeJournal of Turbomachinery:;2026:;volume( 148 ):;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
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