This paper presents a model of working processes in the combustion chambers of micro gas turbine engines, taking into account turbulence, combustion, the detailed mechanism of chemical reactions, radiation, swirling flow, and the presence of oil in the fuel mixture. The results of calculations and experiments with the combustion chamber of the JetCat P100-RX engine are presented. Estimates of the addition of oil to fuel for fuel consumption are given.
Numerical Simulation of Performance of Micro Gas Turbine Engine Combustion Chamber Taking into Account Oil Addition to Fuel
Russ. Aeronaut.
Russian Aeronautics ; 67 , 3 ; 594-600
01.09.2024
7 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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