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undergraduate thesis
Određivanje utjecaja stupnja optočnosti na perfomanse mlaznog motora
Zagreb: University of Zagreb, Faculty of Transport and Traffic Sciences, 2017. urn:nbn:hr:119:405477
Petrin, David
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

Petrin, D. (2017). Određivanje utjecaja stupnja optočnosti na perfomanse mlaznog motora (Undergraduate thesis). Zagreb: University of Zagreb, Faculty of Transport and Traffic Sciences. Retrieved from https://urn.nsk.hr/urn:nbn:hr:119:405477

Petrin, David. "Određivanje utjecaja stupnja optočnosti na perfomanse mlaznog motora." Undergraduate thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, 2017. https://urn.nsk.hr/urn:nbn:hr:119:405477

Petrin, David. "Određivanje utjecaja stupnja optočnosti na perfomanse mlaznog motora." Undergraduate thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, 2017. https://urn.nsk.hr/urn:nbn:hr:119:405477

Petrin, D. (2017). 'Određivanje utjecaja stupnja optočnosti na perfomanse mlaznog motora', Undergraduate thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, accessed 05 November 2024, https://urn.nsk.hr/urn:nbn:hr:119:405477

Petrin D. Određivanje utjecaja stupnja optočnosti na perfomanse mlaznog motora [Undergraduate thesis]. Zagreb: University of Zagreb, Faculty of Transport and Traffic Sciences; 2017 [cited 2024 November 05] Available at: https://urn.nsk.hr/urn:nbn:hr:119:405477

D. Petrin, "Određivanje utjecaja stupnja optočnosti na perfomanse mlaznog motora", Undergraduate thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, Zagreb, 2017. Available at: https://urn.nsk.hr/urn:nbn:hr:119:405477

Metadata
TitleOdređivanje utjecaja stupnja optočnosti na perfomanse mlaznog motora
Title (english)Effect of Bypass Ratio on Turbofan Engine Performance
AuthorDavid Petrin
MentorAnita Domitrović (mentor)
Committee memberErnest Bazijanac (predsjednik povjerenstva)
Committee memberDavor Franjković (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 country2017-09-12, Croatia
Scientific / art field,
discipline and subdiscipline		TECHNICAL SCIENCES
Traffic and Transport Technology
Air Traffic
Abstract
Rad opisuje prednosti primjene zrakoplovnih turbomlaznih motora s visokim stupnjem optočnosti u odnosu na ostale tipove mlaznih motora. Princip rada optočnog mlaznog motora i pojedini dijelovi motora prikazani su na primjeru dvovratilnog optočnog mlaznog motora s visokim stupnjem optočnosti CFM56-B. Opisan je ciklus rada optočnog mlaznog motora i matematički su formulirani izrazi za potisak, iskoristivost, specifičnu potrošnju goriva i ostali parametri koji se koriste za procjenu rada mlaznih motora. Posebno je istaknut utjecaj stupnja optočnosti na performanse mlaznog motora. Prikazani su i mogući pravci razvoja optočnih mlaznih motora u svrhu smanjenja operativnih troškova i poboljšanja njihovih karakteristika.
Abstract (english)
This thesis describes advantages of application of high-bypass turbofan engines in reference to other turbo engine types. Working principle of the turbofan engine and individual engine components are explained using the example of two-spool, high-bypass turbofan engine CFM56-B. The working cycle of high-bypass gas turbine engine is described using mathematical model for thrust, efficiency, thrust specific fuel consumption and other parameters used for jet engine rating. Special attention is given to the effect of bypass ratio on jet engine performance. Probable future developments of high-bypass turbofan engines concerning reduced operational costs and performance improvements are described as well.
Keywords
Keywords (english)
Languagecroatian
URN:NBNurn:nbn:hr:119:405477
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 on2017-09-19 12:17:24