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Rezultati

Computational modeling of aircraft lugs failure under fatigue loading   [2018]

Boljanović, Slobodanka  

Mixed mode crack growth simulation with/without overloads   [2014]

Boljanović, Slobodanka  ; Maksimović, Stevan

Welded joint geometry effect on fatigue crack growth resistance in different metallic materials   [2021]

Sedmak, Aleksandar  ; Hemer, Abubkr; Sedmak, Simon A.  ; Milović, Ljubica  ; Grbović, Aleksandar  ; Čabrilo, Aleksandar; Kljajin, Milan

Editorial: 22nd European Conference on Fracture (ECF 22)   [2020]

Sedmak, Aleksandar  ; Iacoviello, F.; Silberschmidt, V.; Schmauder, S.

Determination of optimum wing spar cross section for maximum fatigue life   [2019]

Grbović, Aleksandar  ; Kastratović, Gordana  ; Sedmak, Aleksandar  ; Eldweib, Khalid; Kirin, Snežana  

Fatigue life prediction of topologically optimized torque link adjusted for additive manufacturing   [2023]

Raicevic, N  ; Grbovic, Aleksandar M  ; Kastratovic, Gordana M  ; Vidanovic, Nenad D  ; Sedmak, Aleksandar S  

Fatigue strength assessment of initial semi-elliptical cracks located at a hole   [2016]

Boljanović, Slobodanka  ; Maksimović, Stevan; Djurić, Mirjana

Fatigue endurance design of plates with two semicircular edge notches and one quarter-elliptical corner crack or through-the-thickness crack   [2019]

Boljanović, Slobodanka  ; Maksimović, Stevan; Carpinteri, Andrea; Ćosić, Milena

The effects of welded clips on fatigue crack growth in AA6156 T6 panels   [2022]

Sedmak, Aleksandar  ; Grbović, Aleksandar  ; Petrovski, Blagoj; Sghayer, Abulgasem; Sedmak, Simon  ; Berto, Filippo; Đurđević, A.

Fatigue crack growth modeling of attachment lugs   [2014]

Boljanović, Slobodanka  ; Maksimović, Stevan

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