Thermochemical Modeling in Hypersonic Reactive Flow Behind Strong Shock Wave
Author:
Publisher
Springer International Publishing
Link
http://link.springer.com/content/pdf/10.1007/978-3-030-11827-3_3
Reference10 articles.
1. Allouche R, Haoui R, Renane R (2014) Numerical simulation of reactive flow in non-equilibrium behind a strong shock wave during re-entry into earth’s atmosphere. J Mech Ind 15:81–87. https://doi.org/10.1051/meca/2014002
2. Candler GV, Park C. (1988) The computation of radiation from nonequilibrium hypersonic flows, AIAA 1988-2678. https://doi.org/10.2514/6.1988-2678
3. Casseau V, Palharini R, Scanlon T, Brown R (2016) A two-temperature open-source cfd model for hypersonic reacting flows, part one: zero-dimensional analysis. Aerospace 3(4):34. https://doi.org/10.3390/aerospace3040034
4. Furudate M, Suzuki T, Sawada K, (2000) Calculation of intermediate hypersonic flow using multi-temperature model, AIAA 2000–0343. https://doi.org/10.2514/6.2000-343
5. Panesi M, Magin T, Bourdon A, Bultel A, Chazot O (2009) Analysis of the FIRE II flight experiment by means of a collisional radiative model. J Thermophys Heat Transfer 23:236–248. https://doi.org/10.2514/1.39034
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