Skip to main content
Log in

Blast Resistance and Damage Modelling of Fibre Metal Laminates to Blast Loads

  • Published:
Applied Composite Materials Aims and scope Submit manuscript

Abstract

A robust and efficient computational model has been developed which is capable of modelling the dynamic non-linear behaviour of GLARE panels subjected to blast loadings. Numerical model validation have been performed considering case studies of GLARE panels subjected to a blast-type pressure pulse for which experimental data on the back-face deflection and post-damage observations were available. Excellent agreement of mid-point deflections and evidence of severe yield line deformation were shown and discussed against the performed blast tests. A further parametric study identified GLARE as a potential blast attenuating structure, exhibiting superior blast potential against monolithic aluminium plates. It was concluded that further work needed to be carried out to take into account the influence of geometry (cylindrical structures), pre-pressurisation effects and boundary conditions

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.

Fig. 1
Fig. 2
Fig. 3
Fig. 4
Fig. 5
Fig. 6
Fig. 7
Fig. 8
Fig. 9
Fig. 10
Fig. 11
Fig. 12
Fig. 13
Fig. 14

Similar content being viewed by others

References

  1. Soutis, C.: Recent advances in building with composites. Plast. Rubber Compos. 9(10), 359 (2009)

    Article  Google Scholar 

  2. Vlot, A., Gunnink, J.: Fibre Metal Laminates: An Introduction. Springer, New York (2001)

    Book  Google Scholar 

  3. Vlot, A.: Impact loading on fibre metal laminates. Int. J. Impact Eng. 18(3), 291 (1996)

    Article  Google Scholar 

  4. Vlot, A., Kroon, E., La Rocca, G.: Impact response of fiber metal laminates. Key Eng. Mater. 141, 235 (1997)

    Article  Google Scholar 

  5. Fatt, H., Lin, C., Revilock, D., Hopkins, D.: Ballistic impact of GLARE fiber-metal laminates. Compos. Struct. 61(1), 73 (2003)

    Article  Google Scholar 

  6. McCarthy, M., Xiao, J., Petrinic, N., Kamoulakos, A., Melito, V.: Modelling of bird strike on an aircraft wing leading edge made from fibre metal laminates—part 1: material modelling. Appl. Compos. Mater. 11(5), 295 (2004)

    Article  CAS  Google Scholar 

  7. Fleisher, H.J.: Design and explosive testing of a blast resistant luggage container. In: Proc. Structures Under Shock and Impact Conference IV, pp. 51–59 (1996)

  8. Langdon, G.S., Chi, Y., Nurick, G.N., Haupt, P.: Response of GLARE© panels to blast loading. Eng. Struct. 31, 3116 (2009)

    Article  Google Scholar 

  9. Karagiozova, D., Langdon, G.S., Nurick, G.N., Chung, K.Y.: Simulation of the response of fibre-metal laminates to localised blast loading. Int. J. Impact Eng. 37(6), 766 (2010)

    Article  Google Scholar 

  10. Langdon, G., Lemanski, S., Nurick, G., Simmons, M., Cantwell, W., Schleyer, G.: Behaviour of fibre-metal laminates subjected to localised blast loading: part I—experimental observations. Int. J. Impact Eng. 34(7), 1202 (2007)

    Article  Google Scholar 

  11. ABAQUS 6.10 Users Manual, Dassault Systemes Simulia Corp, Providence, RI. (2010)

  12. Hoo Fatt, M.S., Palla, L.: Analytical modeling of composite sandwich panels under blast loads. J. Sandw. Struct. Mater. 11(4), 357 (2009)

    Article  Google Scholar 

  13. Vlot, A.: High Strain Rate Tests on Fibre Metal Laminates, Series 07. Tech. rep., Delft University Press, The Netherlands (1998)

  14. Hagenbeek, M.: Characterisation of fibre metal laminates under thermo-mechanical loadings. Ph.D. thesis, Delft University of Technology, Delft, The Netherlands (2005)

  15. Linde, P., de Boer, H.: Modelling of inter–rivet buckling of hybrid composites. Compos. Struct. 73(2), 221 (2006)

    Article  Google Scholar 

  16. Hashin, Z.: Failure criteria for unidirectional fiber composites. J. Appl. Mech. 47, 329 (1980)

    Article  Google Scholar 

  17. Kashtalyan, M., Soutis, C.: Analysis of composite laminates with intra-and interlaminar damage. Prog. Aerosp. Sci. 41(2), 152 (2005)

    Article  Google Scholar 

  18. Kashtalyan, M., Soutis, C.: Mechanisms of internal damage and their effect on the behavior and properties of cross-ply composite laminates. Int. Appl. Mech. 38(6), 641 (2002)

    Article  Google Scholar 

  19. Soutis, C., Beaumont, P., Ebrary, Inc.: Multi-Scale Modelling of Composite Material Systems: The Art of Predictive Damage Modelling. Woodhead, Cambridge (2005)

  20. Lapczyk, I., Hurtado, J.: Progressive damage modeling in fiber-reinforced materials. Compos., Part A Appl. Sci. Manuf. 38(11), 2333 (2007)

    Article  Google Scholar 

  21. Johnson, G., Cook, W.: A constitutive model and data for metals subjected to large strains, high strain rates and high temperatures. In: Proceedings of the 7th International Symposium on Ballistics, pp. 541–547. The Hague, Netherlands (1983)

  22. Ravichandran, G., Rosakis, A., Hodowany, J., Rosakis, P.: On the Conversion of Plastic Work into Heat During High-Strain-Rate Deformation. American Institute of Physics, New York (2002)

    Google Scholar 

  23. Buyuk, M., Kan, S., Loikkanen, M.J.: Explicit finite-element analysis of 2024-T3/T351 aluminum material under impact loading for airplane engine containment and fragment shielding. J. Aerosp. Eng. 22(3), 287 (2009)

    Article  Google Scholar 

Download references

Author information

Authors and Affiliations

Authors

Corresponding author

Correspondence to Galal F. A. Mohamed.

Rights and permissions

Reprints and permissions

About this article

Cite this article

Mohamed, G.F.A., Soutis, C. & Hodzic, A. Blast Resistance and Damage Modelling of Fibre Metal Laminates to Blast Loads. Appl Compos Mater 19, 619–636 (2012). https://doi.org/10.1007/s10443-011-9225-8

Download citation

  • Received:

  • Accepted:

  • Published:

  • Issue Date:

  • DOI: https://doi.org/10.1007/s10443-011-9225-8

Keywords

Navigation