id	author	title	date	pages	extension	mime	words	sentence	flesch	summary	cache	txt
fis-1451	Telichev, Igor	Development of an engineering methodology for non-linear fracture analysis of impact-damaged pressurized spacecraft structures	2015	11	.pdf	application/pdf	4526	237	64	The traction-free link L0 corresponds to the hole, links L1 and L3 are radial cracks and links L2 and L4 represent the plastic zones. [1] <599 1041 Present approach 590 1082 Deviation,% N/A 3.4 Table 1: Critical crack length (specimen: 2219-T87, ts=3.17 mm) CONCLUSIONS he present paper is focused on the engineering methodology which is viewed as a key element in the spacecraft design procedure providing that under no circumstances will the “unzipping” occur.	cache/fis-1451.pdf	txt/fis-1451.txt