A gas turbine combustion chamber modeling by physical model (CROSBI ID 296273)
Prilog u časopisu | izvorni znanstveni rad
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
nije evidentirano
nije evidentirano
nije evidentirano
nije evidentirano
nije evidentirano
nije evidentirano
Podaci o izdanju
35 (1)
2021.
30-35
objavljeno
1332-0718
1846-8438
Povezanost rada
nije evidentirano