@inproceedings{f52b5b7964554548b73a8622760b5214,
title = "Aerodynamic studies of rotor-stator turbine stage using LES",
abstract = "Aerodynamic studies of stator-rotor turbine stage are performed using the large-eddy simulation approach. The goal of the present research is to understand the blade-vortex interaction mechanism which defines the aerodynamics of rotor-stator turbine stage. The computational studies are carried out in a rotating frame of reference. The analysis is carried out for high-Reynolds number flow, Re = 1.3x105. The analysis reveals that the blade-vortex interaction causes the flow separation on the stator stage and a time-varying lift and drag.",
author = "Marcel Ilie",
note = "Publisher Copyright: {\textcopyright} 2024 Lockheed Martin Corporation. All Rights Reserved.; AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2025 ; Conference date: 06-01-2025 Through 10-01-2025",
year = "2025",
doi = "10.2514/6.2025-2618",
language = "English",
isbn = "9781624107238",
series = "AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2025",
publisher = "American Institute of Aeronautics and Astronautics Inc, AIAA",
booktitle = "AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2025",
}