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master's thesis
Proračun čvrstoće kompozitne konstrukcije krila hidroaviona
Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2022. urn:nbn:hr:235:029036
Jelić, 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

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Jelić, D. (2022). Proračun čvrstoće kompozitne konstrukcije krila hidroaviona (Master's thesis). Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture. Retrieved from https://urn.nsk.hr/urn:nbn:hr:235:029036

Jelić, Domagoj. "Proračun čvrstoće kompozitne konstrukcije krila hidroaviona." Master's thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2022. https://urn.nsk.hr/urn:nbn:hr:235:029036

Jelić, Domagoj. "Proračun čvrstoće kompozitne konstrukcije krila hidroaviona." Master's thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2022. https://urn.nsk.hr/urn:nbn:hr:235:029036

Jelić, D. (2022). 'Proračun čvrstoće kompozitne konstrukcije krila hidroaviona', Master's thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, accessed 26 December 2024, https://urn.nsk.hr/urn:nbn:hr:235:029036

Jelić D. Proračun čvrstoće kompozitne konstrukcije krila hidroaviona [Master's thesis]. Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture; 2022 [cited 2024 December 26] Available at: https://urn.nsk.hr/urn:nbn:hr:235:029036

D. Jelić, "Proračun čvrstoće kompozitne konstrukcije krila hidroaviona", Master's thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, Zagreb, 2022. Available at: https://urn.nsk.hr/urn:nbn:hr:235:029036

Metadata
TitleProračun čvrstoće kompozitne konstrukcije krila hidroaviona
Title (english)Strenght analysis of a hydroplane composite wing structure
AuthorDomagoj Jelić
MentorDarko Ivančević (mentor)
Committee memberMilan Vrdoljak (predsjednik povjerenstva)
Committee memberIvica Smojver (član povjerenstva)
Committee memberJosip Stepanić (član povjerenstva)
Committee memberDragutin Lisjak (član povjerenstva)
GranterUniversity of Zagreb
Faculty of Mechanical Engineering and Naval Architecture
Zagreb
Defense date and country2022-05-12, Croatia
Scientific / art field,
discipline and subdiscipline		TECHNICAL SCIENCES
Aviation, Rocket and Space Technology
Aircraft Construction and Design
Abstract
U radu je provedena numerička analiza proračuna sendvič konstrukcije krila hidroaviona čija maksimalna poletna masa iznosi 1400 kg. Na temelju dobivenog CAD modela hidroaviona izrađen je numerički model konstrukcije krila pri čemu je raspodjela opterećenja pri manevriranju proračunata u programskom paketu XFRL5. Polinom koji opisuje raspodjelu tlaka po donjaci dobiven je u programskom paketu Matlab. Numeričke analize provedene su primjenom Abaqus/Standard programa, a proračun čvrstoće proveden je temeljem graničnog i krajnjeg opterećenja iz V-n dijagrama.
Abstract (english)
In this master’s thesis numerical analysis of the sandwich structure of a seaplane wing with a maximum take-off weight of 1400 kg has been done. Based on the given CAD model of seaplane, a model of the wing structure was made, where the load distribution during maneuvering was calculated in the XFLR5 softwer package. A polynomial describing pressure distribution of the wing lower surface was obtained in Matlab softwer package. Numerical analyses were performed using the Abaqus/Standard program, and the strength analysis was performed based on ultimate and final loads from the V-n diagram.
Keywords
Keywords (english)
Languagecroatian
URN:NBNurn:nbn:hr:235:029036
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 on2022-05-14 15:45:57