On the behaviour of the residual strain produced by matrix cracking in cross-ply laminates

Author:

Bassam F.,Boniface L.,Jones K.,Ogin S.L.

Publisher

Elsevier BV

Subject

Mechanics of Materials,Ceramics and Composites

Reference18 articles.

1. Curing stresses in composite laminates;Hahn;J. Compos. Mater.,1975

2. Bowles, D.E. and Shen, J., Thermal cycling effects on the dimensional stability of P75 and P75-T300 (fabric) hybrid graphite/epoxy laminates. In Proc. 33rd International SAMPE Symp., 1988, p. 1659.

3. Bassam, F., Boniface, L. and Ogin, S.L., Residual strain as a damage parameter for crossply laminates. In Proc. of the Second International Seminar on Experimental Techniques and Design in Composite Materials, Sheffield, UK, September 1994.

4. Highsmith, A.L. and Reifsnider, K.L., Stiffness reduction mechanisms in composites, ASTM STP 775, ed. K. Reifsnider. American Society for Testing and Materials, Philadelphia, 1982, p. 103.

5. Poisson's ratio as a damage parameter in the static tensile loading of simple crossply laminates;Smith;Compos. Sci. Technol.,1990

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