Low-velocity impact damage on dispersed stacking sequence laminates. Part II: Numerical simulations

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Barely visible impact damage in scaled composite laminates: Experiments and numerical simulations (2017, neutral): “By combining Continuum Damage Mechanics (CDM) at the ply level and Cohesive Zone Modelling (CZM) at interlaminar regions, the degradation behaviour of plies and delaminations induced by low-54 velocity impact of laminated composites can be captured [2–11].”
Validation of low velocity impact modelling on different stacking sequences of CFRP laminates and influence of fibre failure (2013, methodology): “For FE modelling, an alternative method is to dissipate the energy release rate of fibre failure spreading over the volume finite element such as the modelling of [8] [1] [13] [12] [11].”
Design of adhesively bonded lap joints with laminated CFRP adherends: Review, challenges and new opportunities for aerospace structures (2021, background): “Nonetheless, by changing the laminate design, composite properties can be tailored to the external loading and research in this ﬁ eld of composites shows that certain stacking sequences can retard delam-ination [6 – 8].”