Numerička analiza naprezanja uzdužnicama ojačanog zrakoplovnog panela koji sadrži otvor

Ceilinger, Petra (2018) Numerička analiza naprezanja uzdužnicama ojačanog zrakoplovnog panela koji sadrži otvor. = Numerical Stress Analysis of an Aeronautical Stringer Stiffened Panel With a Cutout. Undergraduate thesis , Sveučilište u Zagrebu, Fakultet strojarstva i brodogradnje, UNSPECIFIED. Mentor: Ivančević, Darko.

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Abstract (Croatian)

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

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.

Item Type: Thesis (Undergraduate thesis)
Uncontrolled Keywords: panel ojačan uzdužnicama s otvorom; metoda tri uzdužnice; analitička analiza; numerička analiza; MKE
Keywords (Croatian): stringer stiffened panel with cutout; three stringer method; analytical analysis; numerical analysis; FEM
Subjects: TECHNICAL SCIENCE > Aviation, rocket and space technology > construction and establishment of a spacecraft
Divisions: 1300 Department of Aeronautical Engineering > 1310 Chair of Aerodynamics
Date Deposited: 26 Feb 2018 10:10
Last Modified: 06 Mar 2018 11:16
URI: http://repozitorij.fsb.hr/id/eprint/8472

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