DOI QR코드

DOI QR Code

The Experimental Study on the Absorbed Energy of Carbon/Epoxy Composite Laminated Panel Subjected to High-velocity Impact

고속 충격을 받는 Carbon/Epoxy 복합재 적층판의 흡수 에너지 예측에 대한 실험적 고찰

  • 조현준 (충남대학교 항공우주공학과 대학원) ;
  • 김인걸 (충남대학교 항공우주공학과) ;
  • 이석제 (충남대학교 항공우주공학과 대학원) ;
  • 우경식 (충북대학교 토목공학부) ;
  • 김종헌 (국방과학연구소)
  • Received : 2013.05.13
  • Accepted : 2013.06.09
  • Published : 2013.06.30

Abstract

The evaluation and prediction for the absorbed energy, residual velocity, and impact damage are the key things to characterize the impact behavior of composite laminated panel subjected to high-velocity impact. In this paper, the method to predict the residual velocity and the absorbed energy of Carbon/Epoxy laminated panel subjected to high velocity impact are proposed and examined by using quasi-static perforation test and high-velocity impact test. Total absorbed energy of specimen due to the high-velocity impact can be grouped with static energy and kinetic energy. The static energy are consisted of energy due to the failure of the fiber and matrix and static elastic energy, which are related to the quasi-static perforation energy. The kinetic energy are consisted of kinetic energy of moving part of specimen, which are modelled by three modified kinetic model. The high-velocity impact test were conducted by using air gun impact facility and compared with the predicted values. The damage area of specimen were examined by C-scan image. In the high initial impact velocity above the ballistic limit, both the static energy and the kinetic energy are known to be the major contribution of the total absorbed energy.

Acknowledgement

Supported by : 국방과학연구소

References

  1. Morye, S.S., Hine, P.J., Duckett, R.A., Carr, D.J., and Ward, I.M., "Modelling of the Energy Absorption by Polymer Composites upon Ballistic Impact," Composite Science and Technology, Vol. 60, Issue 14, 2000, pp. 2631-2642. https://doi.org/10.1016/S0266-3538(00)00139-1
  2. Wen, H.M., "Predicting the Penetration and Perforation of FRP Laminates Struck Normally by Projectiles with Different Nose Shapes," Composite Structures, Vol. 18, Issue 3, 2000, pp. 321-329.
  3. You, W.Y., A Study on the High Velocity Impact Behavior of Gr/Ep Composite Laminates Based on Quasi-static Perforation Test, MS. Thesis, Chungnam National University, Korea, 2012.
  4. Sun, C.T., and Potti, S.V., "A Simple Model to Predict Residual Velocities of Thick Composite Laminates Subjected to High Velocity Impact," International Journal of Impact Engineering, Vol. 18, No. 3, 1996, pp. 337-353.
  5. Morye, S., Hine, P.J., Duckett, R.A., Carr, D.J., and Ward, I.M., "A Comparison of the Properties of Hot Compacted gel-spun Polyethylene Fiber Composite with Conventional gel-spun polyethylene Fiber Composite," Composites Part A : Applied Science and Manufacturing, Vol. 30, Issue 5, 1999, pp. 649-660. https://doi.org/10.1016/S1359-835X(98)00175-4
  6. Gama, B.A., and Gillespie, Jr. J.W., "Punch Shear Based Penetration Model of Ballistic Impact of Thick-section Composite," Composite Structures, Vol. 86, Issue 144, 2008, pp. 356-369. https://doi.org/10.1016/j.compstruct.2007.11.001
  7. Mines, R.A.W., Roach, A.M., and Jones, N., "High Velocity Perforation Behaviour of Polymer Composite Laminates," Interna-tional Journal of Impact Engineering, Vol. 22, Issue 6, 1999, pp. 561-588. https://doi.org/10.1016/S0734-743X(99)00019-6
  8. Nailk, N.K., Shrirao, P., and Reddy, B.C.K., "Ballistic Impact Behaviour of Woven Fabric Composites: Formulation," International Journal of Impact Engineering, Vol. 32, Issue 9, 2006, pp. 1521-1552. https://doi.org/10.1016/j.ijimpeng.2005.01.004
  9. Ha, S.C., Cho, S.G., Kim, I.G., Choi, I.H., and Kim, J.H., "Comparison between Static Indentation and Impact Behavior of Composite Laminates," Proceeding of the 2010 KSAS Fall Conference, 2010, pp. 272-276.

Cited by

  1. Ring burst test of filament wound composites for environmental resistance vol.50, pp.18, 2016, https://doi.org/10.1177/0021998315607611