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undergraduate thesis
Određivanje optimalne visine leta jednomotornog klipnog zrakoplova na odabranoj ruti
Zagreb: University of Zagreb, Faculty of Transport and Traffic Sciences, 2021. urn:nbn:hr:119:495464
Zorić, Marko
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

Zorić, M. (2021). Određivanje optimalne visine leta jednomotornog klipnog zrakoplova na odabranoj ruti (Undergraduate thesis). Zagreb: University of Zagreb, Faculty of Transport and Traffic Sciences. Retrieved from https://urn.nsk.hr/urn:nbn:hr:119:495464

Zorić, Marko. "Određivanje optimalne visine leta jednomotornog klipnog zrakoplova na odabranoj ruti." Undergraduate thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, 2021. https://urn.nsk.hr/urn:nbn:hr:119:495464

Zorić, Marko. "Određivanje optimalne visine leta jednomotornog klipnog zrakoplova na odabranoj ruti." Undergraduate thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, 2021. https://urn.nsk.hr/urn:nbn:hr:119:495464

Zorić, M. (2021). 'Određivanje optimalne visine leta jednomotornog klipnog zrakoplova na odabranoj ruti', Undergraduate thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, accessed 19 January 2025, https://urn.nsk.hr/urn:nbn:hr:119:495464

Zorić M. Određivanje optimalne visine leta jednomotornog klipnog zrakoplova na odabranoj ruti [Undergraduate thesis]. Zagreb: University of Zagreb, Faculty of Transport and Traffic Sciences; 2021 [cited 2025 January 19] Available at: https://urn.nsk.hr/urn:nbn:hr:119:495464

M. Zorić, "Određivanje optimalne visine leta jednomotornog klipnog zrakoplova na odabranoj ruti", Undergraduate thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, Zagreb, 2021. Available at: https://urn.nsk.hr/urn:nbn:hr:119:495464

Metadata
TitleOdređivanje optimalne visine leta jednomotornog klipnog zrakoplova na odabranoj ruti
Title (english)Determining the Optimum Flight Altitude of a Single-engine Piston Aircraft on the Selected Route
AuthorMarko Zorić
MentorPetar Andraši (mentor)
Committee memberDoris Novak (predsjednik povjerenstva)
Committee memberKarolina Krajček Nikolić (član povjerenstva)
Committee memberDavor Franjković (član povjerenstva)
GranterUniversity of Zagreb
Faculty of Transport and Traffic Sciences
(Division of Aeronautics)
(Department of Aeronautics)
Zagreb
Defense date and country2021-09-14, Croatia
Scientific / art field,
discipline and subdiscipline		TECHNICAL SCIENCES
Traffic and Transport Technology
Air Traffic
Abstract
Jednomotorni klipni zrakoplov služi za kratke rute te se njegov let sastoji od faze polijetanja te faze krstarenja i faze slijetanja. Za svaku od navedenih faza se rade proračuni vremena leta te potrošnje goriva, osim za fazu slijetanja u kojem je potrošnja goriva jednaka kao i u horizontalnom letu. Zapovjednik zrakoplova odabire visinu krstarenja na temelju performansi zrakoplova i na temelju podataka o smjeru i jačini vjetra na raznim visinama na ruti. U sadržaju ovog završnog rada objašnjen je odabir optimalne visine jednomotornog klipnog zrakoplova koja se temelji na izračunatim podatcima o potrošenom gorivu te vremenom leta na odabranoj ruti. Različite postavke snage utječu na brzinu zrakoplova što može uzrokovati manju ili veću potrošnju goriva na ruti te vrijeme leta.
Abstract (english)
Single engine piston aircraft is used for short routes and flight is composed of three phases which are climb, cruise and landing. For each of the phases, calculations must be made for flight time and fuel consumption, except for the landing phase because fuel consumption is the same as in horizontal flight. Commander of aircraft selects the cruise altitude based on the performance of aircraft and based on wind direction and velocity at various altitudes on the route. The content of this final paper explains the optimal height selection of a single piston engine aircraft based on calculated data of fuel consumption and flight time on the seleted route. Different power settings affect the speed of the aircraft which can cause less or more fuel consumption on the route and flight time.
Keywords
Keywords (english)
Languagecroatian
URN:NBNurn:nbn:hr:119:495464
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 on2021-10-11 12:34:42