prikaz prve stranice dokumenta Model aerodinamike nadzvučnih brzina modernog lovačkog aviona
Embargo period 2026-03-21
master's thesis
Model aerodinamike nadzvučnih brzina modernog lovačkog aviona
Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2024. urn:nbn:hr:235:319658
Špelić, Nikolina
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

Špelić, N. (2024). Model aerodinamike nadzvučnih brzina modernog lovačkog aviona (Master's thesis). Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture. Retrieved from https://urn.nsk.hr/urn:nbn:hr:235:319658

Špelić, Nikolina. "Model aerodinamike nadzvučnih brzina modernog lovačkog aviona." Master's thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2024. https://urn.nsk.hr/urn:nbn:hr:235:319658

Špelić, Nikolina. "Model aerodinamike nadzvučnih brzina modernog lovačkog aviona." Master's thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2024. https://urn.nsk.hr/urn:nbn:hr:235:319658

Špelić, N. (2024). 'Model aerodinamike nadzvučnih brzina modernog lovačkog aviona', Master's thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, accessed 25 August 2024, https://urn.nsk.hr/urn:nbn:hr:235:319658

Špelić N. Model aerodinamike nadzvučnih brzina modernog lovačkog aviona [Master's thesis]. Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture; 2024 [cited 2024 August 25] Available at: https://urn.nsk.hr/urn:nbn:hr:235:319658

N. Špelić, "Model aerodinamike nadzvučnih brzina modernog lovačkog aviona", Master's thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, Zagreb, 2024. Available at: https://urn.nsk.hr/urn:nbn:hr:235:319658

Metadata
TitleModel aerodinamike nadzvučnih brzina modernog lovačkog aviona
Title (english)Supersonic aerodynamics model for modern fighter aircraft
AuthorNikolina Špelić
MentorMilan Vrdoljak (mentor)
MentorMarijan Andrić (komentor)
GranterUniversity of Zagreb
Faculty of Mechanical Engineering and Naval Architecture
Zagreb
Defense date and country2024-03-27, Croatia
Scientific / art field,
discipline and subdiscipline		TECHNICAL SCIENCES
Aviation, Rocket and Space Technology
Abstract
U ovom diplomskom radu napravljen je model aerodinamike nadzvučnih brzina modernog lovačkog aviona s konfiguracijom kanard-krilo, nalik na Dassault Rafale. Prikazane su osnove geometrijske i inercijske značajke aviona. Metodama projektne aerodinamike procijenjene su aerodinamičke značajke aviona za normalnu silu i moment propinjanja, za bočnu silu i moment skretanja, te za moment valjanja. Procjene su napravljene za dva Machova broja: 1,2 i 1,6. Nadalje, određeni su linearni modeli dinamike leta i analizirana je stabilnost u odabranim režimima nadzvučnog leta. Linearno uzdužno i bočno gibanje aviona je razmatrano odvojeno. Provedena je ocjena kvalitete direktnog upravljanja u odabranim režimima nadzvučnog leta. Konačno, pregledno su prikazani svi rezultati dobiveni za nadzvučni let zajedno s ranije dostupnim rezultatima za dozvučni let.
Abstract (english)
In this thesis supersonic aerodynamics model for modern fighter aircraft with a canard-wing configuration, similar to Dassault Rafale, is made. The basic information about geometric and inertial characteristics of airplane are shown. Airplane aerodynamic characteristics for normal force and pitching moment, for side force and yawing moment, and for rolling moment are evaluated using analytic aerodynamic methods. Evaluations are made for two Mach numbers: 1,2 and 1,6. Moreover, linear models of flight dynamics are made and stability in selected regimes of supersonic flight is analysed. Linear longitudinal and lateral motion of the airplane was considered separately. Flying qualities of airplane in selected regimes of supersonic flight are evaluated. Finally, all results obtained for supersonic flight are presented together with previously available results for subsonic flight.
Keywords
Keywords (english)
Languagecroatian
URN:NBNurn:nbn:hr:235:319658
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 conditionsEmbargoed access
Embargo expiration date: 2026-03-21
Terms of useLicence In copyright icon
Created on2024-03-26 08:13:36