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undergraduate thesis
Proračun performansi zrakoplova Diamond DV20 Katana
Zagreb: University of Zagreb, Faculty of Transport and Traffic Sciences, 2019. urn:nbn:hr:119:813080
Katić, Miljenka
University of Zagreb
Faculty of Transport and Traffic Sciences
Division of Aeronautics
Department of Aeronautics

Cite this document

Katić, M. (2019). Proračun performansi zrakoplova Diamond DV20 Katana (Undergraduate thesis). Zagreb: University of Zagreb, Faculty of Transport and Traffic Sciences. Retrieved from https://urn.nsk.hr/urn:nbn:hr:119:813080

Katić, Miljenka. "Proračun performansi zrakoplova Diamond DV20 Katana." Undergraduate thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, 2019. https://urn.nsk.hr/urn:nbn:hr:119:813080

Katić, Miljenka. "Proračun performansi zrakoplova Diamond DV20 Katana." Undergraduate thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, 2019. https://urn.nsk.hr/urn:nbn:hr:119:813080

Katić, M. (2019). 'Proračun performansi zrakoplova Diamond DV20 Katana', Undergraduate thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, accessed 28 December 2024, https://urn.nsk.hr/urn:nbn:hr:119:813080

Katić M. Proračun performansi zrakoplova Diamond DV20 Katana [Undergraduate thesis]. Zagreb: University of Zagreb, Faculty of Transport and Traffic Sciences; 2019 [cited 2024 December 28] Available at: https://urn.nsk.hr/urn:nbn:hr:119:813080

M. Katić, "Proračun performansi zrakoplova Diamond DV20 Katana", Undergraduate thesis, University of Zagreb, Faculty of Transport and Traffic Sciences, Zagreb, 2019. Available at: https://urn.nsk.hr/urn:nbn:hr:119:813080

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Metadata
TitleProračun performansi zrakoplova Diamond DV20 Katana
Title (english)Calculation of Performance Data for Diamond DV20 Katana Aircraft
AuthorMiljenka Katić
MentorKarolina Krajček Nikolić (mentor)
Committee memberDavor Franjković (predsjednik povjerenstva)
Committee memberAnita Domitrović (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 country2019-09-17, Croatia
Scientific / art field,
discipline and subdiscipline		TECHNICAL SCIENCES
Traffic and Transport Technology
Air Traffic
Abstract
Pod pojmom performanse nekog zrakoplova podrazumijeva se sposobnost zrakoplova da pri određenim uvjetima leta (visina, brzina, masa) posjeduje što povoljnije karakteristike u vidu doleta, istrajnosti, što manje potrošnje goriva, optimalne duljine potrebne za polijetanje i slijetanje, itd. Pri samom početku ovog rada predstavljene su deklarirane performanse zrakoplova Diamond Katana DV20 koje se nalaze u njegovom operativnom priručniku. U nastavku rada opisan je model propulzije zrakoplova koji se koristi u sljedećim poglavljima skupa sa aerodinamičkim modelom iz rada Petra Papočija za izračun performansi zrakoplova u fazi krstarenja i penjanja. Na temelju teorijskih izračuna dobivene su vrijednosti za maksimalnu istrajnost leta od 4,9 h, maksimalnu brzinu krstarenja od 236 km/h, maksimalnu brzinu uzdizanja od 4,8 m/s, te brzina za maksimalnu brzinu uzdizanja od 100 km/h. Na kraju ovog rada uspoređeni su podatci dobiveni u ovom radu s objavljenim podatcima o performansama. Temeljem usporedbe teorijski dobivenih podataka i deklariranih podataka može se zaključiti da da su odstupanja minimalna i prihvatljiva.
Abstract (english)
The term performance of an aircraft means the ability of an aircraft to to have the mosta efficient characteristics under certain conditions (altitude, speed, mass) in form of flight endurance, range, fuel consumption, length required for take off and landing, etc. At the beginning of this paper are presented performance of the aircraft Diamond Katana DV20 which are found in it′s manual. The following section of the paper describe the model of propulsion, used in aircraft, along with aerodynamic model form the work of Petar Papoči, to calculate performance of this aircraft in the cruise and climb phase. At the end of this paper, the data obtained in this paper will be compared with the published performance data. In accordance with theoretical calculation the given figure for maximum flight endurance is 4,9 h, maximum cruising Zagreb, 2019. speed is 236km/h, maximum lifting speed is 4,8 m/s, and the speed for maximum velocity is 100km/h. At the end of this paper the data acquired during theoretical research was compared to the published performance data of the aircraft. Based on the comparison between the theoretically obtained data and the declared performance data it can be concluded that deviations in data are minimal and acceptable.
Keywords
Keywords (english)
Languagecroatian
URN:NBNurn:nbn:hr:119:813080
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
RepositoryFaculty of Transport and Traffic Sciences
Created on2019-09-23 10:20:07

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