Finite element analysis on the compression and crush responses of laminates with unidirectionally arrayed chopped strand in 0° plies

Abstract The outstanding mechanical performance and flowability of unidirectionally arrayed chopped strands laminates (UACS) give them an advantage in the manufacture of engineering structures with complex geometries. In this research, the mechanical response of UACS laminates with bi‐angled slits and staggered slits under quasi‐static compression and progressive crushing loads is numerically analyzed for the first time. The aim is to clarify the damage mechanism of UACS laminates under compressive and crushing load. Simulation results reveal that the compressive strength of [90/0] 4s UACS laminates with bi‐angled slits is 635.9 MPa, with an error of 4.2% compared to experimental data. For the stacking sequence of [0/90] 4s , the strength is measured as 581.96 MPa with a 5% error. Proposed finite element model could accurately describe the mechanical properties of UACS laminates. Additionally, the progressive crushing response is in good agreement with the experimental data, the error in energy absorption for [90/0] 4s UACS laminates with bi‐angled slits is noted at 7% compared to experimental values. It has been demonstrated that bi‐angled slits significantly contribute in restraining the propagation of delamination and improving the amount of energy absorption of UACS laminates. Highlights The mechanical response of UACS laminates under compressive and progressive crushing load was numerically analyzed. The compressive damage propagation of UACS laminates with different slit patterns in 0° layer was demonstrated. The effect of different slit patterns on inhibiting delamination propagation and increasing energy absorption of UACS laminates under progressive crushing load was numerically analyzed.