Minimising Damage And Delaying Failure Of Composite Laminates

Advanced Polymer Composites for Structural Applications in Construction: ACIC 2004

Volumn , Issue , 2004, Pages 517-524

  McCartney, L N ^a  

^a NATIONAL PHYSICAL LABORATORY   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

BRIDGES; CARBON; CARBON FIBERS; CONSTRUCTION INDUSTRY; LAMINATED COMPOSITES; PAPER LAMINATES; SAFETY ENGINEERING; STRESS ANALYSIS;

BRIDGE STRENGTHENING; CARBON FIBRE COMPOSITES; COMPOSITE LAMINATE; ENERGY BASED APPROACH; ENGINEERING COMPONENTS; ENVIRONMENTAL EXPOSURE; SYMMETRIC LAMINATES; THERMAL RESIDUAL STRESS;

LAMINATES;

EID: 84942240762     PISSN: None     EISSN: None     Source Type: Book    
DOI: 10.1016/B978-1-85573-736-5.50058-3     Document Type: Chapter

References (5)

1. Soden P D, Hinton M J, Kaddour A S 'Lamina properties, lay-up configurations and loading conditions for a range of fibre reinforced composite laminates'. Comp. Sci. Tech 1998, 58:1011-1022. and other papers in the same special issue. Part B of the exercise is published in Comp. Sci. Tech. 2002 62, 1479-1797.
2. L N McCartney, 'Physically based damage models for laminated composites', Proc. Instn. Mech. Engrs. 2003, 217, Part L: J. Materials: Design & Applications, 163-199.
3. Johnson P, Chang F-K 'Characterisation of matrix crack induced laminate failure - Part I: Experiments'. J. Comp. Mater 2001, 35:2009-2035. Part II: Analysis and verifications, 35, 2037-2073.
4. McCartney L N 'Model to predict effects of triaxial loading on ply cracking in general symmetric laminates'. Comp. Sci. Tech 2000, 60:2255-2279. (see Errata in Comp. Sci. Tech. 2002, 62, 1273-1274).
5. Software system 'PREDICT' which is a specific module of CoDA. http://www.npl.co.uk/npl/cmmt/cog/coda.html.