@inproceedings{3aedb581cee5453e9d750d2a9b790d64,
title = "Aerodynamics and aeroacoustics studies of supersonic flow past wing",
abstract = "Computational studies of transient three-dimensional supersonic flows over a wing are carried out using the large eddy simulation (LES) approach. The studies concern the understanding of the effect of Mach number on the flow field, aerodynamic coefficients and aeroacoustics. Numerical computations are carried out for five different Mach numbers, M=2.0, M=2.5, M=3.0, M=3.5 and M=4.0. The results show that the Mach number affects the aerodynamics and aeroacoustics of the supersonic wing.",
author = "Marcel Ilie and Geoffrey Sullivan",
note = "Publisher Copyright: {\textcopyright} 2020, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.; AIAA AVIATION 2020 FORUM ; Conference date: 15-06-2020 Through 19-06-2020",
year = "2020",
doi = "10.2514/6.2020-2602",
language = "English",
isbn = "9781624105982",
series = "AIAA AVIATION 2020 FORUM",
publisher = "American Institute of Aeronautics and Astronautics Inc, AIAA",
booktitle = "AIAA AVIATION 2020 FORUM",
}