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Browsing by Author Stevan Maksimović
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| Issue Date | Title | Author(s) | Type | М-cat. |
|---|---|---|---|---|
| 2010 | An analysis of crack propagation and a plasticity-induced closure effect | Boljanović, Slobodanka S.   ; Stevan Maksimović; Andrea Carpinteri | Article | 52M52 |
| 2013 | ANALYSIS OF AICRAFT STRUCTURES WITH RESPECTS TO FATIGUE AND FRACTURE MECHANICS | Stevan Maksimović; Vasović, Ivana ; Mirko Maksimović; Mirjana Đurić | Conference Paper | Mp. category will be shown later |
| 2019 | Analysis of two symmetric cracks at a hole under cyclic loading | Boljanović, Slobodanka S. ; Stevan Maksimović; Strain Posavljak | Conference Paper | Mp. category will be shown later |
| 2019 | CFD CALCULATION OF COMPOSITE UNMANNED AERIAL VEHICLE FOR ITS STRENGTH ANALYSIS | Stevan Maksimović; Maksimović, Katarina S. ; Vasović, Ivana V. | Conference Paper | Mp. category will be shown later |
| 2019 | CFD Load analysis and strength analysis of tail construction of tactical unmanned aerial vehicle made from composite materials (✓) | Stevan Maksimović; Zoran Vasić; Katarina Maksimović; Ivana Vasović Maksimović ; Mirko Maksimović | Conference Paper | Mp. category will be shown later |
| 2021 | CFD load and strength analysis of tactical unmanned aerial vehicle made from composite materials (✓) | Katarina Maksimović; Mirko Maksimović; Ivana Vasovic ; Dragi Stamenković; Stevan Maksimović | Other | Mp. category will be shown later |
| 2013 | Crack growth analysis of edge notched components under cyclic loading | Boljanović, Slobodanka S. ; Stevan Maksimović; Andrea Carpinteri | Conference Paper | Mp. category will be shown later |
| 2017 | Crack propagation analysis of cyclically loaded structural components | Boljanović, Slobodanka S. ; Stevan Maksimović; Strain Posavljak | Conference Paper | Mp. category will be shown later |
| 2010 | Fatigue crack analysis under mixed mode loading | Boljanović, Slobodanka S. ; Stevan Maksimović | Conference Paper | Mp. category will be shown later |
| 2016 | Fatigue failure analysis of pin-loaded lugs | Boljanović, Slobodanka S. ; Stevan Maksimović | Article | Mp. category will be shown later |
| 2011 | Fatigue life defining of aircraft engine disks | Strain Posavljak; Stevan Maksimović; Boljanović, Slobodanka S. | Conference Paper | Mp. category will be shown later |
| 2015 | FATIGUE LIFE ESTIMATION OF AIRCRAFT STRUCTURAL COMPONENTS WITH SURFACE CRACKS UNDER LOAD SPECTRUM | Mirko Maksimović; Stevan Maksimović; Mirjana Đurić; Vasović, Ivana | Conference Paper | Mp. category will be shown later |
| 2011 | Fatigue life estimation of cracked structural components | Boljanović, Slobodanka S. ; Stevan Maksimović; Strain Posavljak | Conference Paper | Mp. category will be shown later |
| 2010 | Fatigue Life Estimation of Notched Structural Components | Dragi Stamenković; Katarina Maksimović; Vera Nikolić-Stanojević; Stevan Maksimović; Stupar, Slobodan ; Vasović, Ivana | Article | 23M23 |
| 2013 | Fatigue life evaluation of damaged aircraft lugs | Boljanović, Slobodanka S. ; Stevan Maksimović; Andrea Carpinteri | Article | 51M51 |
| 2015 | Fatigue strength simulation of aircraft lug | Boljanović, Slobodanka S. ; Stevan Maksimović; Dragi Stamenković | Conference Paper | Mp. category will be shown later |
| 2009 | Finite element analyses of stress inensity factors of an elliptical surface cracks in a circural rode under tension | Blažić, Marija B. ; Stevan Maksimović | Conference Paper | Mp. category will be shown later |
| 2013 | IMPROVED COMPUTATION METHOD TO FATIGUE AND FRACTURE MECHANICS ANALYSIS OF AIRCRAFT STRUCTURES | Stevan Maksimović; Vasović, Ivana ; Mirko Maksimović; Mirjana Đurić | Conference Paper | Mp. category will be shown later |
| 2021 | Kompozitni segment lopatice glavnog rotora helikoptera ht-40 (✓) | Stevan Maksimović; Mirko Maksimović; Ivana Vasovic ; Katarina Maksimović; Marko Jarić | Patent | Mp. category will be shown later |
| 2016 | Modeling of crack growth under mixed mode loading - Paper No. 00091_0091 | Boljanović, Slobodanka ; Stevan Maksimović | Conference Paper | Mp. category will be shown later |