Spectral stiffness microplane model for quasibrittle composite laminates - Part I: Theory

Journal of Applied Mechanics, Transactions ASME

Volumn 75, Issue 2, 2008, Pages 0210091-0210099

  Cusatis, Gianluca ^a,c   Beghini, Alessandro ^b   Bažant, Zdeněk P ^c  

^a RENSSELAER POLYTECHNIC INSTITUTE   (United States)

^b Owings and Merrill LLP   (United States)

^c NORTHWESTERN UNIVERSITY   (United States)

Author keywords

Crack band model; Damage; Failure criteria; Fiber composites; Finite elements; Fracture energy; Laminates; Microplane model; Spectral methods

Indexed keywords

CHARACTERISTIC LENGTHS; COMPOSITE LAMINATES; DEVIATORIC; FAILURE ENVELOPES; LINEAR STRAINS; MICROPLANE MODELS; MODE COUPLINGS; MULTI DIRECTIONAL LAMINATES; NONLINEARITY (INCLUDING BIFURCATION THEORY); POST PEAK; PRE-PEAK; SPECTRAL DECOMPOSITION; TEST DATA; TRANSVERSELY ISOTROPIC; UNIDIRECTIONAL (UD); UNIDIRECTIONAL (UD) COMPOSITES;

CONSTITUTIVE MODELS; FRACTURE; FRACTURE FIXATION; GEOLOGIC MODELS; IRON; LAMINATES; STIFFNESS; STIFFNESS MATRIX; TEST FACILITIES; TESTING;

PAPER LAMINATES;

EID: 47049109147     PISSN: 00218936     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.2744036     Document Type: Article

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