Spectral stiffness microplane model for quasibrittle composite laminates - Part II: Calibration and validation

Journal of Applied Mechanics, Transactions ASME

Volumn 75, Issue 2, 2008, Pages 0210101-0210106

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

^a Skidmore Owings and Merrill LLP   (United States)

^b Rensselaer Polytechnic Institute   (United States)

^c NORTHWESTERN UNIVERSITY   (United States)

Author keywords

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

Indexed keywords

BIAXIAL TESTING; CHARACTERISTIC LENGTHS; COMPOSITE LAMINATES; CRACK BAND APPROACH; EXPERIMENTAL DATA; FAILURE STRESSES; MICROPLANE MODELS; MULTI DIRECTIONAL LAMINATES; POST PEAK; SOFTENING BEHAVIOR; UNIDIRECTIONAL (UD);

CRACKS; FRACTURE FIXATION; STIFFNESS;

LAMINATES;

EID: 47049111420     PISSN: 00218936     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.2744037     Document Type: Article

References (13)

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