The analysis of skin-to-stiffener debonding in composite aerospace structures

Composite Structures

Volumn 57, Issue 1-4, 2002, Pages 425-435

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

^a RMIT UNIVERSITY   (Australia)

^b Advanced Composite Structures Limited ^*  (Australia)

^c AIRBUS OPERATIONS GMBH   (Germany)

Author keywords

Composite stiffened panel; Debonding; Finite element analysis; Postbuckling; Strain energy release rate

Indexed keywords

AEROSPACE APPLICATIONS; CRACK PROPAGATION; DEBONDING;

FINITE ELEMENT (FE);

COMPOSITE STRUCTURES;

AEROSPACE TEXTILE; BUCKLING; DEBONDING; HIGH PERFORMANCE; INDUSTRIAL USE;

EID: 0036659335     PISSN: 02638223     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0263-8223(02)00110-1     Document Type: Article

References (13)

1. Stringer peeling effects at stiffened composite panels in the postbuckling range
2. Durability of postbuckling fibre composite shear panels
3. Postbuckling failure analysis of carbon/epoxy compression panel
4. Postbuckling and failure of stiffened composite plates
5. Postbuckling failure of carbon-epoxy compression panels