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undergraduate thesis
Analiza statičke stabilnosti i ravnotežnog leta ultra-lakog zrakoplova
Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2017. urn:nbn:hr:235:420858
Ruklić, Kristijan
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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Ruklić, K. (2017). Analiza statičke stabilnosti i ravnotežnog leta ultra-lakog zrakoplova (Undergraduate thesis). Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture. Retrieved from https://urn.nsk.hr/urn:nbn:hr:235:420858

Ruklić, Kristijan. "Analiza statičke stabilnosti i ravnotežnog leta ultra-lakog zrakoplova." Undergraduate thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2017. https://urn.nsk.hr/urn:nbn:hr:235:420858

Ruklić, Kristijan. "Analiza statičke stabilnosti i ravnotežnog leta ultra-lakog zrakoplova." Undergraduate thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2017. https://urn.nsk.hr/urn:nbn:hr:235:420858

Ruklić, K. (2017). 'Analiza statičke stabilnosti i ravnotežnog leta ultra-lakog zrakoplova', Undergraduate thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, accessed 25 November 2024, https://urn.nsk.hr/urn:nbn:hr:235:420858

Ruklić K. Analiza statičke stabilnosti i ravnotežnog leta ultra-lakog zrakoplova [Undergraduate thesis]. Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture; 2017 [cited 2024 November 25] Available at: https://urn.nsk.hr/urn:nbn:hr:235:420858

K. Ruklić, "Analiza statičke stabilnosti i ravnotežnog leta ultra-lakog zrakoplova", Undergraduate thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, Zagreb, 2017. Available at: https://urn.nsk.hr/urn:nbn:hr:235:420858

Metadata
TitleAnaliza statičke stabilnosti i ravnotežnog leta ultra-lakog zrakoplova
Title (english)Static stability and trim analysis for ultra-light aircraft
AuthorKristijan Ruklić
MentorMilan Vrdoljak (mentor)
GranterUniversity of Zagreb
Faculty of Mechanical Engineering and Naval Architecture
Zagreb
Defense date and country2017-03-02, Croatia
Scientific / art field,
discipline and subdiscipline		TECHNICAL SCIENCES
Aviation, Rocket and Space Technology
Abstract
Cilj ovog završnog rada je analizirati uzdužnu statičku stabilnost i ravnotežni let ultra-lakog zrakoplova za različite uvjete leta. Analizom se ostvaruje uvid u dio mogućnosti uporabe zrakoplova. Ultra-laki zrakoplov, koji se razmatra, predstavlja repliku zrakoplova Zlin XII. Nakon definirane geometrije, određeni su ukupni stacionarni koeficijenti normalne sile i momenta propinjanja čime je određen aerodinamički model. Određivanjem koeficijenata, omogućena je provjera statičke stabilnosti i analiza ravnotežnog leta. Osim toga, napravljena je procjena maksimalnog koeficijenta sile uzgona i maksimalnog napadnog kuta krila.
Abstract (english)
The aim of this thesis is to analyze the longitudinal static stability and trimmed flight of ultra-light aircraft for different flight conditions. The analysis gives us better insight into some possibilities of the aircraft. Ultra-light aircraft, which is being considered, is a replica of the aircraft Zlin XII. After the geometry of the aircraft is defined, a total steady normal force and pitching moment coefficients are determined. This defined aerodynamic model for this work. Determined coefficients allows verification of static stability and trim analysis. In addition, the maximum lift coefficient and maximum angle of attack of wing is also determined.
Keywords
Keywords (english)
Languagecroatian
URN:NBNurn:nbn:hr:235:420858
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 09:35:41