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master's thesis
Aerodinamička analiza PrandtlD letećeg krila
2022. urn:nbn:hr:235:353035
Aradski, David
University of Zagreb
Faculty of Mechanical Engineering and Naval Architecture

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Aradski, D. (2022). Aerodinamička analiza PrandtlD letećeg krila (Master's thesis). Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture. Retrieved from https://urn.nsk.hr/urn:nbn:hr:235:353035

Aradski, David. "Aerodinamička analiza PrandtlD letećeg krila." Master's thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2022. https://urn.nsk.hr/urn:nbn:hr:235:353035

Aradski, David. "Aerodinamička analiza PrandtlD letećeg krila." Master's thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2022. https://urn.nsk.hr/urn:nbn:hr:235:353035

Aradski, D. (2022). 'Aerodinamička analiza PrandtlD letećeg krila', Master's thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, accessed 19 April 2024, https://urn.nsk.hr/urn:nbn:hr:235:353035

Aradski D. Aerodinamička analiza PrandtlD letećeg krila [Master's thesis]. Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture; 2022 [cited 2024 April 19] Available at: https://urn.nsk.hr/urn:nbn:hr:235:353035

D. Aradski, "Aerodinamička analiza PrandtlD letećeg krila", Master's thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, Zagreb, 2022. Available at: https://urn.nsk.hr/urn:nbn:hr:235:353035

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Metadata
TitleAerodinamička analiza PrandtlD letećeg krila
Title (english)PrandtlD flying wing aerodynamic analysis
AuthorDavid Aradski
MentorDubravko Matijašević (mentor)
GranterUniversity of Zagreb
Faculty of Mechanical Engineering and Naval Architecture
Zagreb
Defense date and country2022-07-20, Croatia
Scientific / art field,
discipline and subdiscipline		TECHNICAL SCIENCES
Aviation, Rocket and Space Technology
Abstract
U ovom radu analizirana je letjelica PrandtlD. PrandtlD leteće krilo je konstuirano kako bi se istražila mogućnost leta sa zvonolikom raspodjelom opterećenja te kako bi se testirali efekti koji se pojavljuju zbog pozitivne brzine ispiranja pri vrhovima krila. Rekonstuirana je geometrija letjelice, provedeni su proračuni krila i aeroprofila metodom konačnih volumena te je provedena analiza numeričkom adaptacijom noseće linije za otklon upravljačkih površina kako bi se istražila mogućnost povoljnog skretanja.
Abstract (english)
In this thesis, the PrandtlD aircraft was analyzed. PrandtlD flying wing was constructed to investigate the possibility of flight with a bell-shaped spanload and to test the effects that occur due to the upwash velocity at the wingtips. The geometry of the aircraft was reconstructed, wing and airfoil calculations were carried out using the finite volume method and numerical adaptation of the lifting line was used to analyze deflection of the control surfaces in order to investigate the possibility of a proverse yaw.
Keywords
Keywords (english)
Languagecroatian
URN:NBNurn:nbn:hr:235:353035
Study programmeTitle: Aeronautical Studies
Study programme type: university
Study level: graduate
Academic / professional title: magistar/magistra inženjer/inženjerka zrakoplovnog inženjerstva (magistar/magistra inženjer/inženjerka zrakoplovnog inženjerstva)
Type of resourceText
File originBorn digital
Access conditionsOpen access
Terms of useLicence Attribution-ShareAlike 4.0 International (CC BY-SA 4.0) icon
Created on2022-07-18 07:41:34