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undergraduate thesis
Aerodinamička svojstva NACA laminarnih aeroprofila
Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2021. urn:nbn:hr:235:275562
Ćorić, Domagoj
University of Zagreb
Faculty of Mechanical Engineering and Naval Architecture

Institutional repository: Repository of Faculty of Mechanical Engineering and Naval Architecture University of Zagreb

Cite this document

Ćorić, D. (2021). Aerodinamička svojstva NACA laminarnih aeroprofila (Undergraduate thesis). Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture. Retrieved from https://urn.nsk.hr/urn:nbn:hr:235:275562

Ćorić, Domagoj. "Aerodinamička svojstva NACA laminarnih aeroprofila." Undergraduate thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2021. https://urn.nsk.hr/urn:nbn:hr:235:275562

Ćorić, Domagoj. "Aerodinamička svojstva NACA laminarnih aeroprofila." Undergraduate thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2021. https://urn.nsk.hr/urn:nbn:hr:235:275562

Ćorić, D. (2021). 'Aerodinamička svojstva NACA laminarnih aeroprofila', Undergraduate thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, accessed 20 December 2024, https://urn.nsk.hr/urn:nbn:hr:235:275562

Ćorić D. Aerodinamička svojstva NACA laminarnih aeroprofila [Undergraduate thesis]. Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture; 2021 [cited 2024 December 20] Available at: https://urn.nsk.hr/urn:nbn:hr:235:275562

D. Ćorić, "Aerodinamička svojstva NACA laminarnih aeroprofila", Undergraduate thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, Zagreb, 2021. Available at: https://urn.nsk.hr/urn:nbn:hr:235:275562

Metadata
TitleAerodinamička svojstva NACA laminarnih aeroprofila
Title (english)Aerodynamic properties of NACA laminar airfoils
AuthorDomagoj Ćorić
MentorDubravko Matijašević (mentor)
GranterUniversity of Zagreb
Faculty of Mechanical Engineering and Naval Architecture
Zagreb
Defense date and country2021-10-01, Croatia
Scientific / art field,
discipline and subdiscipline		TECHNICAL SCIENCES
Aviation, Rocket and Space Technology
Aircraft Construction and Design
Abstract
U ovom radu prikazana je numerička analiza NACA laminarnih aeroprofila. Svođenjem debelih aeroprofila na srednju liniju pomoću teorije tankih aeroprofila određena je vrijednost idealnog napadnog kuta. Zatim, koristeći metodu kontrolnih volumena i 2D panelnu metodu implementiranu u XFOIL-u, određena su aerodinamička svojstva ispitnih aeroprofila s naglaskom na drag bucket. Konačno, numerička rješenja svojstava aeroprofila uspoređena su s dostupnim eksperimentima, a interpolacijom radijalnim baznim funkcijama i polinomijalnom linearnom regresijom obrađeni su prikupljeni podaci.
Abstract (english)
This thesis focuses on numerical analysis of NACA laminar airfoils. First of all, thick airfoils are reduced to main line by thin airfoil theory in order to analytically determine the ideal angle of attack. The aerodynamic properties of airfoils are determined using the Finite Volume Method and the 2D panel method implemented in XFOIL with emphasis on drag bucket analysis. Finally, numerical solutions of aerodynamic properties are compared to available measurements and gathered data is processed by means of radial basis function interpolation and polynomial linear regression.
Keywords
Keywords (english)
Languagecroatian
URN:NBNurn:nbn:hr:235:275562
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
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Created on2021-09-29 19:02:05