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Numerical analysis of high velocity, oblique impacts and residual tensile strength of carbon/epoxy laminates (2020)
Journal Article

This paper presents prediction of the high velocity, oblique impact response and quasi-static residual tensile strength of thin [45/90/−45/0]2s carbon/epoxy laminates using finite element (FE) models. A High-Fidelity Finite Element Method (Hi-FEM) wi... Read More about Numerical analysis of high velocity, oblique impacts and residual tensile strength of carbon/epoxy laminates.

Virtual characterization of nonlocal continuum damage model parameters using a high fidelity finite element model (2020)
Journal Article

A virtual finite element framework is presented to provide the transition from a high fidelity model to a more computationally efficient continuum model for simulating fibre-dominated damage behavior in composite laminates subjected to tensile loadin... Read More about Virtual characterization of nonlocal continuum damage model parameters using a high fidelity finite element model.

Novel tape termination method for automated fibre placement: Cutting characteristics and delamination suppression (2020)
Journal Article

A novel tape termination method for tapering the ply end and removing the fibre discontinuity owing to a dropped ply in a tapered composite was demonstrated. The forces required for this process – referred to as tape scarfing – were experimentally in... Read More about Novel tape termination method for automated fibre placement: Cutting characteristics and delamination suppression.

An experimental study of scaling effects in notched quasi-isotropic carbon/epoxy laminates under compressive loads (2020)
Journal Article

The size effects in centre-notched quasi-isotropic carbon/epoxy laminates under compression were investigated. The in-plane dimensions of the baseline specimen were scaled up by a factor of up to 14. The centre-notched specimens were compared to open... Read More about An experimental study of scaling effects in notched quasi-isotropic carbon/epoxy laminates under compressive loads.