@inproceedings{aedb145a08cc4de7be9d902d35611434,
title = "Nitric Oxide Infrared Radiation Modeling from a Hypersonic Flow",
abstract = "Nitric Oxide (NO) Infrared (IR) radiation modeling is performed for a hypersonic flow at M=7.2 over a cylinder case. The flowfield results for the base flow is calculated using the Direct Simulation Monte Carlo (DSMC) method. A collisional radiative model is constructed to obtain accurate results for the vibrational level populations of NO. This collisional radiative model will be incorporated to a mass transport equation solver (MassTR) as a source term that couples the radiation with the flow.",
author = "Karpuzcu, {Irmak T.} and Shubham Thirani and Levin, {Deborah A.} and Daniil Andrienko",
note = "Publisher Copyright: {\textcopyright} 2022, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.; AIAA AVIATION 2022 Forum ; Conference date: 27-06-2022 Through 01-07-2022",
year = "2022",
doi = "10.2514/6.2022-3501",
language = "English (US)",
isbn = "9781624106354",
series = "AIAA AVIATION 2022 Forum",
publisher = "American Institute of Aeronautics and Astronautics Inc, AIAA",
booktitle = "AIAA AVIATION 2022 Forum",
}