On a general constitutive description for the inelastic and failure behavior of fibrous laminates - Part II: Laminate theory and applications

Computers and Structures

Volumn 80, Issue 13, 2002, Pages 1177-1199

  Huang, Zheng Ming ^a  

^a NATIONAL UNIVERSITY OF SINGAPORE   (Singapore)

Author keywords

Composite structure; Constitutive relationship; Flexural failure; In plane failure; Laminated composite; Load deflection curve; Mechanical property; Metal matrix composite; Stiffness discount; Strength prediction; Textile composite; Thermo mechanical fatigue

Indexed keywords

BENDING STRENGTH; COMPOSITE BEAMS AND GIRDERS; COMPOSITE MICROMECHANICS; COMPUTER SIMULATION; FATIGUE OF MATERIALS; FIBER REINFORCED MATERIALS; FINITE ELEMENT METHOD; LAMINATED COMPOSITES; MATRIX ALGEBRA; METALLIC MATRIX COMPOSITES; RESIDUAL STRESSES; STRAIN; STRESS ANALYSIS; STRUCTURAL ANALYSIS; STRUCTURAL LOADS;

FIBROUS LAMINATES; LAMINATED BRAIDED FABRIC REINFORCED BEAMS;

COMPOSITE STRUCTURES;

EID: 0036563621     PISSN: 00457949     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0045-7949(02)00075-5     Document Type: Article

References (14)

1. On a general constitutive description for the inelastic and failure behavior of fibrous laminates - Part I: Lamina theory
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7. A bridging model prediction of the ultimate strength of composite laminates subjected to biaxial loads
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