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undergraduate thesis
Performanse borbene bespilotne letjelice
2022. urn:nbn:hr:235:761479
Samardžić, Tin
University of Zagreb
Faculty of Mechanical Engineering and Naval Architecture

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Samardžić, T. (2022). Performanse borbene bespilotne letjelice (Undergraduate thesis). Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture. Retrieved from https://urn.nsk.hr/urn:nbn:hr:235:761479

Samardžić, Tin. "Performanse borbene bespilotne letjelice." Undergraduate thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2022. https://urn.nsk.hr/urn:nbn:hr:235:761479

Samardžić, Tin. "Performanse borbene bespilotne letjelice." Undergraduate thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2022. https://urn.nsk.hr/urn:nbn:hr:235:761479

Samardžić, T. (2022). 'Performanse borbene bespilotne letjelice', Undergraduate thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, accessed 27 December 2024, https://urn.nsk.hr/urn:nbn:hr:235:761479

Samardžić T. Performanse borbene bespilotne letjelice [Undergraduate thesis]. Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture; 2022 [cited 2024 December 27] Available at: https://urn.nsk.hr/urn:nbn:hr:235:761479

T. Samardžić, "Performanse borbene bespilotne letjelice", Undergraduate thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, Zagreb, 2022. Available at: https://urn.nsk.hr/urn:nbn:hr:235:761479

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Metadata
TitlePerformanse borbene bespilotne letjelice
Title (english)Performance of unmanned combat aerial vehicle
AuthorTin Samardžić
MentorMilan Vrdoljak (mentor)
GranterUniversity of Zagreb
Faculty of Mechanical Engineering and Naval Architecture
Zagreb
Defense date and country2022-03-04, Croatia
Scientific / art field,
discipline and subdiscipline		TECHNICAL SCIENCES
Aviation, Rocket and Space Technology
Abstract
Tema ovog završnog zadatka je analiza performansi borbene bespilotne letjelice nalik na MQ-9 Reaper. U svrhu te analize promatraju se dostupni podaci za samu aerodinamiku letjelice kao i karakteristike motora Honeywell TPE331-10. U početnom dijelu zadatka prikazane su karakteristike spomenutog motora i pretpostavljene karakteristike propelera. Primjenom metode ukupne energije analizirana je ovojnica leta. U nastavku ovog završnog zadatka analizirane su performanse u penjanju i horizontalnom letu pri čemu su izračunate brzina leta u režimu BRC, dolet i maksimalna duljina trajanja leta.
Abstract (english)
The topic of this bachelor thesis is the performance analysis of a combat unmanned aerial vehicle resembling MQ-9 Reaper. For this analysis available data for aircraft aerodynamics as well as Honeywell TPE331-10 characteristics is used. In the starting section of this thesis motor characteristics are shown and propeller characteristics are assumed. The flight envelope was analysed by applying the total energy method. In the latter part of this thesis the climbing and horizontal flight perfomance analysis was conducted during which the climbing speed, range and endurance have been calculated.
Keywords
Keywords (english)
Languagecroatian
URN:NBNurn:nbn:hr:235:761479
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 conditionsOpen access
Terms of useLicence In copyright icon
Created on2022-03-03 14:25:55