F. Girot, Perçage des structures aéronautiques : Les résultats du projet MEDOC, 1 er colloque Aquitaine -Québec -Mécanique des Matériaux et des Structures pour l'Aéronautique, 2008.

M. Elajrami, M. Benguediab, and G. Ronald, Effect of various drilling procedures on the fatigue life of rivet holes. Synthèse: Revue des Sciences et de la Technologie, vol.19, pp.67-75, 2008.

D. Sun, P. Lemoine, D. Keys, P. Doyle, S. Malinov et al., Hole-making processes and their impacts on the microstructure and fatigue response of aircraft alloys, The International Journal of Advanced Manufacturing Technology, vol.94, issue.5-8, pp.1719-1726, 2018.

W. C. Ralph, W. S. Jonhson, A. Makeev, C. James, and J. Newman, Fatigue performance of production-quality aircraft fastener holes, International Journal of Fatigue, vol.29, issue.7, pp.1319-1327, 2007.

R. A. Everett, The effect of hole quality on the fatigue life of 2024-T3 aluminum alloy sheet, 2004.

W. C. Ralph, W. S. Johnson, P. Toivonen, A. Makeev, and J. Newman, Effect of various aircraft production drilling procedures on hole quality, International Journal of Fatigue, vol.28, issue.8, pp.943-950, 2006.

A. M. Abdelhafeez, S. L. Soo, D. K. Aspinwall, A. Dowson, and D. Arnold, Burr formation and hole quality when drilling titanium and aluminium alloys, Procedia CIRP, vol.37, pp.230-235, 2015.

R. B. Pereira, L. C. Brandao, A. P. De-paiva, J. R. Ferreira, and J. P. Davim, A review of helical milling process, International Journal of Machine Tools and Manufacture, vol.120, pp.27-48, 2017.

W. Ni, Orbital drilling of aerospace materials. SAE Technical Paper, 2007.

H. Kitagawa and S. Takahashi, Applicability of fracture mechanics to very small cracks or the cracks in the early stage, International Conference on Mechanical Behaviour of Materials, pp.627-631, 1976.

V. K. Choo, P. G. Reinhall, and S. Ghassaei, Effect of high rate deformation induced precipitation hardening on the failure of aluminium rivets, Journal of Materials Science, vol.24, issue.2, pp.599-608, 1989.

M. O. Lai, . T. Oh-j, and . Y. Nee-a, Fatigue properties of holes with residual stresses. Engineering Fracture Mechanics, vol.45, pp.551-557, 1993.

, Federal Aviation Administration. Assessment of residual stresses and hole quality on the fatigue behavior of aircraft structural joints, 2009.