Zobrazeno 1 - 10
of 81
pro vyhledávání: '"Maksimović Stevan"'
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
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
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 65, Iss 3, Pp 46-54 (2015)
Performance of aircraft in general, its systems and airframe materials, can be significantly reduced by environmental conditions in which the aircraft operates during the service life. Material performance of steel and aluminum alloys can be greatly
Externí odkaz:
https://doaj.org/article/6e75479d5d88430389c11099ee30e126
Publikováno v:
MATEC Web of Conferences, Vol 300, p 11005 (2019)
This work explores the failure resistance of fatigue damages with random orientation through a new computational framework. Such analytical model aims to enable designers to properly and quickly assess stress state and residual life under cyclic load
Externí odkaz:
https://doaj.org/article/fc370d8e65d34c63ab1f858183ade68e
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
Publikováno v:
In Theoretical and Applied Fracture Mechanics August 2020 108
Publikováno v:
In International Journal of Fatigue October 2019 127:45-52
Autor:
Maksimović, Mirko, Vasović, Ivana, Maksimović, Katarina, Maksimović, Stevan, Stamenković, Dragi
Publikováno v:
In Procedia Structural Integrity 2018 13:1888-1894
Publikováno v:
In Procedia Structural Integrity 2018 13:1093-1098