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A gas turbine combustion chamber modeling by physical model (CROSBI ID 296273)

Prilog u časopisu | izvorni znanstveni rad

Glavan, Ivica ; Poljak, Igor ; Kosor, Mate A gas turbine combustion chamber modeling by physical model // Pomorstvo : scientific journal of maritime research, 35 (2021), 1; 30-35

Podaci o odgovornosti

Glavan, Ivica ; Poljak, Igor ; Kosor, Mate

engleski

A gas turbine combustion chamber modeling by physical model

The validity of the gas turbine unit model largely depends on the accuracy of the flue gas temperature value calculation at the gas turbine inlet (TIT). This temperature is determined by the maximum combustion temperature. In variable running mode, the temperature value is regulated by changing the ratio of air and fuel at the inlet to the combustion chamber. The paper presents a model of a gas turbine combustion chamber using Modelica, an object-oriented language for modeling complex physical systems with the aim of determining the temperature of combustion flue gases, specific heat capacity, enthalpy, and flue gas composition at different gas turbine loads.

Gas turbine ; Combustion chamber ; Combustion temperature ; Modelica ; SimulationX

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Podaci o izdanju

35 (1)

2021.

30-35

objavljeno

1332-0718

1846-8438

Povezanost rada

nije evidentirano

Indeksiranost