Fuel Combustion in Combustion Chambers of a Gas–Turbine Engine with a Rotating Injector

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Abstract

Specific features of combustion in combustion chambers of a gas-turbine engine with a rotating injector are considered. The region of the combustion site and the temperature field are found. A method for three-dimensional simulation of heat and mass transfer is described. The calculation results are compared with the temperature fields of real engines.

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