Preliminary numerical study of three-temperature model investigation of hypersonic oxygen flow under rotational nonequilibrium

Autor: Rabah Haoui, A. Chpoun, Y. Ghezali
Přispěvatelé: Université des Sciences et de la Technologie Houari Boumediene = University of Sciences and Technology Houari Boumediene [Alger] (USTHB), Laboratoire de Mécanique et d'Energétique d'Evry (LMEE), Université d'Évry-Val-d'Essonne (UEVE)-Université Paris-Saclay, University of Sciences and Technology Houari Boumediene [Alger] (USTHB)
Jazyk: angličtina
Rok vydání: 2021
Předmět:
Zdroj: Thermophysics and Aeromechanics
Thermophysics and Aeromechanics, 2021, 27 (6), pp.869-872. ⟨10.1134/S0869864320060086⟩
Thermophysics and Aeromechanics, MAIK Nauka/Interperiodica, 2021, 27 (6), pp.869-872. ⟨10.1134/S0869864320060086⟩
ISSN: 0869-8643
1531-8699
DOI: 10.1134/S0869864320060086⟩
Popis: International audience; The effect of rotational nonequilibrium on the macroscopic parameters of the flow behind a normal shock wave in oxygen gas flow has been examined. The electron thermal equilibrium was taken into account where the electron temperature was equal to the vibrational temperature according to Park’s assumption. Therefore, only the effect of rotational nonequilibrium on the translational and vibrational temperature was analyzed. Rotational and vibrational relaxation time for the O2-O2 and O2-O collisions proposed recently by Andrienko and Boyd are used. Also, the O2 dissociation rates proposed by Kim and Park are used. The results obtained with the three-temperature model well reproduce the data obtained in shock tube for the shock velocity of 4.44 km/s.
Databáze: OpenAIRE