Tensile strength of unidirectional CFRP laminate under high strain rate

  • Published : 2007.06.01

Abstract

The tensile strength of unidirectional carbon fiber reinforced plastics under a high strain rate was experimentally investigated. A high-strain-rate test was performed using the tension-type split Hopkinson bar technique. In order to obtain the tensile stress-strain relations, a special fixture was used for the impact tensile specimen. The experimental results demonstrated that the tensile modulus and strength in the longitudinal direction are independent of the strain rate. In contrast, the tensile properties in the transverse direction and the shear properties increase with the strain rate. Moreover, it was observed that the strain-rate dependence of the shear strength is much stronger than that of the transverse strength. The tensile strength of off-axis specimens was measured using an oblique tab, and the experimental results were compared with the tensile strength predicted based on the Tsai-Hill failure criterion. It was concluded that the tensile strength can be characterized quite well using the above failure criterion under dynamic loading conditions.

Keywords

References

  1. T. Nishiwaki, Designing of CFRP baseball bats, SAMPE Journal 38, 80-82 (2002)
  2. N. Taniguchi, T. Nishiwaki and H. Kawada, Evaluating the mechanical properties of a CFRP tube under a lateral impact load using the split Hopkinson bar, Adv. Compos. Mater. 14, 263-276 (2005) https://doi.org/10.1163/1568551054922601
  3. G. H. Staab and A. Gilat, High strain rate response of angle-ply glass/epoxy laminates, J. Compos. Mater. 29, 1308-1320 (1995) https://doi.org/10.1177/002199839502901003
  4. J. Harding and Y. L. Li, Determination of interlaminar shear strength for glass/epoxy and carbon/epoxy laminates at impact rates of strain, Compos. Sci. Technol. 45, 161-171 (1992) https://doi.org/10.1016/0266-3538(92)90038-5
  5. J. Tsai and C. T. Sun, Dynamic compressive strength of polymeric composites, Int. J. Solids Struct. 41, 3211-3224 (2004) https://doi.org/10.1016/j.ijsolstr.2003.12.010
  6. B.W. Rosen, Mechanics of composite strengthening, in: Fiber Composites Materials. American Society of Metals, Metals Park, OH, pp. 35-75 (1965)
  7. J. Harding and L. M. Welsh, A testing technique for fibre-reinforced composites at impact rates of strain, J. Mater. Sci. 18, 1810-1826 (1983) https://doi.org/10.1007/BF00542078
  8. S. V. Thiruppukuzhi and C. T. Sun, Models for the strain-rate-dependent behavior of polymer composites, Compos. Sci. Technol. 61, 1-12 (2001) https://doi.org/10.1016/S0266-3538(00)00133-0
  9. C. A. Ross, W. H. Cook and L. L. Wilson, Dynamic tensile tests of composite materials using a split-Hopkinson pressure bar, Exper. Technol. 30-33 (1984)
  10. T. Yokoyama, Impact tensile stress-strain characteristics of wrought magnesium alloys, Strain 39, 167-175 (2003) https://doi.org/10.1046/j.1475-1305.2003.00086.x
  11. ASTM D3518
  12. K. F. Graff, Wave Motion in Elastic Solids. Dover Publications, ISBN 0-486-66745-6 (1991)
  13. J. Harding, Effect of strain rate and specimen geometry on the compressive strength of woven glass-reinforced epoxy laminates, Composites 24, 323-332 (1993) https://doi.org/10.1016/0010-4361(93)90042-7
  14. C. T. Sun and S. P. Berreth, A new end tab design for off-axis tension test of composite materials, J. Compos. Mater. 22, 766-779 (1988) https://doi.org/10.1177/002199838802200805
  15. C. T. Sun and I. Chung, An oblique end-tab design for testing off-axis composite specimens, Composites 24, 619-623 (1993) https://doi.org/10.1016/0010-4361(93)90124-Q
  16. F. Pierron and A. Vautrin, The $10^{\circ}$ off-axis tensile test: a critical approach, Compos. Sci. Technol. 56, 483-488 (1996) https://doi.org/10.1016/0266-3538(96)00004-8
  17. F. Pierron, E. Alloba, Y. Surrel and A. Vautrin, Whole-field assessment of the effects of boundary conditions on the strain field in off-axis tensile testing of unidirectional composites, Compos. Sci. Technol. 58, 1939-1947 (1998) https://doi.org/10.1016/S0266-3538(98)00027-X