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undergraduate thesis
Izračun performansi zrakoplova Dash 8 Q400 u penjanju
Zagreb: University of Zagreb, Faculty of Transport and Traffic Sciences, 2017. urn:nbn:hr:119:036421
Cicnjak, Matija
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

Cicnjak, M. (2017). Izračun performansi zrakoplova Dash 8 Q400 u penjanju (Undergraduate thesis). Zagreb: University of Zagreb, Faculty of Transport and Traffic Sciences. Retrieved from https://urn.nsk.hr/urn:nbn:hr:119:036421

Cicnjak, Matija. "Izračun performansi zrakoplova Dash 8 Q400 u penjanju." Undergraduate thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, 2017. https://urn.nsk.hr/urn:nbn:hr:119:036421

Cicnjak, Matija. "Izračun performansi zrakoplova Dash 8 Q400 u penjanju." Undergraduate thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, 2017. https://urn.nsk.hr/urn:nbn:hr:119:036421

Cicnjak, M. (2017). 'Izračun performansi zrakoplova Dash 8 Q400 u penjanju', Undergraduate thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, accessed 06 November 2024, https://urn.nsk.hr/urn:nbn:hr:119:036421

Cicnjak M. Izračun performansi zrakoplova Dash 8 Q400 u penjanju [Undergraduate thesis]. Zagreb: University of Zagreb, Faculty of Transport and Traffic Sciences; 2017 [cited 2024 November 06] Available at: https://urn.nsk.hr/urn:nbn:hr:119:036421

M. Cicnjak, "Izračun performansi zrakoplova Dash 8 Q400 u penjanju", Undergraduate thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, Zagreb, 2017. Available at: https://urn.nsk.hr/urn:nbn:hr:119:036421

Metadata
TitleIzračun performansi zrakoplova Dash 8 Q400 u penjanju
Title (english)Performance of Dash 8 Q400 Aircraft During Climb
AuthorMatija Cicnjak
MentorKarolina Krajček Nikolić (mentor)
Committee memberAnita Domitrović (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 country2017-05-02, Croatia
Scientific / art field,
discipline and subdiscipline		TECHNICAL SCIENCES
Traffic and Transport Technology
Air Traffic
Abstract
Penjanje je segment leta zrakoplova koji traje od uzlijetanja zrakoplova sve do dostizanja željene visine leta. Najbitnije veličine koje se promatraju tijekom penjanja zrakoplova su brzina uzdizanja, kut penjanja, vrijeme penjanja i potrošnja goriva. Na penjanje velik utjecaj imaju masa zrakoplova, raspoloživa snaga motora te meteorološki uvjeti. Ovisno o odnosima navedenih veličina, mogu se odrediti različiti režimi penjanja. Unutar ovog rada analizirane su razlike između teorijske i stvarne brzine uzdizanja, kuta penjanja, vremena penjanja i potrošnje goriva zrakoplova Dash 8 Q400.
Abstract (english)
Climbing is a segment of flight from the flight departure until reaching the desired altitude. The most important variables that are observed during the climb are: rate of climb, angle of climb, climb time and fuel consumption of the aircraft. Climb performance is strongly affected by the mass of the aircraft, the available engine power and meteorological conditions. Different regimes of climb can be determined by combining the values of previously mentioned factors. Within this study the differences between theoretical and actual speed of ascent, the angle of climb, climbing time and fuel consumption have been analyzed for the aircraft Dash 8 Q400.
Keywords
Keywords (english)
Languagecroatian
URN:NBNurn:nbn:hr:119:036421
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 on2017-05-05 13:32:27