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undergraduate thesis
Procjena doleta borbenog zrakoplova
Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2020. urn:nbn:hr:235:546594
Vidović, Adriana
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

Vidović, A. (2020). Procjena doleta borbenog zrakoplova (Undergraduate thesis). Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture. Retrieved from https://urn.nsk.hr/urn:nbn:hr:235:546594

Vidović, Adriana. "Procjena doleta borbenog zrakoplova." Undergraduate thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2020. https://urn.nsk.hr/urn:nbn:hr:235:546594

Vidović, Adriana. "Procjena doleta borbenog zrakoplova." Undergraduate thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2020. https://urn.nsk.hr/urn:nbn:hr:235:546594

Vidović, A. (2020). 'Procjena doleta borbenog zrakoplova', Undergraduate thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, accessed 02 October 2024, https://urn.nsk.hr/urn:nbn:hr:235:546594

Vidović A. Procjena doleta borbenog zrakoplova [Undergraduate thesis]. Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture; 2020 [cited 2024 October 02] Available at: https://urn.nsk.hr/urn:nbn:hr:235:546594

A. Vidović, "Procjena doleta borbenog zrakoplova", Undergraduate thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, Zagreb, 2020. Available at: https://urn.nsk.hr/urn:nbn:hr:235:546594

Metadata
TitleProcjena doleta borbenog zrakoplova
Title (english)Estimation of the fighter aircraft range
AuthorAdriana Vidović
MentorMilan Vrdoljak (mentor)
Committee memberMilan Vrdoljak (predsjednik povjerenstva)
GranterUniversity of Zagreb
Faculty of Mechanical Engineering and Naval Architecture
Zagreb
Defense date and country2020-09-23, Croatia
Scientific / art field,
discipline and subdiscipline		TECHNICAL SCIENCES
Aviation, Rocket and Space Technology
Aircraft Construction and Design
Abstract
Tema ovog završnog rada jest analiza doleta i ostalih performansi borbenog zrakoplova korištenjem modela ravnotežnog leta, uz primjenu uvjeta za horizontalni let kao i usporedba istih s referentnim vrijednostima odabranog zrakoplova iščitanih iz tehničkog priručnika. Prije same numeričke analize, dolet, te sve karakteristike i metode vezane za računanje istog, detaljno su opisane. Procjeni doleta prethodi računanje ostalih značajki zrakoplova potrebnih za samu analizu. Te značajke dobivene su pokretanjem numeričkog modela za ravnotežni let u ovisnosti o različitim visinama, brzinama, konfiguracijama zrakoplova, te u ovisnosti o promjeni mase zrakoplova tijekom leta. Dobivene značajke ubacili smo u poseban program koji računa dolet za različite visine leta i različite konfiguracije zrakoplova. Osim iznosa doleta za svaku kombinaciju različite visine i konfiguracije, dobili smo iznose trajanja leta i mase rezervnog goriva za alternativna slijetanja. Usporedbom dobivenih rezultata, uočeno je prihvatljivo odstupanje od referentnih vrijednosti.
Abstract (english)
Topic of this bachelor thesis is the analysis of range and other performance of a combat aircraft using model for trimmed aircraft, applying the horizontal flight conditions as well as comparing them with reference values of the selected aircraft, taken from the technical manual. Before the numerical analysis, the range, and all the characteristics and methods related to its calculation, are described in detail. The range assessment is preceded by the calculation of the other aircraft characteristics required for the analysis itself. These features were obtained by running a numerical model for trimmed flight as a function of different altitudes, velocities, aircraft configurations, and as a function of change in mass of the aircraft during the flight. We included the obtained features in a special program that calculates the range for different flight altitudes and different aircraft configurations. In addition to the resultes of range for each combination of different altitudes and configurations, we obtained the results of endurance and reserve fuel masses for alternative landings. By comparing the obtained results, acceptable deviation was observed.
Keywords
Keywords (english)
Languagecroatian
URN:NBNurn:nbn:hr:235:546594
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
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Created on2020-09-22 06:57:58