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undergraduate thesis
Aerodinamičke značajke konfiguracije tandem krila
2022. urn:nbn:hr:235:315642
Matić, Filip
University of Zagreb
Faculty of Mechanical Engineering and Naval Architecture

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Matić, F. (2022). Aerodinamičke značajke konfiguracije tandem krila (Undergraduate thesis). Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture. Retrieved from https://urn.nsk.hr/urn:nbn:hr:235:315642

Matić, Filip. "Aerodinamičke značajke konfiguracije tandem krila." Undergraduate thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2022. https://urn.nsk.hr/urn:nbn:hr:235:315642

Matić, Filip. "Aerodinamičke značajke konfiguracije tandem krila." Undergraduate thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2022. https://urn.nsk.hr/urn:nbn:hr:235:315642

Matić, F. (2022). 'Aerodinamičke značajke konfiguracije tandem krila', Undergraduate thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, accessed 03 May 2024, https://urn.nsk.hr/urn:nbn:hr:235:315642

Matić F. Aerodinamičke značajke konfiguracije tandem krila [Undergraduate thesis]. Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture; 2022 [cited 2024 May 03] Available at: https://urn.nsk.hr/urn:nbn:hr:235:315642

F. Matić, "Aerodinamičke značajke konfiguracije tandem krila", Undergraduate thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, Zagreb, 2022. Available at: https://urn.nsk.hr/urn:nbn:hr:235:315642

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Metadata
TitleAerodinamičke značajke konfiguracije tandem krila
Title (english)Aerodynamic characteristics of tandem wing configuration
AuthorFilip Matić
MentorMilan Vrdoljak (mentor)
GranterUniversity of Zagreb
Faculty of Mechanical Engineering and Naval Architecture
Zagreb
Defense date and country2022-03-03, Croatia
Scientific / art field,
discipline and subdiscipline		TECHNICAL SCIENCES
Aviation, Rocket and Space Technology
Aircraft Construction and Design
Abstract
Konfiguracije zrakoplova kroz povijest se nisu puno mijenjale primarno zbog rigoroznih sigurnosnih zahtijevam koji za sobom povlače dugotrajan razvoj koji je potrebna za certifikaciju novih konfiguracija i naravno sve to košta te je i također pitanje isplativosti. Tandem konfiguracija ako je pravilno izvedena potencijalno može značajno povećati koristan teret zrakoplova, bez da se povećava raspon krila. U ovom radu koristeći Weissingerovu metodu noseće linije sa slobodnim tragom napravljena je procjena aerodinamičkih veličina za tandem konfiguraciju, ova metoda je odabrana da se može bolje proučiti interakcija stražnjeg i prednjeg krila.
Abstract (english)
Aircraft configurations haven't changed very much primarily because of rigorous safety requirements which require long development times in order to certify such new configurations of course this costs money, and that raises the question of profitability. Tandem configuration, if done right, could potentially increase useful cargo, without increasing wingspan. In scope of this work an assessment of aerodynamic coefficients has been made using Weissinger's lifting line method with free wake, this method was selected to better understand the interaction between front and rear wing
Keywords
Keywords (english)
Languagecroatian
URN:NBNurn:nbn:hr:235:315642
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 on2022-02-28 13:04:08