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master's thesis
Numerička simulacija krila s korigiranim napadnim rubom
2021. urn:nbn:hr:122:321824
Sitar, Kristina
University North
University centre Varaždin
Department of Mechanical Engineering

Cite this document

Sitar, K. (2021). Numerička simulacija krila s korigiranim napadnim rubom (Master's thesis). Koprivnica: University North. Retrieved from https://urn.nsk.hr/urn:nbn:hr:122:321824

Sitar, Kristina. "Numerička simulacija krila s korigiranim napadnim rubom." Master's thesis, University North, 2021. https://urn.nsk.hr/urn:nbn:hr:122:321824

Sitar, Kristina. "Numerička simulacija krila s korigiranim napadnim rubom." Master's thesis, University North, 2021. https://urn.nsk.hr/urn:nbn:hr:122:321824

Sitar, K. (2021). 'Numerička simulacija krila s korigiranim napadnim rubom', Master's thesis, University North, accessed 19 November 2024, https://urn.nsk.hr/urn:nbn:hr:122:321824

Sitar K. Numerička simulacija krila s korigiranim napadnim rubom [Master's thesis]. Koprivnica: University North; 2021 [cited 2024 November 19] Available at: https://urn.nsk.hr/urn:nbn:hr:122:321824

K. Sitar, "Numerička simulacija krila s korigiranim napadnim rubom", Master's thesis, University North, Koprivnica, 2021. Available at: https://urn.nsk.hr/urn:nbn:hr:122:321824

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Metadata
TitleNumerička simulacija krila s korigiranim napadnim rubom
Title (english)Numerical simulation of wing with tubercles
AuthorKristina Sitar
MentorJasna Leder Horina (mentor)
Committee memberJasna Leder Horina (predsjednik povjerenstva)
Committee memberSanja Šolić (član povjerenstva)
Committee memberMatija Bušić (član povjerenstva)
GranterUniversity North
(University centre Varaždin)
(Department of Mechanical Engineering)
Koprivnica
Defense date and country2021-09-29, Croatia
Scientific / art field,
discipline and subdiscipline		TECHNICAL SCIENCES
Mechanical Engineering
Abstract
U ovom diplomskom radu izvršena je numerička simulacija turbulentnog strujanja oko krila aviona pomoću programskog paketa ANSYS Fluent 2020R2. Cilj ovog rada je dati uvid u primjenu napadnog ruba te njegov utjecaj na aeroprofil. Objašnjen je matematički model viskoznog strujanja fluida, koji se temelji na Reynoldsovim osrednjenim Navier-Stokesovim jednadžbama (RANS). Za potrebe numeričke simulacije izrađena su tri modela aeroprofila. Prikazana je raspodjela polja brzina i polja tlakova, kao i aerodinamički koeficijenti uzgona i otpora.
Abstract (english)
In this thesis a numerical simulation of turbulent flow was performed around the airfoil using ANSYS Fluent 2020R2 software package. The main goal of this thesis is to give insights into the application of tubercles on the airfoil. Description of mathematical model of viscous fluid flow is given, which is based on Reynolds Averaged Navier-Stokes (RANS) equations. Three models of airfoil were created for the purpose of numerical simulation. Distribution of velocity and pressure fields are shown, as well as the aerodynamic lift and drag coefficient.
Keywords
Keywords (english)
Languagecroatian
URN:NBNurn:nbn:hr:122:321824
Study programmeTitle: Mechanical engineering
Study programme type: university
Study level: graduate
Academic / professional title: magistar/magistra inženjer/inženjerka strojarstva (magistar/magistra inženjer/inženjerka strojarstva)
Type of resourceText
File originBorn digital
Access conditionsOpen access
Terms of useLicence In copyright icon
Created on2022-03-18 14:50:50