Numerical Simulation of Delamination Growth in Composite Materials
By Pedro P. Camanho, C. Dávila, D. Ambur. 2001
136 citations recorded by the source corpus.
View Paper: https://www.semanticscholar.org/paper/23d3beeaed1cf841abc0c12bbd75ad528631c687
How researchers see this paper
The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.
- Pedro P. Camanho
- De Xie
- Marco Gherlone
- Alexander Tessler
- Tong Earn Tay
- Anthony M. Waas
- J. Pascoe
- C. Dávila
Citations in the corpus
- Progressive Failure Analysis of Composites (2008, methodology): “Another similar example but with degradation factors assigned to different failure modes for threedimensional (3D) finite element implementation was developed by Camanho and Matthews [21] to predict damage progression and strength of mechanically fastened joints in carbon fiber-reinforced plastics f”
- Discrete cohesive zone model for mixed-mode fracture using finite element analysis (2006, methodology): “[37–41] have implemented this type of element in ABAQUS and provided many valuable results for wide range of problems.”
- Methods for the prediction of fatigue delamination growth in composites and adhesive bonds: A critical review (2013, background): “Ultimately all the XFEM-based delamination growth methods proposed so far, as well as potential future methods based on the CZMs discussed earlier, rely on a fracture mechanics model, correlating SIF or SERR with the delamination growth rate.”
- Finite element modeling of mode I delamination growth in laminated DCB specimens with R-curve effects (2013, unknown): “[22] assumed that the rmax is about 40% of the matrix yield strength to mitigate convergence problems.”
- Mixed-Mode Decohesion Finite Elements for the Simulation of Delamination in Composite Materials (2002, methodology): “Decohesion elements are based on a Dudgale-Barenblatt cohesive zone approach [12], [13], which can be related to Griffith’s theory of fracture when the cohesive zone size is negligible when compared with characteristic dimensions, regardless of the shape of the constitutive equation [14].”
- A homogeneous limit methodology and refinements of computationally efficient zigzag theory for homogeneous, laminated composite, and sandwich plates (2011, methodology): “Computational methods for nonlinear progressive failure analysis commonly employ cohesive elements and ply-by-ply discretizations, resulting in exceedingly intensive computations, particularly when large structures are analyzed [18,19].”