Measuring the notched compressive strength of composite laminates : Specimen size effects

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Thin ply composites: Experimental characterization and modeling of size-effects (2014, unknown): “Residual strains, fibre alignment and waviness, porosity and the amount of fibre clustering and resin rich zones tend to increase in larger and thicker structures, thus introducing another kind of size effect which is closely related to the production process [2,9,10].”
Failure mechanisms and damage evolution of laminated composites under compression after impact (CAI): Experimental and numerical study (2018, unknown): “Compressive failure strengths for the exact layups used here are not available but results from literature for layups similar to the Ps and Ss cases are 643 MPa [36] for a [452/902/-452/02]3S laminate and 675 MPa [37] a [45/90/-45/0]4S laminate.”
Progressive damage modeling of open-hole composite laminates under compression (2015, methodology): “Failure mechanism of 4 mm ply-level scaled laminates (a) experiment [25]; (b”