Further validation of the Jain and Mai models for interlaminar fracture of stitched composites

Abstract Micromechanical models proposed by Jain and Mai to predict the improvement in Modes I and II interlaminar fracture toughness ( G R ) of polymer composites when reinforced by through-thickness stitching have been further validated against a large number of measured G R values. Experimental G R values were obtained from the literature for a variety of carbon- and glass-fibre-reinforced polymer composites stitched over a wide range of densities with different yarn materials (polyester, carbon, glass, Kevlar ® ) of varying thickness. Good agreement was found between the measured and theoretical interlaminar fracture toughness values for both the Modes I and II conditions, despite some major assumptions having to be made about the failure mechanism and mechanical properties of the stitches. An assessment of the experimental Mode II G R data reveals that the commonly used end-notched flexure method is not suitable for the interlaminar fracture toughness testing of stitched composites. It is recommended that Mode II delamination resistance should be measured by using the end-notched cantilever method.

[1]  Adrian P. Mouritz,et al.  A review of the effect of stitching on the in-plane mechanical properties of fibre-reinforced polymer composites , 1997 .

[2]  L. K. Jain,et al.  Analysis of stitched laminated ENF specimens for interlaminar mode II fracture toughness , 1994 .

[3]  L. K. Jain,et al.  Determination of mode II delamination toughness of stitched laminated composites , 1995 .

[4]  Y. Mai,et al.  On the effects of stitching in CFRPs—II. Mode II delamination toughness , 1998 .

[5]  L. K. Jain,et al.  ON THE EFFECT OF STITCHING ON MODE I DELAMINATION TOUGHNESS OF LAMINATED COMPOSITES , 1994 .

[6]  H. Dexter,et al.  Impact resistance and interlaminar fracture toughness of through-the-thickness reinforced graphite/epoxy , 1986 .

[7]  N. Harris,et al.  Multiaxial stitched preform reinforcements , 1992 .

[8]  A. Jackson,et al.  Advanced textile applications for primary aircraft structures , 1992 .

[9]  Paul J. Hogg,et al.  The role of reinforcement architecture on impact damage mechanisms and post-impact compression behaviour , 1996, Journal of Materials Science.

[10]  Gregory M. Glenn,et al.  Fiber-reinforced composites , 1988 .

[11]  S. Sharma,et al.  Effects of stitching on fracture toughness of uniweave textile graphite/epoxy laminates , 1995 .

[12]  S. Sharma,et al.  Effect of Stitching on Impact and Interlaminar Properties of Graphite/Epoxy Laminates , 1997 .

[13]  S. Peters Handbook of Composites , 1998 .

[14]  Yiu-Wing Mai,et al.  Improving the delamination resistance of CFRP by stitching—a review , 1994 .

[15]  Yury Kropp Development of a stitched/RFI composite transport wing , 1995 .

[16]  Kb Su Delamination Resistance of Stitched Thermoplastic Matrix Composite Laminates , 1989 .

[17]  G. Newaz Advances in Thermoplastic Matrix Composite Materials , 1989 .