Failure analysis in postbuckled composite T-sections

Composite Structures

Volumn 86, Issue 1-3, 2008, Pages 146-153

  Orifici, A C ^a,b   Shah, S A ^a   Herszberg, I ^b   Kotler, A ^c   Weller, T ^c  

^a RMIT UNIVERSITY   (Australia)

^b Cooperative Research Centre for Advanced Composite Structures ^*  (Australia)

^c TECHNION ISRAEL INSTITUTE OF TECHNOLOGY   (Israel)

Author keywords

Buckling; COCOMAT; Postbuckling; Skin stiffener damage; Stiffened panels

Indexed keywords

BEAMS AND GIRDERS; COMPOSITE STRUCTURES; DEFORMATION; FAILURE ANALYSIS; FINITE DIFFERENCE METHOD; FINITE ELEMENT METHOD; FORECASTING; INTERFACES (MATERIALS); LOADING; LOADS (FORCES); NUMERICAL ANALYSIS; PIGMENTS; RELIABILITY; SAFETY FACTOR; SKIN; STRENGTH OF MATERIALS; STRUCTURAL DESIGN; TWO DIMENSIONAL;

(N-1) CRITERION; (R ,S)-SYMMETRIC; ANALYSIS APPROACH; COHESIVE ELEMENTS; CRITICAL DAMAGE; EFFICIENT ANALYSIS; ELSEVIER (CO); EXPERIMENTAL RESULTS; FAILURE LOADS; FINITE ELEMENT (FE) MODELING; GLOBAL LOCAL; HIGHLY EFFICIENT; IN ORDER; INITIATION (ELECTRIC DISCHARGES); NUMERICAL PREDICTIONS; POST-BUCKLING; STIFFENED PANELS; STRENGTH (IGC: D5/D6); TWO-DIMENSIONAL (2-D) MODELING;

QUALITY ASSURANCE;

BUCKLING; DEFORMATION; FAILURE ANALYSIS; FINITE ELEMENT ANALYSIS;

EID: 46749135156     PISSN: 02638223     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.compstruct.2008.03.022     Document Type: Article

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