This article is cited in 9 scientific papers (total in 9 papers)
Simulation of stochastic pulsating flows with instabilities using minimum-stencil difference schemes
O. A. Azarova
Dorodnicyn Computing Center, Russian Academy of Sciences,
ul. Vavilova 40, Moscow, 119333, Russia
Pulsating flows with contact discontinuity instabilities and generated regions of turbulent-like gas parameter fluctuations were numerically simulated. The flows were driven by the interaction of an infinite heated rarefied channel with a shock layer. Pulsating flow regimes were analyzed for an energy source located symmetrically or asymmetrically relative to the body. Averaged steady flows characterized by stagnation point oscillations about a new position at the end face were examined, and steady-state flow structures with gas parameter nonmonotonicities near the body end face were studied. The simulation was based on minimum-stencil modified schemes.
minimum-stencil difference scheme, Richtmyer–Meshkov instability, tangential discontinuity instability, pulsating flow, turbulent-like pulsations.
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Computational Mathematics and Mathematical Physics, 2009, 49:8, 1397–1414
O. A. Azarova, “Simulation of stochastic pulsating flows with instabilities using minimum-stencil difference schemes”, Zh. Vychisl. Mat. Mat. Fiz., 49:8 (2009), 1466–1483; Comput. Math. Math. Phys., 49:8 (2009), 1397–1414
Citation in format AMSBIB
\paper Simulation of stochastic pulsating flows with instabilities using minimum-stencil difference schemes
\jour Zh. Vychisl. Mat. Mat. Fiz.
\jour Comput. Math. Math. Phys.
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Azarova O. Knight D. Kolesnichenko Yu., “Flow Control via Instabilities, Vortices and Steady Structures Under the Action of External Microwave Energy Release”, Proc. Inst. Mech. Eng. Part G-J. Aerosp. Eng., 227:9 (2013), 1498–1515
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O. A. Azarova, “Complex conservative difference schemes for computing supersonic flows past simple aerodynamic forms”, Comput. Math. Math. Phys., 55:12 (2015), 2025–2049
Azarova O.A. Gvozdeva L.G., “Unsteady triple-shock configurations and vortex contact structures initiated by the interaction of an energy source with a shock layer in gases”, Tech. Phys. Lett., 42:8 (2016), 799–803
Azarova O.A. Gvozdeva L.G., “Control of Triple-Shock Configurations and Vortex Structures Forming in High Speed Flows of Gaseous Media past an AD Body under the Action of External Energy Sources ?”, Aerospace, 4:1 (2017), 9
Azarova O.A. Erofeev A.V. Lapushkina T.A., “A Comparison of Plasma and Thermal Effects Upon Supersonic Flow Past Aerodynamic Bodies”, Tech. Phys. Lett., 43:4 (2017), 405–408
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