Theoretical and experimental investigations of the working processes in a gas turbine combustor with steam injection have been conducted. Selected concept of a gas turbine combustor can provide higher performance, wider turn down ratios, lower emission of nitrogen oxides, demonstrate satisfactory major gravimetric and volumetric parameters. Obtained results and recommendations can be used for the gas turbine combustor operation modes modeling, geometry optimization, prospective propulsion and power generation units design and engineering.

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