The usage of composite material have been increasing the last decades, especially
in industries such as aerospace and automotive. However, one of the
concerns regarding the usage of composite is its susceptibility to damage due
to low velocity impact (LVI). LVI can cause a barely visible impact damage
(BVID) which can compromise the compression strength significantly. In
this reseach, finite element method (FEM) models based on Kirchoff’s Plate
Theory, Hashin-Rottem damage modelling, and Benzggagh-Kenane fracture
criterion are proposed to simulate the low velocity impact and compression
after impact (CAI) on composite laminate. The models are modelled and validated
with existing experiment data. The FEM model is used to find the
relationship between the impact energy and laminate orientations on the CAI
strength. The developed model could predict the composite behaviour considerably
well. The LVI impact energy is found to have an inverse power law
relationship with the CAI strength. The laminates with more 0 degree plies
tends to have higher compression strength while laminate with ±45 tends to
have better damage resistance.