Zobrazeno 1 - 10
of 53
pro vyhledávání: '"Maksimović Katarina"'
Autor:
Maksimović Katarina, Maksimović Mirko, Vasović-Maksimović Ivana, Rašuo Boško, Maksimović Stevan
Publikováno v:
FME Transactions, Vol 48, Iss 2, Pp 447-453 (2020)
This work considers the buckling and postbuckling behaviour of axially compressed layered composite panels including initial failure analysis. For determination stresses in layered composite panels Finite Element Method (FEM) used. A series of experi
Externí odkaz:
https://doaj.org/article/3281feeb553e49e9bfe1a1c0e99ad1f5
Mathematical research is often motivated by the desire to reach a beautiful result or to prove it in an elegant way. Mathematician's work is thus strongly influenced by his aesthetic judgments. However, the criteria these judgments are based on remai
Externí odkaz:
http://arxiv.org/abs/2405.05379
Autor:
Maksimović Mirko S., Vasović Ivana V., Maksimović Katarina S., Trišović Nataša, Maksimović Stevan M.
Publikováno v:
FME Transactions, Vol 46, Iss 1, Pp 124-128 (2018)
The subject of this investigation is focused on developing computation procedure for strength analysis of damaged aircraft structural components with respect to fatigue and fracture mechanics. For that purpose, here will be defined computation proced
Externí odkaz:
https://doaj.org/article/2a835748208d4f25874110a175aeb3ae
Publikováno v:
Scientific Technical Review, Vol 66, Iss 3, Pp 27-33 (2016)
Rotational components of aero engine turbine are the most important components. It operates at high temperature and under conditions of extreme environmental attack such as oxidation, corrosion and wear. These conditions can cause cracking of rotatio
Externí odkaz:
https://doaj.org/article/21b82cffcac44991af841da8a509bb7d
Autor:
Ugrčić Marinko, Maksimović Stevan M., Stamenković Dragi P., Maksimović Katarina S., Nabil Khettou
Publikováno v:
FME Transactions, Vol 43, Iss 1, Pp 76-81 (2015)
Bird strike events are a potential dangerous problem faced by flight safety nowadays. These events are usually simulated through numerical approaches due mainly to the technical difficulties and high costs associated with experimental tests. The cons
Externí odkaz:
https://doaj.org/article/8fe493a2dfa545988abe1296aa8d5e7f
Publikováno v:
Scientific Technical Review, Vol 64, Iss 1, Pp 30-34 (2014)
The main and primary structures in airframes are composed of stiffened panels in order to obtain high specific strength. This paper considers the finite element modelling to evaluate the fracture behaviour of cracked thin-walled structural components
Externí odkaz:
https://doaj.org/article/f273a3c5ca7b441b9b2fc6c19a1d3ae1
Publikováno v:
Theoretical and Applied Mechanics, Vol 40, Iss 2, Pp 247-261 (2013)
This work considers the numerical computation methods and procedures for the fatigue crack growth predicting of cracked notched structural components. Computation method is based on fatigue life prediction using the strain energy density approach.
Externí odkaz:
https://doaj.org/article/a3cc2086633345de8187fd266017bbb6
Autor:
You, Justin a, Maksimovic, Katarina a, Metri, Mark N. a, b, Schoeppe, Anneka a, b, Chen, Karin a, b, Lee, Jooyun a, b, Santos, Jhune Rizsan a, b, Youssef, Mohieldin M.M. a, Salter, Michael W. c, d, Park, Jeehye a, b, ⁎
Publikováno v:
In Heliyon 30 September 2024 10(18)
Akademický článek
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Autor:
Maksimović, Katarina
Publikováno v:
Arhe. (34):61-83
Externí odkaz:
https://www.ceeol.com/search/article-detail?id=945073