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undergraduate thesis
Konstrukcija i performanse motora Snecma M88 na zrakoplovu Dassault Rafale
Zagreb: University of Zagreb, Faculty of Transport and Traffic Sciences, 2023. urn:nbn:hr:119:374718
Kodrić, Ivan
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

Kodrić, I. (2023). Konstrukcija i performanse motora Snecma M88 na zrakoplovu Dassault Rafale (Undergraduate thesis). Zagreb: University of Zagreb, Faculty of Transport and Traffic Sciences. Retrieved from https://urn.nsk.hr/urn:nbn:hr:119:374718

Kodrić, Ivan. "Konstrukcija i performanse motora Snecma M88 na zrakoplovu Dassault Rafale." Undergraduate thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, 2023. https://urn.nsk.hr/urn:nbn:hr:119:374718

Kodrić, Ivan. "Konstrukcija i performanse motora Snecma M88 na zrakoplovu Dassault Rafale." Undergraduate thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, 2023. https://urn.nsk.hr/urn:nbn:hr:119:374718

Kodrić, I. (2023). 'Konstrukcija i performanse motora Snecma M88 na zrakoplovu Dassault Rafale', Undergraduate thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, accessed 22 December 2024, https://urn.nsk.hr/urn:nbn:hr:119:374718

Kodrić I. Konstrukcija i performanse motora Snecma M88 na zrakoplovu Dassault Rafale [Undergraduate thesis]. Zagreb: University of Zagreb, Faculty of Transport and Traffic Sciences; 2023 [cited 2024 December 22] Available at: https://urn.nsk.hr/urn:nbn:hr:119:374718

I. Kodrić, "Konstrukcija i performanse motora Snecma M88 na zrakoplovu Dassault Rafale", Undergraduate thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, Zagreb, 2023. Available at: https://urn.nsk.hr/urn:nbn:hr:119:374718

Metadata
TitleKonstrukcija i performanse motora Snecma M88 na zrakoplovu Dassault Rafale
Title (english)Design and Performance of the Snecma M88 Engine on the Dassault Rafale Aircraft
AuthorIvan Kodrić
MentorAnita Domitrović (mentor)
Committee memberKarolina Krajček Nikolić (predsjednik povjerenstva)
Committee memberDavor Franjković (član povjerenstva)
Committee memberErnest Bazijanac (član povjerenstva)
GranterUniversity of Zagreb
Faculty of Transport and Traffic Sciences
(Division of Aeronautics)
(Department of Aeronautics)
Zagreb
Defense date and country2023-09-20, Croatia
Scientific / art field,
discipline and subdiscipline		TECHNICAL SCIENCES
Traffic and Transport Technology
Air Traffic
Abstract
U ovom završnom radu opisuju se konstrukcijske karakteristike i performanse mlaznih motora za borbene zrakoplove na primjeru turbo ventilatorskog motora sa naknadnim izgaranjem Snecma M88 koji je ugrađen na borbenom zrakoplovu Dassault Rafale. Prikazan je idealni Braytonov ciklus za mlazni motor i za mlazni motor sa naknadnim izgaranjem. Prikazan je matematički model za izračun potiska ove vrste mlaznih motora. Ovisnost potiska o eksploatacijskim parametrima prikazana je pomoću dijagrama.
Abstract (english)
This thesis is created to describe structural characteristics and performance of jet engines constructed for fighter planes on an example of a jet engine with afterburner capability Snecma M88 engine which is installed and used on Dassault Rafale aircraft. Ideal Brayton cycle has been shown for turbojet engines and turbojet engines with afterburners. Mathematical model is presented for calculating the thrust on this type of engine. The dependence of thrust on the exploitation parameters which are shown using diagrams.
Keywords
Keywords (english)
Languagecroatian
URN:NBNurn:nbn:hr:119:374718
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 on2023-10-19 13:21:53