Farhad Shahabi - Academia.edu (original) (raw)
Papers by Farhad Shahabi
xii 4.6 Couple stress components (m 331) β , (m 332) β , and (m 333) β. .. .. .. .. .. .. .. . 85... more xii 4.6 Couple stress components (m 331) β , (m 332) β , and (m 333) β. .. .. .. .. .. .. .. . 85 4.7 Couple stress components (m 331) β , (m 332) β , and (m 333) β for cases with (4 × 4 × 8) and (8 × × 16) unit cells and (2 × 2 × 4) averaging domains .
Theoretical and Applied Fracture Mechanics, 2016
Engineering Fracture Mechanics, 2015
Applied Mathematical Modelling, 2013
Procedia Engineering, 2011
In this paper, the cohesive zone constitutive law is implemented at interface between delaminated... more In this paper, the cohesive zone constitutive law is implemented at interface between delaminated layers to simulate buckling driven delamination propagation in the laminates. The influence of single and multi delaminations on post-buckling behaviour of laminated are investigated and compared by obtained results of other method and the available experiments. It is shown that post-buckling delamination propagation can be predicted well, by utilizing a damageable interface element.
xii 4.6 Couple stress components (m 331) β , (m 332) β , and (m 333) β. .. .. .. .. .. .. .. . 85... more xii 4.6 Couple stress components (m 331) β , (m 332) β , and (m 333) β. .. .. .. .. .. .. .. . 85 4.7 Couple stress components (m 331) β , (m 332) β , and (m 333) β for cases with (4 × 4 × 8) and (8 × × 16) unit cells and (2 × 2 × 4) averaging domains .
Theoretical and Applied Fracture Mechanics, 2016
Engineering Fracture Mechanics, 2015
Applied Mathematical Modelling, 2013
Procedia Engineering, 2011
In this paper, the cohesive zone constitutive law is implemented at interface between delaminated... more In this paper, the cohesive zone constitutive law is implemented at interface between delaminated layers to simulate buckling driven delamination propagation in the laminates. The influence of single and multi delaminations on post-buckling behaviour of laminated are investigated and compared by obtained results of other method and the available experiments. It is shown that post-buckling delamination propagation can be predicted well, by utilizing a damageable interface element.