A Shell/3D Modeling Technique for the Analysis of Delaminated Composite Laminates

By Krueger Ronald. 2000

186 citations recorded by the source corpus.

How researchers see this paper

The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.

Barely visible impact damage in scaled composite laminates: Experiments and numerical simulations (2017, unknown): “…al. [28,29] for a non-matched mesh coupling techniques, Ledentsov et al. [30] for applications of sheet metal forming simulation, Krueger et al.[31–34] in studying composite structures with delaminations, Cho and Kim [35] in investigating bifurcation buckling behaviour of delaminated composites,…”
Comparison of 2D finite element modeling assumptions with results from 3D analysis for composite skin-stiffener debonding (2002, methodology): “For future detailed modeling and analysis of the damage observed during the experiments, the shell/3D modeling technique [11] offers great potential for saving modeling and computational effort because only a relatively small section in the vicinity of the delamination front needs to modeled with so”