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undergraduate thesis
Opstrujavanje aerodinamičnog profila
2022. urn:nbn:hr:190:092445
Čuček, Matej
University of Rijeka
Faculty of Engineering
Department of Fluid Mechanics and Computational Engineering
Section of Fluid Mechanics and Hydraulic Machines

Cite this document

Čuček, M. (2022). Opstrujavanje aerodinamičnog profila (Undergraduate thesis). Rijeka: University of Rijeka, Faculty of Engineering. Retrieved from https://urn.nsk.hr/urn:nbn:hr:190:092445

Čuček, Matej. "Opstrujavanje aerodinamičnog profila." Undergraduate thesis, University of Rijeka, Faculty of Engineering, 2022. https://urn.nsk.hr/urn:nbn:hr:190:092445

Čuček, Matej. "Opstrujavanje aerodinamičnog profila." Undergraduate thesis, University of Rijeka, Faculty of Engineering, 2022. https://urn.nsk.hr/urn:nbn:hr:190:092445

Čuček, M. (2022). 'Opstrujavanje aerodinamičnog profila', Undergraduate thesis, University of Rijeka, Faculty of Engineering, accessed 24 January 2025, https://urn.nsk.hr/urn:nbn:hr:190:092445

Čuček M. Opstrujavanje aerodinamičnog profila [Undergraduate thesis]. Rijeka: University of Rijeka, Faculty of Engineering; 2022 [cited 2025 January 24] Available at: https://urn.nsk.hr/urn:nbn:hr:190:092445

M. Čuček, "Opstrujavanje aerodinamičnog profila", Undergraduate thesis, University of Rijeka, Faculty of Engineering, Rijeka, 2022. Available at: https://urn.nsk.hr/urn:nbn:hr:190:092445

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Metadata
TitleOpstrujavanje aerodinamičnog profila
Title (english)Flow around aerodynamic body
AuthorMatej Čuček
MentorLado Kranjčević (mentor)
Committee memberKristian Lenić (predsjednik povjerenstva)
Committee memberLado Kranjčević (član 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 country2022-09-20, Croatia
Scientific / art field,
discipline and subdiscipline		TECHNICAL SCIENCES
Mechanical Engineering
Abstract
Ovaj rad bavi se aerodinamikom aviona. Prvi dio rada odnosi se na izradu 3D modela aviona s prilagođenim novim krilom, odnosno NACA 2411 profilom u programu Autodesk Inventor. Nakon izrade 3D modela, korišten je Hypermesh za izradu numeričke mreže. Dobivena numerička mreža ubačena je u Virtual Wind Tunnel gdje je provedeno nekoliko simulacija koje su uspoređene i na temelju kojih su doneseni zaključci.
Abstract (english)
The topic of this final thesis is the aerodynamics of airplanes. The first part refers to the creation of a 3D model of the airplane with an adapted new wing NACA 2411 profile in the Autodesk Inventor program. After a 3D model was created, Hypermesh was used to create the numerical mesh. The resulting numerical network was inserted into Virtual Wind Tunnel, where several simulations were performed, compared, and based on which conclusions were drawn.
Keywords
Keywords (english)
Languagecroatian
URN:NBNurn:nbn:hr:190:092445
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 conditionsOpen access
Terms of useLicence Attribution 4.0 International (CC BY 4.0) icon
Created on2022-11-28 09:25:25