Investigation for the reduction of in-plane compressive strength in preconditioned thin composite panels

Journal of Composite Materials

Volumn 39, Issue 5, 2005, Pages 391-422

  Zhou, G ^a   Rivera, L A ^a  

^a LOUGHBOROUGH UNIVERSITY   (United Kingdom)

Author keywords

Composite panels; Compression after impact; Damage tolerance; Delamination; Global buckling; Local buckling

Indexed keywords

BUCKLING; COMPOSITE STRUCTURES; COMPRESSION TESTING; COMPRESSIVE STRENGTH; DELAMINATION; FAILURE ANALYSIS; GLASS FIBER REINFORCED PLASTICS; LAMINATES; MATHEMATICAL MODELS; STRAIN; STRAIN GAGES; STRUCTURAL LOADS;

COMPOSITE PANELS; COMPRESSION-AFTER-IMPACT; DAMAGE TOLERANCE; GLOBAL BUCKLING; LOCAL BUCKLING; RESIDUAL COMPRESSIVE STRENGTH (RCS);

STRUCTURAL PANELS;

EID: 17544382506     PISSN: 00219983     EISSN: None     Source Type: Journal    
DOI: 10.1177/0021998305047093     Document Type: Article

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