Результаты поиска по 'plasma-assisted combustion':
Найдено статей: 2
  1. Firsov A.A., Isaenkov Yu.I., Krupskiy M.G., Rudakov V.Yu., Filimonova E.A., Yarantsev D.A., Leonov S.B.
    Nonequilibrium initiation of volumetric combustion in a combustion engine: modeling and experimental setup
    Computer Research and Modeling, 2014, v. 6, no. 6, pp. 911-922

    The paper presents results of experimental, computational and analytical study of the effect of nonequilibrium chemical activation of air-fuel mixture on effectiveness of Diesel process. The generation of a high-voltage multi-streamer discharge in combustion chamber at the compression phase is considered as the method of the activation. The description of electrical discharge system, results of measurement and visualization are presented. The plasma-chemical kinetics of nonequilibrium ignition is analyzed to establish a passway for a proper reduction of chemical kinetics scheme. The results of numerical simulation of gas dynamic processes at presence of plasma-assisted combustion in a geometrical configuration close to the experimental one are described.

    Keywords: combustion, internal combustion engine, streamer discharge, chemical kinetics, computational fluid dynamics, numerical simulation.
    Views (last year): 3. Citations: 4 (RSCI).
  2. Firsov A.A., Yarantsev D.A., Leonov S.B., Ivanov V.V.
    Numerical simulation of ethylene combustion in supersonic air flow
    Computer Research and Modeling, 2017, v. 9, no. 1, pp. 75-86

    In the present paper, we discuss the possibility of a simplified three-dimensional unsteady simulation of plasma-assisted combustion of gaseous fuel in a supersonic airflow. Simulation was performed by using FlowVision CFD software. Analysis of experimental geometry show that it has essentially 3D nature that conditioned by the discrete fuel injection into the flow as well as by the presence of the localized plasma filaments. Study proposes a variant of modeling geometry simplification based on symmetry of the aerodynamic duct and periodicity of the spatial inhomogeneities. Testing of modified FlowVision $k–\varepsilon$ turbulence model named «KEFV» was performed for supersonic flow conditions. Based on that detailed grid without wall functions was used the field of heat and near fuel injection area and surfaces remote from the key area was modeled with using of wall functions, that allowed us to significantly reduce the number of cells of the computational grid. Two steps significantly simplified a complex problem of the hydrocarbon fuel ignition by means of plasma generation. First, plasma formations were simulated by volumetric heat sources and secondly, fuel combustion is reduced to one brutto reaction. Calibration and parametric optimization of the fuel injection into the supersonic flow for IADT-50 JIHT RAS wind tunnel is made by means of simulation using FlowVision CFD software. Study demonstrates a rather good agreement between the experimental schlieren photo of the flow with fuel injection and synthetical one. Modeling of the flow with fuel injection and plasma generation for the facility T131 TSAGI combustion chamber geometry demonstrates a combustion mode for the set of experimental parameters. Study emphasizes the importance of the computational mesh adaptation and spatial resolution increasing for the volumetric heat sources that model electric discharge area. A reasonable qualitative agreement between experimental pressure distribution and modeling one confirms the possibility of limited application of such simplified modeling for the combustion in high-speed flow.

    Keywords: combustion in supersonic flow, numerical simulation, direct current discharge, plasma-assisted combustion.
    Views (last year): 8. Citations: 3 (RSCI).

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