C. Bouvet, B. Castanié, M. Bizeul, and J. J. Barrau, Low velocity impact modelling in laminate composite panels with discrete interface elements, Int J. Sol Struct, vol.46, pp.2809-2821, 2009.
URL : https://hal.archives-ouvertes.fr/hal-01851855

W. Tan, B. G. Falzon, L. Chiu, and M. Price, Predicting low velocity impact damage and Compression-After-Impact (CAI) behaviour of composite laminates, Comp Part A, vol.71, pp.212-226, 2015.

L. Adam, C. Bouvet, B. Castanié, A. Daidié, and E. Bonhomme, Discrete ply model of circular pull-through test of fasteners in laminates, Comp Struct, vol.94, issue.10, pp.3082-3091, 2012.
URL : https://hal.archives-ouvertes.fr/hal-00759881

M. R. Wisnom, On the high compressive strains achieved in bending tests on unidirectional carbon-fibre/epoxy, Comp Sci Tech, vol.1992, issue.3, pp.229-235

B. Castanié, S. Crézé, J. J. Barrau, F. Lachaud, and L. Risse, Experimental analysis of failures in filled hole compression tests of carbon/epoxy laminate, Comp Struct, vol.92, issue.5, pp.1192-1199, 2010.

J. Serra, J. E. Pierré, J. C. Passieux, J. N. Périé, C. Bouvet et al., Validation and modeling of aeronautical composite structures subjected to combined loadings: The VERTEX project. Part 1: Experimental setup, FE-DIC instrumentation and procedures, Comp Struct, vol.179, pp.224-244, 2017.
URL : https://hal.archives-ouvertes.fr/hal-01617966

J. Serra, J. E. Pierré, J. C. Passieux, J. N. Périé, C. Bouvet et al., Validation and modeling of aeronautical composite structures subjected to combined loadings: The VERTEX project. Part 2: Load envelopes for the assessment of panels with large notches, Comp Struct, vol.180, pp.550-567, 2017.
URL : https://hal.archives-ouvertes.fr/hal-01617966

J. W. Mar and K. Y. Lin, Characterization of Splitting Process in Graphite/Epoxy Composites, J Comp Mat, vol.13, pp.278-287, 1979.

J. G. Goree and J. M. Wolla, Longitudinal splitting in Unidirectional composites, Analysis and Experiments. NASA Contractor Report, vol.3881, 1985.

J. G. Goree and J. M. Wolla, Experimental Evaluation of Longitudinal Splitting in Unidirectional Composites, J Comp Mat, vol.21, pp.49-67, 1987.

S. L. Bazhenov, Longitudinal splitting in unidirectional fibre-reinforced composites with an open hole, Comp Sci Tech, vol.58, issue.1, pp.83-89, 1998.

J. Tan, V. S. Deshpande, and N. A. Fleck, Failure mechanisms of a notched CFRP laminate under multi-axial loading Comp Part A, pp.77-56, 2015.

S. Ramani and D. Williams, Notched and unnotched fatigue behavior of angle ply graphiteepoxy composites, vol.191, 1976.

H. H. Daken and J. W. Mar, Splitting initiation and propagation in notched unidirectional graphite/epoxy composites under tension-tension cyclic loading, Comp Struct, vol.4, issue.2, pp.111-133, 1985.

M. H. Jen and J. Hsu, Residual strength in notched composite materials, Int J Fat, vol.12, pp.267-274, 1990.

S. M. Spearing and P. Beaumont, Fatigue damage mechanics of composite materials. I: Experimental measurement of damage and post-fatigue properties, Comp Sci Tech, vol.44, issue.2, pp.159-168, 1992.

C. Wang and C. Shin, Residual properties of notched [0/90]4s AS4/PEEK of composite laminates after fatigue and re-consolidation, Comp Part B, vol.33, pp.67-76, 2002.

C. S. Shin and C. Wang, A comparison of as-fatigue and re-consolidation residual properties for

, Comp Part A, vol.33, pp.1519-1528, 2002.

S. W. Choi, H. T. Hahn, and P. Shyprykevich, Damage development in notched composite laminates under compression-dominated fatigue, Comp Sci Tech, vol.62, pp.851-860, 2002.

M. Kawai and T. Shiratsuchi, Vanishing notch sensitivity approach to fatigue life prediction of notched cross-ply CFRP laminates at room temperature, J Comp Mat, vol.46, issue.23, pp.2935-2950, 2012.

O. J. Nixon-pearson and S. R. Hallett, An investigation into the damage development and residual strengths of open-hole specimens in fatigue, Comp Part A, vol.69, pp.266-278, 2015.

Y. L. Cui, Mechanics of splitting in orthotropic materials, Int J. Sol Struct, vol.31, issue.15, p.2015, 1994.

M. R. Wisnom and F. K. Chang, Modelling of splitting and delamination in notched cross-ply laminates, Comp Sci Tech, vol.60, issue.15, pp.2849-2856, 2000.

E. V. Iarve, D. Mollenhauer, and R. Kim, Theoretical and experimental investigation of stress redistribution in open hole composite laminates due to damage accumulation, Comp Part A, vol.36, pp.163-171, 2005.

F. P. Van-der-meer and L. J. Sluys, A phantom node formulation with mixed mode cohesive law for splitting in laminates, Int J Fract, vol.158, issue.2, pp.107-124, 2009.

S. R. Hallett, B. G. Green, W. G. Jiang, and M. R. Wisnom, An experimental and numerical investigation into the damage mechanisms in notched composites, Comp Part A, vol.40, pp.613-624, 2009.

V. Achard, C. Bouvet, B. Castanié, and C. Chirol, Discrete ply modelling of open hole tensile tests Comp Struct, pp.369-381, 2014.

M. Q. Le, H. Bainier, D. Néron, C. Ha-minh, and P. Ladevèze, On matrix cracking and splits modeling in laminated composites, Comp Part A, vol.115, pp.294-301, 2018.
URL : https://hal.archives-ouvertes.fr/hal-02275163

J. Lee and C. Soutis, Measuring the notched compressive strength of composite laminates: specimen size effects, Comp Sci Tech, vol.68, pp.2359-2366, 2008.
URL : https://hal.archives-ouvertes.fr/hal-00545285

H. Bao and G. Liu, Progressive failure analysis on scaled open-hole tensile composite laminates, Comp, vol.150, pp.173-180, 2016.

J. Serra, C. Bouvet, B. Castanié, and C. Petiot, Scaling effect in notched composites: The Discrete Ply Model approach, Comp Struct, vol.148, pp.127-143, 2016.
URL : https://hal.archives-ouvertes.fr/hal-02454601

S. Catche, R. Piquet, F. Lachaud, B. Castanie, and A. Benaben, Analysis of hole wall defects of drilled carbon fiber reinforced polymer laminates, J Comp Mat, vol.49, issue.10, pp.1223-1240, 2015.
URL : https://hal.archives-ouvertes.fr/hal-01951221

Y. Yan, W. D. Wen, F. K. Chang, and P. Shyprykevich, Experimental study on clamping effects on the tensile strength of composite plates with a bolt-filled hole, Comp Part A, issue.10, pp.1215-1229, 1999.

, Airbus Patent US20160023425 (A1)

, Failure mode patterns for double lap shear specimens: reference specimens (left) and notched specimens, vol.18

, W=16mm (upper) & W=25mm (lower)