@inproceedings{8a312e0e465b4d7da29b9f6568694b6c,
title = "Numerical analysis of the aerodynamic heating in hypersonic thermo-chemical nonequilibrium flows",
abstract = "A series of typical points of a hypersonic flight trajectory with Ma from 8 to 22 and altitudes from 47.8km to 72.8km for a R=0.4m sphere are simulated by solving conservative Navier-Stokes equations including thermo-chemical nonequilibium effects. Results illustrate that different thermodynamic and chemical kinetic models almost have no impacts on the prediction of the aerodynamic heating in the hypersonic nonequilibrium flow. It is also found that there is only 10% difference on the heat transfer calculation between two thermal conductivity models: Eucken relation and Gupta fitting formula.",
author = "Jingying Wang and Jiaao Hao and Guangsheng Du",
note = "Funding Information: This work is supported by the Natural Science Foundation of Shandong Province, China (Grant No. ZR2016AB06). Publisher Copyright: {\textcopyright} 2017, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved. Copyright: Copyright 2020 Elsevier B.V., All rights reserved.; 21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017 ; Conference date: 06-03-2017 Through 09-03-2017",
year = "2017",
doi = "10.2514/6.2017-2222",
language = "English",
isbn = "9781624104633",
series = "21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017",
publisher = "American Institute of Aeronautics and Astronautics Inc, AIAA",
booktitle = "21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017",
}