Experimental and numerical studies on adhesively bonded CFRP laminates with closed debonds

Composite Structures

Volumn 95, Issue , 2013, Pages 598-606

  Senthil, K ^a   Arockiarajan, A ^b   Palaninathan, R ^b   Santhosh, B ^a   Usha, K M ^a  

^a INDIAN SPACE RESEARCH ORGANISATION   (India)

^b INDIAN INSTITUTE OF TECHNOLOGY MADRAS   (India)

Author keywords

Adhesive joints; Buckling; Debond; Finite element analysis (FEA); Laminates

Indexed keywords

BUCKLING LOADS; CARBON/EPOXY LAMINATES; CFRP LAMINATE; COMPOSITE LAMINATE; DEBOND; DEBONDS; EXPERIMENTAL STUDIES; FIBRE REINFORCED; FINITE ELEMENT PACKAGES; FREE BOUNDARY CONDITIONS; LOAD BEARING CAPABILITIES; LOAD-BEARING CAPACITY; MSC/NASTRAN; NUMERICAL STUDIES;

ADHESIVE JOINTS; BUCKLING; CARBON FIBERS; FINITE ELEMENT METHOD; FUNCTIONALLY GRADED MATERIALS; LAMINATES;

LOADING;

EID: 84868159568     PISSN: 02638223     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.compstruct.2012.08.007     Document Type: Article

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