Influence of post-buckling behaviour of composite stiffened panels on the damage criticality

Composite Structures

Volumn 66, Issue 1-4, 2004, Pages 197-206

  Yap, Jeff W H ^a   Thomson, Rodney S ^b   Scott, Murray L ^b   Hachenberg, Dieter ^c  

^a RMIT UNIVERSITY   (Australia)

^b Advanced Composite Structures Ltd ^*  (Australia)

^c AIRBUS OPERATIONS GMBH   (Germany)

Author keywords

Composite stiffened panel; Debonding; Delamination; Finite element analysis; Post buckling; Strain energy release rate

Indexed keywords

BUCKLING; DEFECTS; DELAMINATION; FINITE ELEMENT METHOD; FRACTURE MECHANICS; STIFFNESS; STRAIN;

DAMAGE CRITICALITY; SKIN DELAMINATION;

STRUCTURAL PANELS;

COMPOSITE;

EID: 4143145183     PISSN: 02638223     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.compstruct.2004.04.038     Document Type: Article

References (8)

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