@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 = "The research is being performed at the University of Illinois Urbana-Champaign is supported by the Air Force Office of Scientific Research through AFOSR Grant No. FA9550-19-1-0342. Computational resources for this research is provided by the National Science Foundation TACC{\textquoteright}s Stampede2 supercomputer, which is a part of XSEDE, with the project number TG-ATM200010. The authors are also thankful to Dr. Daniil Andrienko and Alexander Fangman for providing the QCT rates for NO vibrational relaxation. The authors would also like to thank Drs. Sergey F. Gimelshein and Ingrid Wysong for providing the Bias-LB model setup and useful discussions.; 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",
}