Skip to main content
Log in

Impact energy absorption mechanism of largely deformable composites with different reinforcing structures

  • Published:
Fibers and Polymers Aims and scope Submit manuscript

Abstract

Impact behaviors of the large deformable composites of Kevlar fiber reinforced composites of different preform structures have been investigated. An analytic tool was developed to characterize the impact behavior of the Kevlar composites. The image analysis technique, and deply technique were employed to develop energy balance equation under impact loading. An energy method was employed to establish the impact energy absorption mechanism of Kevlar multiaxial warp knitted composites. The total impact energy was classified into four categories including delamination energy, membrane energy, bending energy and rebounding energy under low velocity impact. Membrane and bending energy were calculated from the image analysis of the deformed shape of impacted specimen and delamination energy was calculated using the deplying technique. Also, the impact behavior of Kevlar composites under high velocity impact of full penetration of the composite specimen was studied. The energy absorption mechanisms under high velocity impact were modelled and the absorbed energy was classified into global deformation energy, shear-out energy, deformation energy and fiber breakage energy. The total energy obtained from the model corresponded reasonably well with the experimental results.

This is a preview of subscription content, log in via an institution to check access.

Access this article

Price excludes VAT (USA)
Tax calculation will be finalised during checkout.

Instant access to the full article PDF.

Similar content being viewed by others

References

  1. F. Scardino, “Comp. Mat. Series”, (R. Pipes Ed.)s, Vol. 6, pp. 22–24, Elsevier, NY, 1989.

    Google Scholar 

  2. A. Kinsey, D. E. Saunders, and C. Soutis,Composites,26, 661 (1995).

    Article  CAS  Google Scholar 

  3. G. Clark,Composites,20, 209 (1989).

    Article  CAS  Google Scholar 

  4. D. Delfosse and A. Poursartip,Composites,28A, 647 (1997).

    CAS  Google Scholar 

  5. C. C. Jr. Poe, “Simulated impact damage in a thick graphite/epoxy laminate using spherical indenters”, NASA TM-100539, NASA Langley Research, Center, VA, 1988.

  6. C. T. Sun and J. E. Grady,Composite Science and Technology,31, 55 (1988).

    Article  CAS  Google Scholar 

  7. S. Abrate,Applied Mechanics Reviews,44(4), 155–190 (1991).

    Article  Google Scholar 

  8. W. J. Cantwell and J. Morton,Composites,22(5), 347 (1991).

    Article  CAS  Google Scholar 

  9. R. Ayres, E. G. Brewer, and S. W. Holland,Transactions SAE,88, 2630 (1979).

    Google Scholar 

  10. A. Miyoshi, A. Yoshioka, and G. Yagawa,Engineerings with Computers,3, 149 (1988).

    Article  Google Scholar 

  11. J. H. Vogel and D. Lee,Journal of Materials Shaping Technology,6, 205 (1989).

    Article  Google Scholar 

  12. E. G. Gyunn and T. K. Obrien, “Proc. 26th Structures, Structural Dynamics, Material Conf.”, Orlando, FL, April, 187 (1985).

  13. G. Zhu, W. Goldsmith, and C. Dharan,Int. J. Solids Structures,29, 399 (1992).

    Article  Google Scholar 

Download references

Author information

Authors and Affiliations

Authors

Corresponding author

Correspondence to Tae Jin Kang.

Rights and permissions

Reprints and permissions

About this article

Cite this article

Kang, T.J., Kim, C. Impact energy absorption mechanism of largely deformable composites with different reinforcing structures. Fibers Polym 1, 45–54 (2000). https://doi.org/10.1007/BF02874876

Download citation

  • Received:

  • Accepted:

  • Issue Date:

  • DOI: https://doi.org/10.1007/BF02874876

Keywords

Navigation