id	author	title	date	pages	extension	mime	words	sentence	flesch	summary	cache	txt
fis-113	Carta, F.; Pirondi, A.	Damage tolerance analysis of aircraft reinforced panels	2013	9	.pdf	application/pdf	3175	139	51	The inclusion of the anti-bending device in the model 04-NB until the second reinforcement leads at a more faithful reproduction of the initial stage of crack propagation. The stress intensity factor trend obtained numerically as a function of crack growth was used to determine the fatigue crack growth rate, obtaining a good approximation of the experimental crack propagation rate in the skin.	cache/fis-113.pdf	txt/fis-113.txt