Abstract
A three-dimensional eigenfunction expansion technique, based in part on separation of the thickness variable and partly utilizing a modified Frobenius-type series expansion in conjunction with the Eshelby–Stroh formalism, is used to compute the local stress singularity, in the vicinity of a kinked fibre/matrix trimaterial junction front, representing a measure of the degree of inherent flaw sensitivity of unidirectional carbon-fibre-reinforced composites under compression. Micro-kinking, more prominent in the misaligned regions of carbon fibres, is caused by crystallite disorientations, as detected by the Raman and X-ray measurements, as well as dislocation glide in crystallites and intra/intercrystallite disorders. The present analysis explains the test results relating to propagation of failure from such discontinuities in a unidirectional composite under compression. Numerical results presented include the effect of fibre wedge aperture angle on the strengths of the mode I and mode II singularities. Of special practical interest is the comparison of the inherent flaw sensitivity of carbon/epoxy and glass/epoxy composites, because improvement of the compressive strength and kink toughness was earlier accomplished through commingling of highly anisotropic (and crystalline) carbon and isotropic (and amorphous) glass fibres at the tow level. Compression fracture of these composites can be fully explained and quantified by the present three-dimensional linear elastic stress singularity analysis-based method. Finally, numerical results, pertaining to the through-thickness variation of ‘stress intensity factor’ for symmetric uniform load and its skew-symmetric counterpart that also satisfies the boundary conditions on the top and bottom surfaces of a compressed composite monolayer, in the vicinity of a trimaterial junction front, are also presented.
Acknowledgments
Initial phase of this research was performed under the sponsorship of In-house Research Program (IR) at the NSWC, Carderock Division, and the Office of Naval Research (ONR) through the Navy Laboratory Participation Program (NLPP), and also a grant to the University of Utah. The authors are grateful for helpful guidance received from the program monitors and collaborating Navy scientists – Dr. Yapa Rajapakse of ONR, and Drs. Bruce Douglas, Joseph Corrado, Martin Krenzke and Himatlal Garala, NSWC, Carderock Division. The author also wishes to thank Dr. Minsheng Xie for his help in the initial phase (2D) of computation. Thanks are also due to Professor Fionn Dunne (assoc. editor) and an anonymous reviewer for their suggestions on the previous version of the manuscript, which have contributed to its improvement.