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undergraduate thesis
Analiza statičke stabilnosti i ravnotežnog leta električno-propelerskog poslovnog zrakoplova
Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2021. urn:nbn:hr:235:984783
Perica, Ante
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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Perica, A. (2021). Analiza statičke stabilnosti i ravnotežnog leta električno-propelerskog poslovnog zrakoplova (Undergraduate thesis). Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture. Retrieved from https://urn.nsk.hr/urn:nbn:hr:235:984783

Perica, Ante. "Analiza statičke stabilnosti i ravnotežnog leta električno-propelerskog poslovnog zrakoplova." Undergraduate thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2021. https://urn.nsk.hr/urn:nbn:hr:235:984783

Perica, Ante. "Analiza statičke stabilnosti i ravnotežnog leta električno-propelerskog poslovnog zrakoplova." Undergraduate thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2021. https://urn.nsk.hr/urn:nbn:hr:235:984783

Perica, A. (2021). 'Analiza statičke stabilnosti i ravnotežnog leta električno-propelerskog poslovnog zrakoplova', Undergraduate thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, accessed 26 December 2024, https://urn.nsk.hr/urn:nbn:hr:235:984783

Perica A. Analiza statičke stabilnosti i ravnotežnog leta električno-propelerskog poslovnog zrakoplova [Undergraduate thesis]. Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture; 2021 [cited 2024 December 26] Available at: https://urn.nsk.hr/urn:nbn:hr:235:984783

A. Perica, "Analiza statičke stabilnosti i ravnotežnog leta električno-propelerskog poslovnog zrakoplova", Undergraduate thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, Zagreb, 2021. Available at: https://urn.nsk.hr/urn:nbn:hr:235:984783

Metadata
TitleAnaliza statičke stabilnosti i ravnotežnog leta električno-propelerskog poslovnog zrakoplova
Title (english)Static stability and trim analysis for electric propeller business aircraft
AuthorAnte Perica
MentorMilan Vrdoljak (mentor)
Committee memberIvica Smojver (predsjednik povjerenstva)
Committee memberJosip Stepanić (član povjerenstva)
Committee memberDarko Ivančević (član povjerenstva)
GranterUniversity of Zagreb
Faculty of Mechanical Engineering and Naval Architecture
Zagreb
Defense date and country2021-02-26, Croatia
Scientific / art field,
discipline and subdiscipline		TECHNICAL SCIENCES
Aviation, Rocket and Space Technology
Aircraft Control
Abstract
U ovom završnom radu analiziraju se performanse zrakoplova nalik na električni poslovni zrakoplov Alice, koji je djelo Izraelske kompanije Eviation. U samom početku istraženi su dostupni podatci o navedenom zrakoplovu, dok su ostale vrijednosti pretpostavljene na osnovu dostupnih slika na internetu i već stečenog znanja. Nakon definiranja geometrije kreće se u proračun koeficijenata normalne sile i koeficijenta momenta propinjanja. S definiranim aerodinamičkim koeficijentima provedena je analiza uzdužne statičke stabilnosti i ravnotežnog leta zrakoplova pri pretpostavljenim uvjetima leta i očekivanim mogućnostima letjelice. U konačnici u dijagramskim prikazima prikazani su rezultati analize za određene uvjete letenja.
Abstract (english)
This final paper analyzes the performance of an aircraft similar to the Alice electric business aircraft, which is the work of the Israeli company Eviation. At the very beginning, the available data on the mentioned aircraft were researched, while other values were assumed on the basis of available images on the Internet and already acquired knowledge. After defining the geometry, it begins to calculate the coefficients of normal force and the coefficient of moment of pitch. With the defined aerodynamic coefficients, the analysis of longitudinal static stability and balanced flight of the aircraft was performed under the assumed flight conditions and the expected capabilities of the aircraft. Finally, the results of the analysis for specific flight conditions are presented in the diagrams.
Keywords
Keywords (english)
Languagecroatian
URN:NBNurn:nbn:hr:235:984783
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 on2021-02-26 10:10:06