Predictive methods for initiation of delamination and intra-laminar damage in carbon fibre reinforced polymer laminates subject to impact

• Published in: Aeronautical journal Vol. 128; no. 1323; pp. 846 - 874
• Main Authors: Raza, H., Rodera, O., Carpenter, K., Pärnänen, T., Jokinen, J., Kanerva, M., Bayandor, J.
• Format: Journal Article
• Language: English
• Published: 01.05.2024
• ISSN: 0001-9240; 2059-6464
• DOI: 10.1017/aer.2023.95

A comparison of the modelling methodologies to capture the damage onset and delamination initiation in Abaqus and LS-Dyna is presented. A quasi-isotropic carbon fibre reinforced polymer laminate is modelled under a low-energy impact scenario. Hashin, Puck and Cuntze criteria are implemented for assessing intra-laminar damage in Abaqus in the linear elastic regime without damage evolution, with Virtual Crack Closure Technique being used for inter-laminar failure. In LS-Dyna, the Chang-Chang criterion is used for the intra-lamina failure with damage evolution, whereas delamination is captured using cohesive zone model and the tiebreak contact algorithm. The implementations carried out by both finite element software result in a modelling work well set to analyse and predict the impact response at the initial stages of delamination and damage within the plies. The composite damage criteria used in both finite element codes overall predict stiffer results when compared with the experimental data, however, remain in close agreement with each other.