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undergraduate thesis
Operativne performanse putničkog turbo-elisnog zrakoplova
Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2014. urn:nbn:hr:235:048597
Mičuga, Hrvoje
University of Zagreb
Faculty of Mechanical Engineering and Naval Architecture

Institutional repository: Repository of Faculty of Mechanical Engineering and Naval Architecture University of Zagreb

Cite this document

Mičuga, H. (2014). Operativne performanse putničkog turbo-elisnog zrakoplova (Undergraduate thesis). Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture. Retrieved from https://urn.nsk.hr/urn:nbn:hr:235:048597

Mičuga, Hrvoje. "Operativne performanse putničkog turbo-elisnog zrakoplova." Undergraduate thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2014. https://urn.nsk.hr/urn:nbn:hr:235:048597

Mičuga, Hrvoje. "Operativne performanse putničkog turbo-elisnog zrakoplova." Undergraduate thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2014. https://urn.nsk.hr/urn:nbn:hr:235:048597

Mičuga, H. (2014). 'Operativne performanse putničkog turbo-elisnog zrakoplova', Undergraduate thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, accessed 25 November 2024, https://urn.nsk.hr/urn:nbn:hr:235:048597

Mičuga H. Operativne performanse putničkog turbo-elisnog zrakoplova [Undergraduate thesis]. Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture; 2014 [cited 2024 November 25] Available at: https://urn.nsk.hr/urn:nbn:hr:235:048597

H. Mičuga, "Operativne performanse putničkog turbo-elisnog zrakoplova", Undergraduate thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, Zagreb, 2014. Available at: https://urn.nsk.hr/urn:nbn:hr:235:048597

Metadata
TitleOperativne performanse putničkog turbo-elisnog zrakoplova
Title (english)Operational performance of transport turboprop airplane
AuthorHrvoje Mičuga
MentorMilan Vrdoljak (mentor)
GranterUniversity of Zagreb
Faculty of Mechanical Engineering and Naval Architecture
Zagreb
Defense date and country2014-09-23, Croatia
Scientific / art field,
discipline and subdiscipline		TECHNICAL SCIENCES
Aviation, Rocket and Space Technology
Abstract
Svrha ovog rada je izracun performansi zrakoplova nalik na Dash-8 Q400 i usporedba is- tih sa podacima koje na temelju testiranja i vlastitih modela zrakoplova izdaje proizvodac zrakoplova u svom prirucniku o eksploataciji zrakoplova. Podaci o motoru, aerodina- mici i geometriji su poznati. Prikazani su rezultati analize za penjanje u rezimu najvece brzine penjanja i usporedeni su sa dostupnim podacima iz spomenutog prirucnika. U obzir je uzet i utjecaj temperature.Pokazano je da postojeci model aerodinamike i po- gona dovoljno precizno opisuje penjanje u rezimu BRC. Izvsen je izracun specicnog doleta za razlicite mase i brzine leta zrakoplova.Prikazani su rezultati za dva slucaja, maksimalni dolet i ekonomski dolet koji se ostvaruje na 99% vrijednosti maksimalnog doleta uz povecanje brzine leta. Spustanje je podijeljeno u dva dijela, spustanje do vi- sine od 914.4 m i prilaz za slijetanje.Modelirano je za rezim najvece brzine spustanja za koji su podaci dostupni u prirucniku o eksploataciji zrakoplova. Proracunata je brzina rotacije u slijetanju i usporedena sa dostupnim podacima.
Abstract (english)
Purpose of this thesis is performance calculation for the aircraft simmilar to Dash-8 Q400 and comparison of calculated data to data given by the manufacturer in Aircraft Operating Manual which is based on ight test data and manufacturers performance models. Aerodynamics,propulsion and geometry data are known. Analysis of data for best rate of climb regime has been made. Given data has been compared to the available data from AOM with regard to temperature variations.Speci c air range calculations were made for di erent mass and speeds. Descent has been divided into two parts, descent from cruise FL to 3000 ft and approach.Descent has been modelled for high speed descent by the data provided by the AOM. Last two chapters are dedicated to take-o and landing. Rotation speed was calculated and compared to the manufacturer data.
Keywords
Keywords (english)
Languagecroatian
URN:NBNurn:nbn:hr:235:048597
Study programmeTitle: Aeronautical Studies
Study programme type: university
Study level: undergraduate
Academic / professional title: sveučilišni/a prvostupnik/ prvostupnica (baccalaureus/baccalaurea) inženjer/inženjerka zrakoplovnog inženjerstva (sveučilišni/a prvostupnik/ prvostupnica (baccalaureus/baccalaurea) inženjer/inženjerka zrakoplovnog inženjerstva)
Type of resourceText
File originBorn digital
Access conditionsAccess restricted to students and staff of home institution
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Created on2019-05-22 11:47:59