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undergraduate thesis
Aerodinamička svojstva refleksnih aeroprofila
2020. urn:nbn:hr:235:391513
Kos, Matej
University of Zagreb
Faculty of Mechanical Engineering and Naval Architecture

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Kos, M. (2020). Aerodinamička svojstva refleksnih aeroprofila (Undergraduate thesis). Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture. Retrieved from https://urn.nsk.hr/urn:nbn:hr:235:391513

Kos, Matej. "Aerodinamička svojstva refleksnih aeroprofila." Undergraduate thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2020. https://urn.nsk.hr/urn:nbn:hr:235:391513

Kos, Matej. "Aerodinamička svojstva refleksnih aeroprofila." Undergraduate thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2020. https://urn.nsk.hr/urn:nbn:hr:235:391513

Kos, M. (2020). 'Aerodinamička svojstva refleksnih aeroprofila', Undergraduate thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, accessed 16 April 2024, https://urn.nsk.hr/urn:nbn:hr:235:391513

Kos M. Aerodinamička svojstva refleksnih aeroprofila [Undergraduate thesis]. Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture; 2020 [cited 2024 April 16] Available at: https://urn.nsk.hr/urn:nbn:hr:235:391513

M. Kos, "Aerodinamička svojstva refleksnih aeroprofila", Undergraduate thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, Zagreb, 2020. Available at: https://urn.nsk.hr/urn:nbn:hr:235:391513

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Metadata
TitleAerodinamička svojstva refleksnih aeroprofila
Title (english)Reflex airfoils aerodynamic characteristics
AuthorMatej Kos
MentorDubravko Matijašević (mentor)
GranterUniversity of Zagreb
Faculty of Mechanical Engineering and Naval Architecture
Zagreb
Defense date and country2020-09-22, Croatia
Scientific / art field,
discipline and subdiscipline		TECHNICAL SCIENCES
Aviation, Rocket and Space Technology
Abstract
U ovom radu predstavljena je analitčka i numerička aerodinamička analiza refleksnih aeroprofila. Implementirana je metoda za dobivanje srednje linije aeroprofila iz standarndog zapisa aeroprofila iz baze podataka. Dobivena srednja linija aeroprofila aproksimirana je Čebiševljevim polinomima prve vrste i na temelju toga prikazano je alternativno rješenje zadaće teorije tankih aeroprofila. Na kraju, izračunate aerodinamičke značajke uspoređene su s rezutatima dobivenim numeričkim pokusom pomoću paketa OpenFOAM.
Abstract (english)
This thesis deals with reflex airfoils aerodynamic characteristics obtained by analytical and numerical methods. The method implemented for extracting the mean airfoil camber line from standard airfoil format found in the database is described. The extracted mean camber line is approximated using Chebyshev polynomials of the first kind and based on that, an alternative solution to thin airfoil theory is shown. In the end, calculated aerodynamic characteristics are compared to results obtained from numerical experiments using OpenFOAM.
Keywords
Keywords (english)
Languagecroatian
URN:NBNurn:nbn:hr:235:391513
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
Terms of useLicence In copyright icon
Created on2020-09-17 13:58:39