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

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.

Authors

Institutions

Publication Details

Journal
Journal of Turbomachinery
Published
2026-01-19
DOI
https://doi.org/10.1115/1.4070936
Primary Topic
Tribology and Lubrication Engineering
Type
article
Field-Weighted Citation Impact
0.00
Controls
|||
ALL TIME
JAN
FEB
MAR
APR
MAY
JUN
JUL
AUG
SEP
OCT
article

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

Alessio Bonini, Antonio Andreini, Alessio Di Geronimo, Lorenzo Orsini
Journal of Turbomachinery
Tribology and Lubrication Engineering
article

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

Alessio Bonini, Antonio Andreini, Alessio Di Geronimo, Lorenzo Orsini
article en

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.

Journal of TurbomachineryVol. 148(7)
University of Florence (IT)
Affordable and clean energy
Openalex Percentile: Top 84%
Tribology and Lubrication Engineering
AI Navigator

Ask Laika to Summarize, Analyze, and Connect papers live on the map.

Summarize Papers & Methodologies

Extract key findings, datasets, and comparative methods across publications.

Benchmark Rankings & Visual Analytics

Rank top research institutions, authors, funders, topics, and journals by Field-Weighted Citation Impact (FWCI) and paper volume with instant charts.

Connect Distant Disciplines

Bridge topological clusters on the map to find hidden collaborative intersections.