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master's thesis
Analiza odabranih performansi helikoptera s koaksijalnim rotorom
Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2016. urn:nbn:hr:235:783643
Šego, Neven
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

Šego, N. (2016). Analiza odabranih performansi helikoptera s koaksijalnim rotorom (Master's thesis). Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture. Retrieved from https://urn.nsk.hr/urn:nbn:hr:235:783643

Šego, Neven. "Analiza odabranih performansi helikoptera s koaksijalnim rotorom." Master's thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2016. https://urn.nsk.hr/urn:nbn:hr:235:783643

Šego, Neven. "Analiza odabranih performansi helikoptera s koaksijalnim rotorom." Master's thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2016. https://urn.nsk.hr/urn:nbn:hr:235:783643

Šego, N. (2016). 'Analiza odabranih performansi helikoptera s koaksijalnim rotorom', Master's thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, accessed 29 November 2024, https://urn.nsk.hr/urn:nbn:hr:235:783643

Šego N. Analiza odabranih performansi helikoptera s koaksijalnim rotorom [Master's thesis]. Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture; 2016 [cited 2024 November 29] Available at: https://urn.nsk.hr/urn:nbn:hr:235:783643

N. Šego, "Analiza odabranih performansi helikoptera s koaksijalnim rotorom", Master's thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, Zagreb, 2016. Available at: https://urn.nsk.hr/urn:nbn:hr:235:783643

Metadata
TitleAnaliza odabranih performansi helikoptera s koaksijalnim rotorom
Title (english)Selected performance analysis for the helicopter with coaxial rotor
AuthorNeven Šego
MentorMilan Vrdoljak (mentor)
GranterUniversity of Zagreb
Faculty of Mechanical Engineering and Naval Architecture
Zagreb
Defense date and country2016-05-20, Croatia
Scientific / art field,
discipline and subdiscipline		TECHNICAL SCIENCES
Aviation, Rocket and Space Technology
Abstract
Rad obuhvaća postavljanje osnovnih jednadžbi teorije diska za rotor helikoptera, njihovu prilagodbu za potrebe analize koaksijalnog rotora te izradu pripadajućeg aerodinamičkog modela. Rezultati teorije su uspoređeni s relevantnim izvorima (Leishman, Harrington, Dingeldein) te nakon toga primijenjeni na dva helikoptera iz aktivne vojne službe – ruskom Ka-50 i američkom AH-64.
Abstract (english)
This paper consists of putting together the equations neccessary for the momentum theory for helicopter rotors, their modification for the use with coaxial rotors and the making of an aerodynamical model accordingly. The results are compared to those given in relevant papers and books (Leishman, Harrington, Dingeldein) and then applied to two modern military helicopters still in use today – the Russian Ka-50 and the American AH-64.
Keywords
Keywords (english)
Languagecroatian
URN:NBNurn:nbn:hr:235:783643
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 In copyright icon
Created on2019-05-28 09:31:46