@inproceedings{cbf8154bf37541a993fed2956f899424,
title = "Parametric studies of swirl combustor using les; the effect of injectors{\textquoteright} angle",
abstract = "The effect of the injectors{\textquoteright} fuel flow rates and angle on the swirl combustion is 0 0 0 0 computationally studied for a range of fuel/air ratios (1 ÷ 4) and angles (30,45,60,90 ) . The computations are carried out suing the large-eddy simulation (LES) approach. The analysis reveals the presence of a region of high level of temperature, NO and CO2, inside the cavity. The swirl flow causes a preferential distribution of this region towards the side of the combustor.",
author = "Marcel Ilie and Geoffrey Sullivan",
note = "Publisher Copyright: {\textcopyright} 2021, American Institute of Aeronautics and Astronautics Inc, AIAA. All Rights Reserved.; AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2021 ; Conference date: 11-01-2021 Through 15-01-2021",
year = "2021",
doi = "10.2514/6.2021-1110",
language = "English",
isbn = "9781624106095",
series = "AIAA Scitech 2021 Forum",
publisher = "American Institute of Aeronautics and Astronautics Inc, AIAA",
pages = "1--8",
booktitle = "AIAA Scitech 2021 Forum",
}