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undergraduate thesis
Matematički model elisno - mlaznog motora za određivanje performansi zrakoplova u ravnotežnom letu
Zagreb: University of Zagreb, Faculty of Transport and Traffic Sciences, 2016. urn:nbn:hr:119:178792
Đurinović, Juraj
University of Zagreb
Faculty of Transport and Traffic Sciences
Division of Aeronautics
Department of Aeronautics

Institutional repository: Faculty of Transport and Traffic Sciences

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Đurinović, J. (2016). Matematički model elisno - mlaznog motora za određivanje performansi zrakoplova u ravnotežnom letu (Undergraduate thesis). Zagreb: University of Zagreb, Faculty of Transport and Traffic Sciences. Retrieved from https://urn.nsk.hr/urn:nbn:hr:119:178792

Đurinović, Juraj. "Matematički model elisno - mlaznog motora za određivanje performansi zrakoplova u ravnotežnom letu." Undergraduate thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, 2016. https://urn.nsk.hr/urn:nbn:hr:119:178792

Đurinović, Juraj. "Matematički model elisno - mlaznog motora za određivanje performansi zrakoplova u ravnotežnom letu." Undergraduate thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, 2016. https://urn.nsk.hr/urn:nbn:hr:119:178792

Đurinović, J. (2016). 'Matematički model elisno - mlaznog motora za određivanje performansi zrakoplova u ravnotežnom letu', Undergraduate thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, accessed 26 November 2024, https://urn.nsk.hr/urn:nbn:hr:119:178792

Đurinović J. Matematički model elisno - mlaznog motora za određivanje performansi zrakoplova u ravnotežnom letu [Undergraduate thesis]. Zagreb: University of Zagreb, Faculty of Transport and Traffic Sciences; 2016 [cited 2024 November 26] Available at: https://urn.nsk.hr/urn:nbn:hr:119:178792

J. Đurinović, "Matematički model elisno - mlaznog motora za određivanje performansi zrakoplova u ravnotežnom letu", Undergraduate thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, Zagreb, 2016. Available at: https://urn.nsk.hr/urn:nbn:hr:119:178792

Metadata
TitleMatematički model elisno - mlaznog motora za određivanje performansi zrakoplova u ravnotežnom letu
Title (english)Mathematical Model of Turboprop Engine for Determing Aircraft Performance in Steady Flight
AuthorJuraj Đurinović
MentorAnita Domitrović (mentor)
Committee memberErnest Bazijanac (predsjednik povjerenstva)
Committee memberKarolina Krajček Nikolić (član povjerenstva)
Committee memberDoris Novak (član povjerenstva)
GranterUniversity of Zagreb
Faculty of Transport and Traffic Sciences
(Division of Aeronautics)
(Department of Aeronautics)
Zagreb
Defense date and country2016-07-05, Croatia
Scientific / art field,
discipline and subdiscipline		TECHNICAL SCIENCES
Traffic and Transport Technology
Air Traffic
Abstract
U ovom završnom radu dan je matematički model elisno-mlaznog motora koji može poslužiti za izračun snage motora u ravnotežnom letu zrakoplova. Općenito se opisuje konstrukcija mlaznih, odnosno elisno-mlaznih motora i dodatno se iznose karakteristike na primjeru motora ugrađenog na zrakoplov DASH 8 Q 400, odnosno motora P&W150A. Objašnjava se horizontalni let zrakoplova i postavljaju se uvjeti ravnoteže. Definiran je matematički model motora i prikazani su dijagrami koji prikazuju ovisnost potiska, snage, specifične potrošnje goriva i masenog protoka zraka o brzini zrakoplova, odnosno Machovom broju.
Abstract (english)
This thesis analyses mathematical model of turboprop engine which can be used for calculating power of engine in aircraft steady flight. Construction of turboprop engine is described in general and also on example of DASH 8 Q 400's engine, P&W150A. Steady flight of aircraft is explained and balance terms are derived. Mathematical model of turboprop engine is developed and figures of variation of thrust, power, specific fuel consumption and mass flow are shown dependent on aircraft speed - Mach number.
Keywords
Keywords (english)
Languagecroatian
URN:NBNurn:nbn:hr:119:178792
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 on2016-07-08 09:52:27