Author:
Sepe Raffaele,Armentani Enrico,di Lascio Pasquale,Citarella Roberto
Reference20 articles.
1. Fracture mechanics in aircraft failure analysis: Uses and limitations;Wanhill;Eng. Fail. Anal.,2013
2. Numerical investigation on the crack propagation in a flat stiffened panel;Caputo;Key. Eng. Mat.,2006
3. The significance of fatigue crack initiation for predictions of the fatigue limit of specimens and structures;Schijve;Int. J. Fatigue.,2014
4. Residual strength improvement of an aluminium alloy cracked panel;Caputo;The Open Mechanical Engineering Journal.,2013
5. Stochastic improvement of the residual strength of a stiffened panel;Lamanna;Key. Eng. Mat.,2007
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