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undergraduate thesis
Konstrukcija i analiza aerodinamičkog spojlera na automobilu
2019. urn:nbn:hr:190:281195
Berković, Nikša
University of Rijeka
Faculty of Engineering
Department of Fluid Mechanics and Computational Engineering
Section of Fluid Mechanics and Hydraulic Machines

Cite this document

Berković, N. (2019). Konstrukcija i analiza aerodinamičkog spojlera na automobilu (Undergraduate thesis). Rijeka: University of Rijeka, Faculty of Engineering. Retrieved from https://urn.nsk.hr/urn:nbn:hr:190:281195

Berković, Nikša. "Konstrukcija i analiza aerodinamičkog spojlera na automobilu." Undergraduate thesis, University of Rijeka, Faculty of Engineering, 2019. https://urn.nsk.hr/urn:nbn:hr:190:281195

Berković, Nikša. "Konstrukcija i analiza aerodinamičkog spojlera na automobilu." Undergraduate thesis, University of Rijeka, Faculty of Engineering, 2019. https://urn.nsk.hr/urn:nbn:hr:190:281195

Berković, N. (2019). 'Konstrukcija i analiza aerodinamičkog spojlera na automobilu', Undergraduate thesis, University of Rijeka, Faculty of Engineering, accessed 09 January 2025, https://urn.nsk.hr/urn:nbn:hr:190:281195

Berković N. Konstrukcija i analiza aerodinamičkog spojlera na automobilu [Undergraduate thesis]. Rijeka: University of Rijeka, Faculty of Engineering; 2019 [cited 2025 January 09] Available at: https://urn.nsk.hr/urn:nbn:hr:190:281195

N. Berković, "Konstrukcija i analiza aerodinamičkog spojlera na automobilu", Undergraduate thesis, University of Rijeka, Faculty of Engineering, Rijeka, 2019. Available at: https://urn.nsk.hr/urn:nbn:hr:190:281195

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Metadata
TitleKonstrukcija i analiza aerodinamičkog spojlera na automobilu
Title (english)Car wing spoiler design and analysis
AuthorNikša Berković
MentorLado Kranjčević (mentor)
Committee memberKristian Lenić (predsjednik povjerenstva)
GranterUniversity of Rijeka
Faculty of Engineering
(Department of Fluid Mechanics and Computational Engineering)
(Section of Fluid Mechanics and Hydraulic Machines)
Rijeka
Defense date and country2019-09-16, Croatia
Scientific / art field,
discipline and subdiscipline		TECHNICAL SCIENCES
Mechanical Engineering
Abstract
U ovom radu objasnio se postupak odreĎivanja optimalnog kuta nastrujavanja odabranog NACA 6412 profila koji sluţi kao krilo na natjecateljskim bolidima Formule 1 pomoću simulacija u programskom okruţenju Altair Virtual Wind Tunnel-a. Isto tako naveden je način kako poboljšati dobivene vrijednosti sila otpora i aerodinamičkog potiska dodavanjem bokova na krilo. UsporeĎene su i sile i koeficijenti otpora i potiska za dva modela: samostalnog krila i krila s dodanim bokovima. Na kraju se došlo do zaključka koji kut nastrujavanja profila je najbolji za najmanji omjer sile otpora i aerodinamičkog potiska.
Abstract (english)
This paper explained how to get optimal flow angle for NACA 6412 aerofoil used on Formula 1 cars using Altair Virtual Wind Tunnel software. After the simulations upgrades to the wing were constructed. They consisted of wing endplates and then overall drag and lift force was calculated, so as their ratio opposed to wing without endplates. At the end the optimal angle that has the lowest drag/lift ratio was chosen.
Keywords
Keywords (english)
Languagecroatian
URN:NBNurn:nbn:hr:190:281195
Study programmeTitle: Mechanical Engineering
Study programme type: university
Study level: undergraduate
Academic / professional title: sveučilišni/a prvostupnik/ prvostupnica (baccalaureus/baccalaurea) inženjer/inženjerka strojarstva (sveučilišni/a prvostupnik/ prvostupnica (baccalaureus/baccalaurea) inženjer/inženjerka strojarstva)
Type of resourceText
File originBorn digital
Access conditionsAccess restricted to students and staff of home institution
Terms of useLicence In copyright icon
Created on2020-05-09 20:02:16