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undergraduate thesis
Numerička analiza naprezanja uzdužnicama ojačanog zrakoplovnog panela koji sadrži otvor
2018. urn:nbn:hr:235:795643
Ceilinger, Petra
University of Zagreb
Faculty of Mechanical Engineering and Naval Architecture

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Ceilinger, P. (2018). Numerička analiza naprezanja uzdužnicama ojačanog zrakoplovnog panela koji sadrži otvor (Undergraduate thesis). Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture. Retrieved from https://urn.nsk.hr/urn:nbn:hr:235:795643

Ceilinger, Petra. "Numerička analiza naprezanja uzdužnicama ojačanog zrakoplovnog panela koji sadrži otvor." Undergraduate thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2018. https://urn.nsk.hr/urn:nbn:hr:235:795643

Ceilinger, Petra. "Numerička analiza naprezanja uzdužnicama ojačanog zrakoplovnog panela koji sadrži otvor." Undergraduate thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2018. https://urn.nsk.hr/urn:nbn:hr:235:795643

Ceilinger, P. (2018). 'Numerička analiza naprezanja uzdužnicama ojačanog zrakoplovnog panela koji sadrži otvor', Undergraduate thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, accessed 07 December 2024, https://urn.nsk.hr/urn:nbn:hr:235:795643

Ceilinger P. Numerička analiza naprezanja uzdužnicama ojačanog zrakoplovnog panela koji sadrži otvor [Undergraduate thesis]. Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture; 2018 [cited 2024 December 07] Available at: https://urn.nsk.hr/urn:nbn:hr:235:795643

P. Ceilinger, "Numerička analiza naprezanja uzdužnicama ojačanog zrakoplovnog panela koji sadrži otvor", Undergraduate thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, Zagreb, 2018. Available at: https://urn.nsk.hr/urn:nbn:hr:235:795643

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Metadata
TitleNumerička analiza naprezanja uzdužnicama ojačanog zrakoplovnog panela koji sadrži otvor
Title (english)Numerical Stress Analysis of an Aeronautical Stringer Stiffened Panel With a Cutout
AuthorPetra Ceilinger
MentorDarko Ivančević (mentor)
GranterUniversity of Zagreb
Faculty of Mechanical Engineering and Naval Architecture
Zagreb
Defense date and country2018-03-02, Croatia
Scientific / art field,
discipline and subdiscipline		TECHNICAL SCIENCES
Aviation, Rocket and Space Technology
Abstract
Sadržaj ovog rada je analiza naprezanja uzdužnicama ojačanog zrakoplovnog panela koji sadrži otvor. Provedene su analitičke i numeričke analize. Analitička analiza provedena je metodom tri uzdužnice koja je također opisana u sadržaju ovog rada, a numerička analiza je rađena u programu Abaqus/Standard koristeći metodu konačnih elemenata. Rezultati analiza uspoređeni su u poglavlju 5. Na samom kraju ovog rada nalazi se zaključak.
Abstract (english)
The subject of this thesis is stress analysis of an aeronautical stringer stiffened panel with a cutout. Analytical and numerical analyses were performed. Analytical analysis was carried out using three stringer method, which is also described in this thesis, and numerical analysis was performed using Finite Element Method in Abaqus/Standard. The results of analyses were compared in section 5. The final section contains the conclusion.
Keywords
Keywords (english)
Languagecroatian
URN:NBNurn:nbn:hr:235:795643
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
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Created on2019-05-28 09:41:36