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undergraduate thesis
Izračun performansi zrakoplova Airbus A320 u slučaju otkaza jednog motora
Zagreb: University of Zagreb, Faculty of Transport and Traffic Sciences, 2018. urn:nbn:hr:119:898043
Šimon, Danijel
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

Šimon, D. (2018). Izračun performansi zrakoplova Airbus A320 u slučaju otkaza jednog motora (Undergraduate thesis). Zagreb: University of Zagreb, Faculty of Transport and Traffic Sciences. Retrieved from https://urn.nsk.hr/urn:nbn:hr:119:898043

Šimon, Danijel. "Izračun performansi zrakoplova Airbus A320 u slučaju otkaza jednog motora." Undergraduate thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, 2018. https://urn.nsk.hr/urn:nbn:hr:119:898043

Šimon, Danijel. "Izračun performansi zrakoplova Airbus A320 u slučaju otkaza jednog motora." Undergraduate thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, 2018. https://urn.nsk.hr/urn:nbn:hr:119:898043

Šimon, D. (2018). 'Izračun performansi zrakoplova Airbus A320 u slučaju otkaza jednog motora', Undergraduate thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, accessed 05 July 2024, https://urn.nsk.hr/urn:nbn:hr:119:898043

Šimon D. Izračun performansi zrakoplova Airbus A320 u slučaju otkaza jednog motora [Undergraduate thesis]. Zagreb: University of Zagreb, Faculty of Transport and Traffic Sciences; 2018 [cited 2024 July 05] Available at: https://urn.nsk.hr/urn:nbn:hr:119:898043

D. Šimon, "Izračun performansi zrakoplova Airbus A320 u slučaju otkaza jednog motora", Undergraduate thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, Zagreb, 2018. Available at: https://urn.nsk.hr/urn:nbn:hr:119:898043

Metadata
TitleIzračun performansi zrakoplova Airbus A320 u slučaju otkaza jednog motora
Title (english)Performance Calculations of Airbus A320 Aircraft with One Engine Inoperative
AuthorDanijel Šimon
MentorDavor Franjković (mentor)
Committee memberAnita Domitrović (predsjednik povjerenstva)
Committee memberTomislav Radišić (član povjerenstva)
Committee memberŽeljko Marušić (član povjerenstva)
GranterUniversity of Zagreb
Faculty of Transport and Traffic Sciences
(Division of Aeronautics)
(Department of Aeronautics)
Zagreb
Defense date and country2018-03-06, Croatia
Scientific / art field,
discipline and subdiscipline		TECHNICAL SCIENCES
Traffic and Transport Technology
Air Traffic
Abstract
Ovaj rad bavi se problematikom određivanja performansi zrakoplova Airbus A320 u slučaju otkaza jednog od dvaju njegovih motora. Objašnjena je važnost određivanja performansi nekog zrakoplova u takvom slučaju, zakonski zahtjevi performansi s jednim neispravnim motorom, oblici i uzroci otkaza mlaznih motora te općenite karakteristike Airbusa A320. Prikazan je i objašnjen izračun performansi navedenog zrakoplova s jednim neispravnim motorom u fazama polijetanja, penjanja, krstarenja te spuštanja, uz konkretne primjere izračunavanja parametara kao npr. maksimalne dopuštene mase tijekom polijetanja, potrebne vrijednosti potiska motora, potrebne duljine zaleta u polijetanju, vremena penjanja i spuštanja, potrošnje goriva, brzine leta, optimalne i maksimalne visine leta te specifičnog doleta. Performanse u letu s jednim neispravnim motorom uspoređene su s performansama u letu s oba motora ispravna. Opisane su potrebne procedure i postupci posade zrakoplova u slučaju otkaza motora u različitim fazama leta.
Abstract (english)
This paper describes the determination of the performance of the Airbus A320 aircraft in case of failure of one of its two engines. The importance of determination of performance in such cases is described, along with the legal performance requirements, modes and causes of jet engine failures and general characteristics of the Airbus A320 aircraft. The calculation of performance of the mentioned aircraft with one engine inoperative is explained for the take-off, climb, cruise and descent phases of flight, with examples of the calculation of parameters such as maximum take-off mass, required engine thrust, take-off distance required, time for climb and descent, fuel flow, airspeed, optimum and maximum altitude, and specific range. The performance with one engine inoperative is compared with the performance with all engines operative. The required procedures and acts of the crew after engine failure are described for different phases of flight.
Keywords
Keywords (english)
Languagecroatian
URN:NBNurn:nbn:hr:119:898043
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 on2018-03-26 13:55:06