Fiber-Matrix Adhesion and Its Effect on Composite Mechanical Properties: IV. Mode I and Mode II Fracture Toughness of Graphite/Epoxy Composites
- 27 July 1992
- journal article
- research article
- Published by SAGE Publications in Journal of Composite Materials
- Vol. 26 (7), 936-968
- https://doi.org/10.1177/002199839202600701
Abstract
To optimize the level of fiber-matrix adhesion an understanding of the relationship between fiber-matrix interfacial bond strength and the mechanical and frac ture behavior of composites is essential. This study establishes the relationship between fiber-matrix interfacial shear strength (ISS) and interlaminar fracture toughness (both Mode I and Mode II) and failure modes for graphite/epoxy composites. A well defined and characterized graphite fiber/epoxy system was chosen in which the level of adhesion be tween fiber and matrix was changed by using the same graphite fibers with different sur face treatments. These surface treatments changed the level of adhesion between the fiber and matrix thus resulting in an increase of the fiber-matrix ISS by over a factor of two while the fiber and matrix properties remained unchanged. The Mode I and Mode II tests were conducted by the double cantilever beam (DCB) and end-notch flexure (ENF) tests methods, respectively. The Mode I fracture toughness (GIC) of composites having low fiber-matrix ISS could not be determined from the DCB test because of extensive fiber bridging and crack meandering. For the composites having higher values of the ISS, the GIC increased with the ISS. The experimental results demonstrated that there is a strong dependency of Mode II fracture toughness (GIIC) on fiber-matrix adhesion. Increased fiber-matrix adhesion in one group of composites significantly improved the GIIC , but the presence of brittle interphase around graphite fibers in another group of composites tended to cancel part of the improvement resulting from increased adhesion. Based on the major failure modes occurring during the Mode I and Mode II loading conditions, a causal link age between fiber-matrix adhesion and interlaminar fracture behavior of graphite/epoxy composites is established.Keywords
This publication has 34 references indexed in Scilit:
- Delamination Crack Growth in Unidirectional Fiber-Reinforced Composites under Static and Cyclic LoadingPublished by ASTM International ,2009
- Interlaminar fracture toughness and toughening of laminated composite materials: a reviewComposites, 1989
- Strength and toughness of fibre compositesComposites Science and Technology, 1988
- An assessment of the impact performance of CFRP reinforced with high-strain carbon fibresComposites Science and Technology, 1986
- The characterization of Mode I delamination failure in non-woven, multidirectional laminatesComposites, 1984
- Fracture Mechanics for Delamination Problems in Composite MaterialsJournal of Composite Materials, 1983
- Effect of Resin on Impact Damage Tolerance of Graphite/Epoxy LaminatesPublished by ASTM International ,1982
- Fracture toughness of graphite/epoxy laminatesComposites, 1980
- The interlaminar fracture of organic-matrix, woven reinforcement compositesComposites, 1980
- Carbon fibre composites with rubber toughened matricesJournal of Materials Science, 1975