PSI - Issue 2_B

F.Sacchetti et al. / Procedia Structural Integrity 2 (2016) 245–252 251 F.Sacchetti, W.J.B. Grouve, L.L. Warnet, I. Fernandez Villegas/ Structural Integrity Procedia 00 (2016) 000 – 000 7

Figure 8: Micrograph of the surface after peeling in which the crack propagation is from left to right as shown in the arrow. The beach marks are clearly visible as light and dark bands. Right) 10x magnification. Left) A magnified view of the encircled area.

4. Conclusion

The feasibility of the mandrel peel test to characterize the fracture toughness of woven fabric reinforced thermoplastic composites was studied by comparing it to the standardized DCB test. The mandrel peel test can be considered to be an easy and fast test compared to the DCB test. Both testing techniques yielded similar fracture toughness values and have shown similar stick slip behavior. However, the mandrel used in the peel test limited the unstable crack propagation distance. Consequently, a single mandrel peel test has produced more than 20 times the amount of data points per unit crack length than the DCB test. Hence, the mandrel peel test can be considered to be more statistically relevant than DCB test. Nevertheless, this is in contradiction with the slightly higher standard deviation observed in the mandrel peel test with respect to the DBC test. The mandrel peel test seems to be a good alternative to the DCB test for woven fabric reinforced composites. However, further research is required to understand the effect of mode mixity, internal stresses in the sample, and test parameters on the measured results of the mandrel peel test.

Acknowledgements

This project is funded by and performed at the Thermoplastic Composites Research Center (TPRC). The support of the Region Twente and the Gelderland & Overijssel team for the TPRC, by means of the GO Programme EFRO 2007-2015, is gratefully acknowledged.

References

ISO 15024 International standard, 2001. Fibre-reinforced plastic Composites — Determination of mode-I interlaminar fracture toughness, GIC, for unidirectionally reinforced materials. ASMT D 5528, 2001. Standard Test Method for Mode I Interlaminar Fracture Toughness of Unidirectional Fiber-Reinforced Polymer Matrix Composites. De Baere et al., 2012. Study of the Mode I and Mode II Interlaminar Behavior of Carbon Fabric Reinforced Thermoplastic. Polymer Testing 31:322-33. Alif et al., 1998. The effect of weave pattern and crack propagation direction on mode I delamination resistance of woven glass and carbon composites. Composites Part B 29(5):603-611. Gill et al. , 2009. Effect of variation in fibre volume fraction on modes I and II delamination behaviour of 5HS woven composites manufactured by RTM. Composites Science & Technlogy 69(14):2368-23-75. P. Compston and P.-Y. B. Jar, 1998. Comparison of Interlaminar Fracture Toughness in Unidirectional and Woven Roving Marine, Composites, Applied Composite Materials 5:189 – 206. T. W. Webb and E. C. Aifantis, 1997. Crack growth resistance curves and stick-slip fracture inestabilities, Mechanics Research Communications, Vol. 24, No. 2, pp. 123-130. T.W.Webb and E. C. Aifantis, 1995. Stick- Slip Instabilities in Fracture, Computational Mechanics pp 1353-1358, D. Maugis and M. Barquins, 1988. Stick-Slip and peeling of adhesive tapes, Adhesion 12, edited by K. Allen (Elsevier ASP, London,), pp. 205 – 222. Matteo Ciccottia, Bruno Giorgini, Michel Barquins, February 1998. Stick-slip in the peeling of an adhesive tape: evolution of theoretical model, International Journal of Adhesion and Adhesives, Volume 18, Issue 1, Pages 35 – 40.

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