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undergraduate thesis
Strujanje oko objekta u zračnom tunelu
2023. urn:nbn:hr:190:988530
Posarić, Borut
University of Rijeka
Faculty of Engineering

Cite this document

Posarić, B. (2023). Strujanje oko objekta u zračnom tunelu (Undergraduate thesis). Rijeka: University of Rijeka, Faculty of Engineering. Retrieved from https://urn.nsk.hr/urn:nbn:hr:190:988530

Posarić, Borut. "Strujanje oko objekta u zračnom tunelu." Undergraduate thesis, University of Rijeka, Faculty of Engineering, 2023. https://urn.nsk.hr/urn:nbn:hr:190:988530

Posarić, Borut. "Strujanje oko objekta u zračnom tunelu." Undergraduate thesis, University of Rijeka, Faculty of Engineering, 2023. https://urn.nsk.hr/urn:nbn:hr:190:988530

Posarić, B. (2023). 'Strujanje oko objekta u zračnom tunelu', Undergraduate thesis, University of Rijeka, Faculty of Engineering, accessed 05 May 2024, https://urn.nsk.hr/urn:nbn:hr:190:988530

Posarić B. Strujanje oko objekta u zračnom tunelu [Undergraduate thesis]. Rijeka: University of Rijeka, Faculty of Engineering; 2023 [cited 2024 May 05] Available at: https://urn.nsk.hr/urn:nbn:hr:190:988530

B. Posarić, "Strujanje oko objekta u zračnom tunelu", Undergraduate thesis, University of Rijeka, Faculty of Engineering, Rijeka, 2023. Available at: https://urn.nsk.hr/urn:nbn:hr:190:988530

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Metadata
TitleStrujanje oko objekta u zračnom tunelu
Title (english)Streaming around an object in a wind tunnel
AuthorBorut Posarić
MentorLado Kranjčević (mentor)
Committee memberSamir Žic (predsjednik povjerenstva)
Committee memberLado Kranjčević (član povjerenstva)
GranterUniversity of Rijeka
Faculty of Engineering
Rijeka
Defense date and country2023-07-11, Croatia
Scientific / art field,
discipline and subdiscipline		TECHNICAL SCIENCES
Mechanical Engineering
Abstract
U ovom završnom radu provodi se aerodinamička analiza modela aeroprofila NACA 0012. Na temelju NASA-inog eksperimenta aerodinamike aeroprofila, napravljen je slučaj validacije putem Altairovog Virtual Wind Tunnel softverskog paketa. Validacija je potvrđena metodom RMSE (root mean square error) usporedbom eksperimentalnih podataka s numeričkim podacima dobivenim u ovom radu. Aeroprofil se rekreira u CAD softveru koristeći jednadžbu na NASA-inoj web stranici koja opisuje granice aeroprofila. Zatim se generira mreža aeroprofila i unosi u virtualni zračni tunel. Analiza CFD rezultata napravljena je korištenjem programa AcuFieldView i uspoređena pomoću Python programskog jezika.
Abstract (english)
In this undergraduate thesis an aerodynamic analysis of a NACA 0012 airfoil is carried out. Based on NASA’s experiment of aerodynamics of an airfoil, a validation case is made with Altair’s Virtual Wind Tunnel software. The validation is confirmed using RMSE (root mean sqare error) method through comparing experimental data with numerical ones produced in this thesis. The airfoil is recreated in CAD software using an equation provided on NASA’s website which describes the boundaries of the airfoil. A mesh of the airfoil is then generated and imported in a virtual wind tunnel. Analysis of CFD results are made using AcuFieldView and compared using Python programming language.
Keywords
Keywords (english)
Languagecroatian
URN:NBNurn:nbn:hr:190:988530
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-NonCommercial-NoDerivatives 4.0 International (CC BY-NC-ND 4.0) icon
Created on2023-07-13 07:13:44