1. Schmidt HJ. Damage tolerance technology for current and future aircraft structures. In: Dalle Donne C, editor. Proceedings of the 23rd symposium of the International Committee on Aeronautical Fatigue (ICAF), vol. 1; 2005. p. 1–41.
2. Kocik R, Vugrin T, Seefeld T. Laserstrahlschweissen im Flugzeugbau: Stand und künftige Anwendungen. In: Strahltechnik. BIAS, vol. 28; 2006. p. 15–26.
3. Residual stresses in laser beam welded butt joints of the airframe aluminium alloy AA6056;Staron;Mater Sci Forum,2006
4. Influence of the welding sequence on residual stresses in laser welded T-joints of an airframe aluminium alloy;Machold;Mater Sci Forum,2008
5. Zhang X, Irving P, Edwards L, Fitzpatrick M, Sinclair I, Lin J, et al. The influence of residual stress on design and damage tolerance of welded aircraft structures. In: Dalle Donne C, editor. Proceedings of the 23rd symposium of the International Committee on Aeronautical Fatigue (ICAF), vol. 1; 2005. p. 265–81.