The Influence of Matrix Fracture Strain and Interface Strength on Cross-Ply Cracking in CFRP in the Temperature Range of -100°C to +100°C
- 1 September 1989
- journal article
- Published by SAGE Publications in Journal of Composite Materials
- Vol. 23 (9) , 944-960
- https://doi.org/10.1177/002199838902300905
Abstract
Cross-ply cracking in specimens out of the laminate 0/904/0 was in vestigated at -100°C, -40°C, RT, 60° and 100°C. The thermal strain in the transverse ply at these temperatures was determined with the thermal expansion coefficients in fibre direction and transverse to the fibre of a unidirectional laminate. These thermal expansion coefficients were found to vary approximately linearly with the temperature. Multiple fracture of the 90°-ply of 0/904/0 specimens was registered with the aid of a piezo-electric transducer in connection with a computer during a displacement-controlled quasi-static tensile test. The 904-ply is divided in a number of elements N all of which can break. The registered crack data ( n cracks, n < N, with their respective fracture strains) can be described by two-parameter Weibull distributions of the fracture strain ( = thermal plus mechanical strain). From the Weibull distributions and an available model for the transverse fracture strain distribution it was found that at increasing test temperature two phenomena influence the transverse fracture strain. These are the fracture strain (and duc tility) of the matrix and the strength of the interface, which at increasing temperature im proves and reduces the transverse fracture strains respectively. First ply failure proved to be dominated by the increasing fracture strain of the matrix from -100°C to RT. Above RT, however, the influence of the decrease in interface strength dominates over the in fluence of the increased matrix fracture strain.Keywords
This publication has 10 references indexed in Scilit:
- Effects of Cure and Sizing on Fiber-Matrix Bond StrengthJournal of Composite Materials, 1987
- On cross-ply cracking in glass and carbon fibre-reinforced epoxy laminatesComposites, 1987
- Constrained 90-Deg Ply Cracking in 0/90/0 and ±45/90/∓45 CFRP LaminatesPublished by ASTM International ,1986
- The Strength Distribution of 90° Plies in 0/90/0 Graphite-Epoxy LaminatesJournal of Composite Materials, 1984
- Statistical analysis of multiple fracture in 0 /90 /0 glass fibre/epoxy resin laminatesJournal of Materials Science, 1983
- Experimental Determination of the In Situ Transverse Lamina Strength in Graphite/Epoxy LaminatesJournal of Composite Materials, 1982
- The Dependence of Transverse Cracking and Delamination on Ply Thickness in Graphite/Epoxy LaminatesPublished by ASTM International ,1982
- Constrained cracking in glass fibre-reinforced epoxy cross-ply laminatesJournal of Materials Science, 1978
- Curing Stresses in Composite LaminatesJournal of Composite Materials, 1975
- Tensile failure of fibrous compositesAIAA Journal, 1964