Aircraft Engineering
Аuthors
1*, 2**, 3***1. Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia
2. Ishlinsky Institute for Problems in Mechanics of the Russian Academy of Sciences, 101-1, prospekt Vernadskogo, Moscow, 119526, Russia
3. Lomonosov Moscow State University, 1, Leninskie Gory, Moscow, 119991, Russia
*e-mail: larinaelenav@gmail.com
**e-mail: kryukov@ipmnet.ru
***e-mail: ivanovmai@mail.ru
Abstract
The problem of homogenous isotropic turbulence interaction with steady normal shock is considered. Comparison of some variants of k- 8 - and к- CO -models is presented. Special attention was paid to influence different non-equilibrium modifications of the models on turbulence level increasing behind the shock.Keywords:
viscous gas flow, turbulence, two-parametrical models of turbulence, shock wave, non-equilibrium turbulence.
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