Pregled bibliografske jedinice broj: 1134592
A gas turbine combustion chamber modeling by physical model
A gas turbine combustion chamber modeling by physical model // Pomorstvo : scientific journal of maritime research, 35 (2021), 1; 30-35 (podatak o recenziji nije dostupan, članak, znanstveni)
CROSBI ID: 1134592 Za ispravke kontaktirajte CROSBI podršku putem web obrasca
Naslov
A gas turbine combustion chamber modeling by physical model
Autori
Glavan, Ivica ; Poljak, Igor ; Kosor, Mate
Izvornik
Pomorstvo : scientific journal of maritime research (1332-0718) 35
(2021), 1;
30-35
Vrsta, podvrsta i kategorija rada
Radovi u časopisima, članak, znanstveni
Ključne riječi
Gas turbine ; Combustion chamber ; Combustion temperature ; Modelica ; SimulationX
Sažetak
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.
Izvorni jezik
Engleski
Citiraj ovu publikaciju:
Časopis indeksira:
- Web of Science Core Collection (WoSCC)
- Emerging Sources Citation Index (ESCI)
- Scopus
