prikaz prve stranice dokumenta Izračun performansi odabranih transportnih zrakoplova koristeći model BADA
  Download
PDF 772.08 KB
undergraduate thesis
Izračun performansi odabranih transportnih zrakoplova koristeći model BADA
Zagreb: University of Zagreb, Faculty of Transport and Traffic Sciences, 2021. urn:nbn:hr:119:185762
Šimig, Duje
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

Šimig, D. (2021). Izračun performansi odabranih transportnih zrakoplova koristeći model BADA (Undergraduate thesis). Zagreb: University of Zagreb, Faculty of Transport and Traffic Sciences. Retrieved from https://urn.nsk.hr/urn:nbn:hr:119:185762

Šimig, Duje. "Izračun performansi odabranih transportnih zrakoplova koristeći model BADA." Undergraduate thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, 2021. https://urn.nsk.hr/urn:nbn:hr:119:185762

Šimig, Duje. "Izračun performansi odabranih transportnih zrakoplova koristeći model BADA." Undergraduate thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, 2021. https://urn.nsk.hr/urn:nbn:hr:119:185762

Šimig, D. (2021). 'Izračun performansi odabranih transportnih zrakoplova koristeći model BADA', Undergraduate thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, accessed 25 July 2024, https://urn.nsk.hr/urn:nbn:hr:119:185762

Šimig D. Izračun performansi odabranih transportnih zrakoplova koristeći model BADA [Undergraduate thesis]. Zagreb: University of Zagreb, Faculty of Transport and Traffic Sciences; 2021 [cited 2024 July 25] Available at: https://urn.nsk.hr/urn:nbn:hr:119:185762

D. Šimig, "Izračun performansi odabranih transportnih zrakoplova koristeći model BADA", Undergraduate thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, Zagreb, 2021. Available at: https://urn.nsk.hr/urn:nbn:hr:119:185762

Metadata
TitleIzračun performansi odabranih transportnih zrakoplova koristeći model BADA
Title (english)Transport aircraft performance calculation using BADA model
AuthorDuje Šimig
MentorKarolina Krajček Nikolić (mentor)
Committee memberDavor Franjković (predsjednik povjerenstva)
Committee memberDavid Gerhardinger (član povjerenstva)
Committee memberAnita Domitrović (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
Rad obrađuje temu performansi odabranog transportnog zrakoplova u standardnim atmosferskim uvjetima. Performanse zrakoplova promatraju se kroz tri režima: penjanje, krstarenje tj. horizontalni let i spuštanje. Cilj rada je proračun performansi zrakoplova A320 pomoću BADA modela te usporedba s performansama iz programa PEP (Performance Engineering Program) proizvođača u navedenim režimima leta. Analiza performansi napravljena je za dvomotorni mlazni transportni zrakoplov Airbus A320 koji se koristi na manjim i srednjim udaljenostima. Rezultati izračuna pomoću BADA modela daju rezultate s manjim odstupanjima od vrijednostima iz PEP-a. Navedene razlike pripisuju se različitim polarama otpora u PEP i BADA modelu.
Abstract (english)
The paper deals with the topic of the performance of a selected transport aircraft in standard atmospheric conditions. The performance of the aircraft will be observed through three modes: ascent, cruise, ie horizontal flight, and descent. The aim of this paper is to calculate the performance of the A320 aircraft using the BADA model and to compare it with the performance from the Performance Engineering Program (PEP) of the manufacturer in the stated flight modes. Performance analysis was made for the twin-engine jet transport aircraft Airbus A320 used at short and medium distances. The calculations from the BADA model show certain deviations from the results of PEP. These differences are mostly due to different drag polar use din PEP and BADA model.
Keywords
Keywords (english)
Languagecroatian
URN:NBNurn:nbn:hr:119:185762
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 14:03:57