@inproceedings{6e714554c45942b19ec53f7a3272bba0,
title = "Combustion instabilities of supersonic cavity flow computational studies using LES",
abstract = "Experimental studies of supersonic combustion poses significant challenges. Therefore, computational approaches are a promising alternative for the numerical studies of supersonic combustion. The present studies concerns the computational studies of supersonic combustion. Particularly, the study concerns the effect of the Mach number and fuel injection scheme on the combustion efficiency. The combustion efficiency is assessed based on the temperature developed inside the supersonic cavity. The computations are carried out using the large-eddy simulation (LES) approach along with the flamelet combustion model. The analysis reveals the presence of a region of high level of temperature, NO and 2 CO, inside the cavity. The reverse flow causes a preferential distribution of this region towards the step side of the cavity.",
author = "Marcel Ilie and John McAfee and Valentin Soloiu and Mosfequr Rahman",
note = "Publisher Copyright: {\textcopyright} 2023, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.; AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2023 ; Conference date: 12-06-2023 Through 16-06-2023",
year = "2023",
doi = "10.2514/6.2023-4136",
language = "English",
isbn = "9781624107047",
series = "AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2023",
publisher = "American Institute of Aeronautics and Astronautics Inc, AIAA",
booktitle = "AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2023",
}