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undergraduate thesis
Matematički model performansi mlaznog motora s naknadnim izgaranjem
Zagreb: University of Zagreb, Faculty of Transport and Traffic Sciences, 2017. urn:nbn:hr:119:385455
Zrinski, Petar
University of Zagreb
Faculty of Transport and Traffic Sciences
Division of Aeronautics
Department of Aeronautics

Institutional repository: Faculty of Transport and Traffic Sciences

Cite this document

Zrinski, P. (2017). Matematički model performansi mlaznog motora s naknadnim izgaranjem (Undergraduate thesis). Zagreb: University of Zagreb, Faculty of Transport and Traffic Sciences. Retrieved from https://urn.nsk.hr/urn:nbn:hr:119:385455

Zrinski, Petar. "Matematički model performansi mlaznog motora s naknadnim izgaranjem." Undergraduate thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, 2017. https://urn.nsk.hr/urn:nbn:hr:119:385455

Zrinski, Petar. "Matematički model performansi mlaznog motora s naknadnim izgaranjem." Undergraduate thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, 2017. https://urn.nsk.hr/urn:nbn:hr:119:385455

Zrinski, P. (2017). 'Matematički model performansi mlaznog motora s naknadnim izgaranjem', Undergraduate thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, accessed 28 December 2024, https://urn.nsk.hr/urn:nbn:hr:119:385455

Zrinski P. Matematički model performansi mlaznog motora s naknadnim izgaranjem [Undergraduate thesis]. Zagreb: University of Zagreb, Faculty of Transport and Traffic Sciences; 2017 [cited 2024 December 28] Available at: https://urn.nsk.hr/urn:nbn:hr:119:385455

P. Zrinski, "Matematički model performansi mlaznog motora s naknadnim izgaranjem", Undergraduate thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, Zagreb, 2017. Available at: https://urn.nsk.hr/urn:nbn:hr:119:385455

Metadata
TitleMatematički model performansi mlaznog motora s naknadnim izgaranjem
Title (english)Mathematical Model of Turbojet Afterburner Engine Performance
AuthorPetar Zrinski
MentorAnita Domitrović (mentor)
Committee memberErnest Bazijanac (predsjednik povjerenstva)
Committee memberTomislav Radišić (član povjerenstva)
Committee memberTino Bucak (član povjerenstva)
GranterUniversity of Zagreb
Faculty of Transport and Traffic Sciences
(Division of Aeronautics)
(Department of Aeronautics)
Zagreb
Defense date and country2017-07-04, Croatia
Scientific / art field,
discipline and subdiscipline		TECHNICAL SCIENCES
Traffic and Transport Technology
Air Traffic
Abstract
U ovom završnom radu opisuje se rad mlaznih motora i pojedinačnih komponenti mlaznih motora s naknadnim izgaranjem na primjeru motora Tumansky R25 – 300 koji se upotrebljava na zrakoplovu MIG 21 bis. Prikazan je idealni Braytonov ciklus za mlazni motor i mlazni motor s naknadnim izgaranjem. Također je izrađen matematički model kojim se mogu izračunati performanse mlaznog motora u različitim uvjetima eksploatacije. Dijagrami prikazuju potisak, specifičnu potrošnju goriva i maseni protok zraka kod referentnog motora u području podzvučnih brzina i u uvjetima standardne atmosfere. U prilogu rada nalazi se izvorni kod za matematički model.
Abstract (english)
The aim of this thesis is to describe the work cycle of turbojet engines as well as the functioning of individual components of turbojet engines with afterburning using the example of the engine Tumansky R25 – 300 which is usually found on the aircraft MIG 21 bis. The thesis shows an ideal Brayton cycle for a turbojet and a turbojet with afterburning. A mathematical model is provided which can be used to calculate the performances of a turbojet engine in different off-design conditions. The charts show the thrust, specific fuel consumption and air mass flow of the given engine at subsonic speeds and in ISA conditions. In the appendix of the thesis the source code for the aforementioned mathematical model can be found.
Keywords
Keywords (english)
Languagecroatian
URN:NBNurn:nbn:hr:119:385455
Study programmeTitle: Aeronautics
Study programme type: university
Study level: undergraduate
Academic / professional title: sveučilišni/a prvostupnik/prvostupnica (baccalaureus/baccalaurea) inženjer/inženjerka aeronautike (sveučilišni/a prvostupnik/prvostupnica (baccalaureus/baccalaurea) inženjer/inženjerka aeronautike)
Type of resourceText
File originBorn digital
Access conditionsOpen access
Terms of useLicence In copyright icon
Created on2017-07-05 16:55:06