Calculated research characteristics countercurrent combustion chamber of small GTE with the influence of the compressor and turbine

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This article presents the results of investigation of the compressor and turbine on the characteristics of the combustion chamber GTE. Identified the need to integrate the flow parameters of the compressor and the turbine inlet with three-dimensional numerical simulation of the combustion chamber. A method for designing combustion chambers GTE considering joint effect of engine components.

Mathematical model, combustor, compressor, turbine nozzle assembly, numerical modeling

Короткий адрес: https://sciup.org/148202668

IDR: 148202668

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