Simplified braiding through integration points model for triaxially braided composites

Journal of Aerospace Engineering

Volumn 21, Issue 3, 2008, Pages 152-161

  Cheng, Jingyun ^a   Binienda, Wieslaw K ^a  

^a University of Akron   (United States)

Author keywords

Composite materials; Deformation; Finite element method; Plates; Polymers

Indexed keywords

ARBITRARY LAGRANGIAN EULERIAN (ALE) FORMULATIONS; BALLISTIC IMPACTS; BRAIDED COMPOSITES; COMPOSITE PLATES; EQUATION OF STATE (EOS); FINITE ELEMENT ANALYSIS (FEA); INTEGRATION POINTS; LARGE DEFORMATIONS; LS-DYNA; NUMERICAL MODELLING; NUMERICAL PROBLEMS; SHELL ELEMENTS; TWO-DIMENSIONAL (2D);

BALLISTICS; CARBON FIBER REINFORCED PLASTICS; COMPOSITE MATERIALS; COMPUTATIONAL EFFICIENCY; COMPUTATIONAL METHODS; DEFORMATION; EQUATIONS OF STATE; FIBER OPTICS; FORMING; INTEGRATION; MATHEMATICAL MODELS; MODAL ANALYSIS; NONLINEAR ANALYSIS; NUMERICAL METHODS; PREFORMING; PROJECTILES; TWO DIMENSIONAL;

FINITE ELEMENT METHOD;

EID: 45749117590     PISSN: 08931321     EISSN: None     Source Type: Journal    
DOI: 10.1061/(ASCE)0893-1321(2008)21:3(152)     Document Type: Article

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