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undergraduate thesis
Utjecaj mase jednomotornog klipnog zrakoplova na performanse u režimu penjanja
Zagreb: University of Zagreb, Faculty of Transport and Traffic Sciences, 2020. urn:nbn:hr:119:841355
Vitek, Ivan
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

Vitek, I. (2020). Utjecaj mase jednomotornog klipnog zrakoplova na performanse u režimu penjanja (Undergraduate thesis). Zagreb: University of Zagreb, Faculty of Transport and Traffic Sciences. Retrieved from https://urn.nsk.hr/urn:nbn:hr:119:841355

Vitek, Ivan. "Utjecaj mase jednomotornog klipnog zrakoplova na performanse u režimu penjanja." Undergraduate thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, 2020. https://urn.nsk.hr/urn:nbn:hr:119:841355

Vitek, Ivan. "Utjecaj mase jednomotornog klipnog zrakoplova na performanse u režimu penjanja." Undergraduate thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, 2020. https://urn.nsk.hr/urn:nbn:hr:119:841355

Vitek, I. (2020). 'Utjecaj mase jednomotornog klipnog zrakoplova na performanse u režimu penjanja', Undergraduate thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, accessed 27 June 2024, https://urn.nsk.hr/urn:nbn:hr:119:841355

Vitek I. Utjecaj mase jednomotornog klipnog zrakoplova na performanse u režimu penjanja [Undergraduate thesis]. Zagreb: University of Zagreb, Faculty of Transport and Traffic Sciences; 2020 [cited 2024 June 27] Available at: https://urn.nsk.hr/urn:nbn:hr:119:841355

I. Vitek, "Utjecaj mase jednomotornog klipnog zrakoplova na performanse u režimu penjanja", Undergraduate thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, Zagreb, 2020. Available at: https://urn.nsk.hr/urn:nbn:hr:119:841355

Metadata
TitleUtjecaj mase jednomotornog klipnog zrakoplova na performanse u režimu penjanja
Title (english)Influence of a Single-engine Piston Aircraft Mass on Climb Performance
AuthorIvan Vitek
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 country2020-09-15, Croatia
Scientific / art field,
discipline and subdiscipline		TECHNICAL SCIENCES
Traffic and Transport Technology
Air Traffic
Abstract
Performanse predstavljaju specifičnu skupinu sposobnosti koju određeni zrakoplov posjeduje u rasponu različitih masa i brzina na određenim visinama i u određenim fazama leta (horizontalni let, penjanje, spuštanje, polijetanje, slijetanje i zaokreti). Ovaj rad analizira performanse u režimu penjanja. Eksperiment je izveden u tri leta sa penjanjem do visine 8000 stopa gdje su mjereni podaci o brzini uzdizanja, temperaturi, vremenu penjanja, potrošenom gorivu i prijeđenoj udaljenosti. Rezultati mjerenja prikazani su tablično. Kroz analizu rezultata, objašnjeni su i bitni vanjski čimbenici koji se moraju uzeti u obzir pri cjelokupnom izračunu performansi.
Abstract (english)
Performance represents a specific group of capabilities that a particular aircraft possesses in a range of different masses and speeds at certain altitudes and at certain stages of flight (horizontal flight, climb, descent, take-off, landing and turns). This paper analyzes the performance in climbing regime. The experiment was performed in three flights with climbing to an altitude of 8000 feet where data on climb speed, climbing time, temperature, fuel consumption and distance traveled were measured. The measurement results are shown in the tables. Through the analysis of the results, the important external factors that must be taken into account in the overall performance calculation are also explained.
Keywords
Keywords (english)
Languagecroatian
URN:NBNurn:nbn:hr:119:841355
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 on2020-10-23 11:09:51