Modelling of fibre metal laminate shells applied to the inter rivet buckling phenomenon

ECCOMAS 2004 - European Congress on Computational Methods in Applied Sciences and Engineering

Volumn , Issue , 2004, Pages

  Preusch, K ^a   Linde, P ^a   Pleitner, J ^a   De Boer, H ^b   Carmone, C ^c  

^a AIRBUS OPERATIONS GMBH   (Germany)

^b Advanced Lightweight Engineering   (Netherlands)

^c Bishop GmbH Aeronautical Engineers   (Germany)

Author keywords

Damage; Experimental verification; Failure criterion; Fibre metal laminate (FML); Inter rivet buckling; Plasticity

Indexed keywords

ADVANCED COMPOSITE MATERIALS; ALTERNATING LAYERS; DAMAGE; EXPERIMENTAL VERIFICATION; FAILURE CRITERIA; FATIGUE CHARACTERISTICS; FIBRE METAL LAMINATES; GLASS FIBRE REINFORCED;

BUCKLING; COMPUTATIONAL METHODS; FIRE RESISTANCE; PLASTICITY; RIVETS;

FIBERS;

EID: 84893501937     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (12)

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