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undergraduate thesis
Analiza ravnotežnog leta zrakoplova primjenom generičkog globalnog aerodinamičkog modela
Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2015. urn:nbn:hr:235:328493
Franjčić, Antonio
University of Zagreb
Faculty of Mechanical Engineering and Naval Architecture

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

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Franjčić, A. (2015). Analiza ravnotežnog leta zrakoplova primjenom generičkog globalnog aerodinamičkog modela (Undergraduate thesis). Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture. Retrieved from https://urn.nsk.hr/urn:nbn:hr:235:328493

Franjčić, Antonio. "Analiza ravnotežnog leta zrakoplova primjenom generičkog globalnog aerodinamičkog modela." Undergraduate thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2015. https://urn.nsk.hr/urn:nbn:hr:235:328493

Franjčić, Antonio. "Analiza ravnotežnog leta zrakoplova primjenom generičkog globalnog aerodinamičkog modela." Undergraduate thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2015. https://urn.nsk.hr/urn:nbn:hr:235:328493

Franjčić, A. (2015). 'Analiza ravnotežnog leta zrakoplova primjenom generičkog globalnog aerodinamičkog modela', Undergraduate thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, accessed 28 December 2024, https://urn.nsk.hr/urn:nbn:hr:235:328493

Franjčić A. Analiza ravnotežnog leta zrakoplova primjenom generičkog globalnog aerodinamičkog modela [Undergraduate thesis]. Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture; 2015 [cited 2024 December 28] Available at: https://urn.nsk.hr/urn:nbn:hr:235:328493

A. Franjčić, "Analiza ravnotežnog leta zrakoplova primjenom generičkog globalnog aerodinamičkog modela", Undergraduate thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, Zagreb, 2015. Available at: https://urn.nsk.hr/urn:nbn:hr:235:328493

Metadata
TitleAnaliza ravnotežnog leta zrakoplova primjenom generičkog globalnog aerodinamičkog modela
Title (english)Analysis of equilibrium aircraft flight using the Generic Global Aerodynamic Model
AuthorAntonio Franjčić
MentorMilan Vrdoljak (mentor)
GranterUniversity of Zagreb
Faculty of Mechanical Engineering and Naval Architecture
Zagreb
Defense date and country2015-09-22, Croatia
Scientific / art field,
discipline and subdiscipline		TECHNICAL SCIENCES
Aviation, Rocket and Space Technology
Abstract
Tema ovog završnog je analiza generičkog globalnog aerodinamičkog(GGA) modela, usporedba uzdužnog GGA modela s linearnim modelom, stohastično ponašanje modela, njegovo ponašanje u određivanju režima ravnotežnog leta te analiza zrakoplova kao materijalne točke uz pomoć GGA metode. U početku se nalazi kratki uvod u GGA model, njegove značajke te na kojim su zrakoplovima provedena mjerenja u svrhu određivanja GGA koeficijenata. Nakon toga prikazani su rezultati uzgona, otpora, momenta propinjanja te njihova odstupanja od linearnog modela za DHC-6. Drugo poglavlje prikazuje određivanje režima ravnotežnog leta za DHC-6 i F-16C, njihova stohastična odstupanja i razumno područje uporabe. Treće poglavlje prikazuje analizu zrakoplova kao materijalne točke za horizontalni let zrakoplova. Za numeričko i statističko izračunavanje koristi se programski paket MATLAB.
Abstract (english)
The goal of this paper is the analysis of the Generic Global Aerodinamic(GGA) model, comparison of the lognitudal GGA model with its linear counterpart, stohastic behaviour of the model, its behaviour in the state of equilibrium flight and analysis of the aircrafts in this paper as material points. In the beginning of the paper there is a brief explanation on the GGA model, where its characteristics are shown and the aircrafts which are included in the model are listed. After that the results of lift, drag and pitch moment are shown with their according deviations, and their deviations from the linear model are shown in a few examples. The second chapter focuses on equilibrium flight of the analyzed aircrafts , their stohastic deviations and the reasonable applications of the model. The third chapter shows the analysis of the studied aircrafts as a material dots. For statistical calculations the programming language MATLAB is used. The studied aircrafts are the DHC-6 "Twin Otter" and the F-16C "Fighting Falcon".
Keywords
Languagecroatian
URN:NBNurn:nbn:hr:235:328493
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 on2019-05-28 09:29:01