Residual strength analysis using CTOA criteria for fuselage structures containing multiple site damage

Engineering Fracture Mechanics

Volumn 70, Issue 3-4, 2003, Pages 525-545

  Hsu, Ching Long ^a   Lo, James ^a   Yu, Jin ^a   Lee, Xiao Gong ^b   Tan, Paul ^b  

^a BOEING COMPANY   (United States)

^b FAA Wm J Hughes Technical Center   (United States)

Author keywords

CTOA; Damage tolerance; Fuselage structure; Residual strength

Indexed keywords

COMPUTER SIMULATION; FINITE ELEMENT METHOD; FUSELAGES; LOADS (FORCES); RESIDUAL STRESSES;

MULTIPLE SITE DAMAGE (MSD);

CRACKS;

AIRCRAFT; DAMAGE; RESIDUAL STRENGTH;

EID: 0037290760     PISSN: 00137944     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0013-7944(02)00135-2     Document Type: Article

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