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undergraduate thesis
Optimiranje plinskoturbinskog kružnog ciklusa
2015. urn:nbn:hr:235:160622
Stanić, Tomislav
University of Zagreb
Faculty of Mechanical Engineering and Naval Architecture

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Stanić, T. (2015). Optimiranje plinskoturbinskog kružnog ciklusa (Undergraduate thesis). Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture. Retrieved from https://urn.nsk.hr/urn:nbn:hr:235:160622

Stanić, Tomislav. "Optimiranje plinskoturbinskog kružnog ciklusa." Undergraduate thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2015. https://urn.nsk.hr/urn:nbn:hr:235:160622

Stanić, Tomislav. "Optimiranje plinskoturbinskog kružnog ciklusa." Undergraduate thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2015. https://urn.nsk.hr/urn:nbn:hr:235:160622

Stanić, T. (2015). 'Optimiranje plinskoturbinskog kružnog ciklusa', Undergraduate thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, accessed 01 December 2024, https://urn.nsk.hr/urn:nbn:hr:235:160622

Stanić T. Optimiranje plinskoturbinskog kružnog ciklusa [Undergraduate thesis]. Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture; 2015 [cited 2024 December 01] Available at: https://urn.nsk.hr/urn:nbn:hr:235:160622

T. Stanić, "Optimiranje plinskoturbinskog kružnog ciklusa", Undergraduate thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, Zagreb, 2015. Available at: https://urn.nsk.hr/urn:nbn:hr:235:160622

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Metadata
TitleOptimiranje plinskoturbinskog kružnog ciklusa
Title (english)Optimization of gas turbine cycle
AuthorTomislav Stanić
MentorŽeljko Bogdan (mentor)
GranterUniversity of Zagreb
Faculty of Mechanical Engineering and Naval Architecture
Zagreb
Defense date and country2015-09-23, Croatia
Scientific / art field,
discipline and subdiscipline		TECHNICAL SCIENCES
Mechanical Engineering
Process Energy Engineering
Abstract
U ovom radu je analiziran plinsko-turbinski dio kombiniranog postrojenja. Kao referentni model, korišten je predložak rada asistenta na Katedri za energetska postrojenja i energetiku dr.sc.Mislava Čehila. U programskom paketu MATLAB napravljen je matematički model danog plinsko-turbinskog postrojenja koji obuhvaća modele kompresora, komore izgaranja i turbine. Algoritam rješavanja modela osigurava zadovoljavanje masenih i energetskih bilanci za zadano vanjsko opterećenje i temperaturu. Rezultati su uspoređeni s referentnim modelom te su prepoznati i objašnjeni uzroci promjene termodinamičke efikasnosti plinsko-turbinskog dijela postrojenja.
Abstract (english)
This paper analyzes the gas turbine combined plant part. As a reference model, used the template work assistant at the Department of Energy and Energy dr.sc.Mislava Čehila. The software package MATLAB created a mathematical model of a given gas-turbine plant which includes models of compressors, combustors and turbines. The algorithm solving model provides satisfying mass and energy balances for a given external load and temperature. The results are compared with the reference model and are recognized and explained the causes of the changes the thermodynamic efficiency of a gas turbine part of the plant.
Keywords
Keywords (english)
Languagecroatian
URN:NBNurn:nbn:hr:235:160622
Study programmeTitle: Mechanical Engineering
Study programme type: university
Study level: undergraduate
Academic / professional title: sveučilišni/a prvostupnik/ prvostupnica (baccalaureus/baccalaurea) inženjer/inženjerka strojarstva (sveučilišni/a prvostupnik/ prvostupnica (baccalaureus/baccalaurea) inženjer/inženjerka strojarstva)
Type of resourceText
File originBorn digital
Access conditionsOpen access
Terms of useLicence In copyright icon
Created on2019-05-22 14:46:25