Search Results - "Borovik, I. N."

Processes in an Oxygen–Methane Combustion Chamber with Gaseous Fuel by Mukambetov, R. Ya, Borovik, I. N.

“…The processes in an oxygen–methane combustion chamber with gaseous fuel are studied by three-dimensional numerical modeling. The advantages and disadvantages…”
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Simulation of continuous spin detonation in an annular combustion chamber in two-dimensional statement by Borovik, I. N., Farizanov, I. R., Yanovskii, L. S.

“…The article presents the results of a numerical simulation of the phenomenon of continuous spin detonation in a hydrogen-oxygen mixture in two-dimensional…”
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Numerical Study of the Effect of Turbulent Schmidt Number on the Numerical Simulation of Processes in the Multi-Element GCH4-GO2 Combustor by Tyul’kov, K. V., Strokach, E. A., Borovik, I. N., Blyakharskii, S. S., Sternin, A.

“…In this paper, the influence of the diffusion coefficient in the transport equation of the mass fractions is studied. The solution of the Favre-averaged…”
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Application of the Implicit MacCormack Scheme for Computation of Supersonic Turbulent Jets Using the Parabolized Navier—Stokes Equations by Molchanov, A. M., Myakochin, A. S., Borovik, I. N., Tushkanov, A. S.

“…An effective unconditionally stable numerical method for solving equations describing the flow of supersonic turbulent jets is developed. The method does not…”
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Self-Ignition of Fuel Consisting of Hydrogen Peroxide, Kerosene, and Pyrophoric Additives by Kozlov, A. A., Borovik, I. N., Ermashkevich, A. A., Tashev, V. P., Guseinov, Sh. L., Kosykh, V. A.

“…—The possibility of creating an environmentally safe self-igniting fuel mixture for liquid-propellant rocket engines is investigated. The mixture is based on…”
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Fuel preparation and combustion in rocket and jet engines by Brenn, G., Kozlov, A. A., Borovik, I. N., Strokach, E. A.

“…A method is proposed for investigating the processes in the combustion chamber of chemical heat engines. In this method, the processes in the combustion…”
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Numerical Study of the Influence of Turbulent Diffusion Coefficients and Turbulent Prandtl Number on the Reactive Flow Simulation in a Combustor by Zhukov, V. P., Borovik, I. N., Strokach, E. A.

“…The influence of the k –ε–RNG model parameters is studied in terms of simulation of processes in the combustor with the gas oxygen and methane inside including…”
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Analysis of nonstationary thermal state of a low-thrust liquid rocket engine taking into account injection, evaporation and combustion of liquid fuel droplets by Vorobiev, A. G., Borovik, I. N., Ha, Song-Up

“…The physico-chemical state of reaction products in the combustion chamber of a liquid rocket engine of 500N thrust with account for the evaporation of liquid…”
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Analysis of nonstationary thermal state of low-thrust liquid rocket engine with high-concentration hydrogen peroxide and kerosene propellant with film cooling by Vorobiev, A. G., Borovik, I. N., Ha, Song-Up

“…The paper presents an analysis of the nonstationary thermal state of a low-thrust liquid rocket engine with HTHP (high-test hydrogen peroxide) and kerosene…”
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