[HTML][HTML] Heat transfer characteristics of a high-pressure turbine under combined distorted hot-streak and residual swirl: an unsteady computational study

Z Mansouri, R Jefferson-Loveday - International Journal of Heat and Mass …, 2022 - Elsevier
In new generation aero-engines, lean-burn combustors are equipped with swirl injectors in
order to reduce pollutant emissions. At the exit of these combustors, the flow is dominated by …

Study of Combustor–Turbine Interactions by Performing Coupled and Decoupled Hybrid RANS-LES Simulations under Representative Engine-like Conditions

SG Tomasello, R Meloni, L Andrei, A Andreini - Energies, 2023 - mdpi.com
Combustion–turbine interaction phenomena are attracting ever-growing interest in recent
years. As a matter of fact, the strong unsteady and three-dimensional flow field that …

Generation of realistic boundary conditions at the combustion chamber/turbine interface using large-eddy simulation

B Martin, F Duchaine, L Gicquel, N Odier - Energies, 2021 - mdpi.com
Numerical simulation of multiple components in turbomachinery applications is very CPU-
demanding but remains necessary in the majority of cases to capture the proper coupling …

Analysis of Combustor-Turbine Interaction by Using Coupled and Decoupled Scale-Resolving Simulations Under Representative Operating Conditions

SG Tomasello, A Andreini… - … Expo: Power for …, 2023 - asmedigitalcollection.asme.org
The physical phenomena due to the interaction between the combustor chamber and the
first stage nozzle arouse an ever-increasing interest. In fact, a complex and unsteady flow …

Influence of rans turbulent inlet set-up on the swirled hot streak redistribution in a simplified nozzle guide vane passage: comparisons with large-eddy simulations

C Wingel, N Binder, Y Bousquet… - … Expo: Power for …, 2022 - asmedigitalcollection.asme.org
A high-pressure turbine is a complex component of a gas turbine from a thermo-mechanical
point of view. In modern lean-burn combustion chambers, this complexity is enhanced with …

Detailed Characterization of Turbulence Intensity and Dissipation As Boundary Condition for 3D RANS Simulations

V Bologna, P Paliotta, D Petronio… - … Expo: Power for …, 2024 - asmedigitalcollection.asme.org
In the present work, an Hot-Wire Anemometer and a five-hole pressure probe have been
used to characterize the incoming flow of a large-scale turbine cascade. Measurements …

The Effect of Unsteady Inlet Boundary Conditions on the Aero-Thermal Behavior of High-Pressure Turbine Vanes–A Numerical Study Using Scale-Resolving …

J Gründler, K Lehmann… - Journal of …, 2025 - asmedigitalcollection.asme.org
This paper presents the application of a novel method to prescribe unsteady boundary
conditions to transient, scale-resolving computational fluid dynamics simulations of the high …

The Effect of Unsteady Inlet Boundary Conditions on the Aero-Thermal Behavior of High-Pressure Turbine Vanes: A Numerical Study Using Scale-Resolving …

J Gründler, K Lehmann… - … Expo: Power for …, 2023 - asmedigitalcollection.asme.org
This paper presents the application of a novel method to prescribe unsteady boundary
conditions to transient, scale-resolving Computational Fluid Dynamics simulations of the …

[PDF][PDF] Christopher WINGEL Investigation of the RANS approach for the prediction of cooled turbine stage flows submitted to swirled hot streaks

IO EDyF - 2023 - researchgate.net
Investigation of the RANS approach for the prediction of cooled turbine stage flows submitted
to swirled hot streaks Page 1 THÈSE En vue de l’obtention du DOCTORAT DE L’UNIVERSITÉ …