prikaz prve stranice dokumenta A gas turbine combustion chamber modeling by physical model
  Download
PDF 2.96 MB
Scientific paper - Preliminary note / Short communication
A gas turbine combustion chamber modeling by physical model
Pomorstvo, 35 (2021), 1; 30-35. https://doi.org/10.31217/p.35.1.4
Glavan, Ivica; Poljak, Igor; Kosor, Mate

Cite this document

Glavan, I., Poljak, I. & Kosor, M. (2021). A gas turbine combustion chamber modeling by physical model. Pomorstvo, 35. (1), 30-35. doi: 10.31217/p.35.1.4

Glavan, Ivica, et al. "A gas turbine combustion chamber modeling by physical model." Pomorstvo, vol. 35, no. 1, 2021, pp. 30-35. https://doi.org/10.31217/p.35.1.4

Glavan, Ivica, Igor Poljak and Mate Kosor. "A gas turbine combustion chamber modeling by physical model." Pomorstvo 35, no. 1 (2021): 30-35. https://doi.org/10.31217/p.35.1.4

Glavan, I., Poljak, I. and Kosor, M. (2021) 'A gas turbine combustion chamber modeling by physical model', Pomorstvo, 35(1), pp. 30-35. doi: 10.31217/p.35.1.4

Glavan I, Poljak I, Kosor M. A gas turbine combustion chamber modeling by physical model. Pomorstvo [Internet]. 2021 June [cited 2024 July 03];35(1):30-35. doi: 10.31217/p.35.1.4

I. Glavan, I. Poljak and M. Kosor, "A gas turbine combustion chamber modeling by physical model", Pomorstvo, vol. 35, no. 1, pp. 30-35, June 2021. [Online]. Available at: https://urn.nsk.hr/urn:nbn:hr:187:360913. [Accessed: 03 July 2024]

Please login to the repository to save this object to your list.
Metadata
Title (english)A gas turbine combustion chamber modeling by physical model
AuthorIvica Glavan https://orcid.org/0000-0002-7067-4460
AuthorIgor Poljak https://orcid.org/0000-0001-8749-4223
AuthorMate Kosor
Author's institutionUniversity of Rijeka
Faculty of Maritime Studies, Rijeka
Scientific / art field,
discipline and subdiscipline		TECHNICAL SCIENCES
Traffic and Transport Technology
Abstract (english)
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.
Keywords (english)
Languageenglish
Publication typeScientific paper - Preliminary note / Short communication
Publication statusPublished
Peer reviewPeer review
Publication versionPublished version
Journal titlePomorstvo
Numberingvol. 35, no. 1, pp. 30-35
p-ISSN1332-0718
e-ISSN1846-8438
DOIhttps://doi.org/10.31217/p.35.1.4
URN:NBNurn:nbn:hr:187:360913
Publication2021-06
Document URLhttps://hrcak.srce.hr/259310
Type of resourceText
Access conditionsOpen access
Terms of useLicence In copyright icon
Created on2022-02-25 10:54:08