Abstract
In this study, GLARE 5 fiber-metal laminates (FMLs) of dimensions: 254mm25.4mm (10″×1″) with various thicknesses were impacted by a 0.22 caliber bullet shaped projectile using a high-speed gas gun. The specimens were cut transversely through the impact center using a diamond blade cutting wheel for destructive damage evaluation. The results showed that failure pattern was changed as the specimen thickness increased. This was very obvious especially for (5/4) and (6/5) configurations. In addition, a high-speed camera was used to record the damage evolution on the non-impacted side of the specimens. It was found that when impacted ballistically by the same projectile velocity, debonding between the bottom (non-impacted side) aluminum layer and its adjacent glass-fiber reinforced epoxy layer was increased by changing the lay-up configuration from (6/5) to (5/4). This phenomenon was demonstrated experimentally using the video footage obtained from the high-speed camera.
The 3D dynamic nonlinear finite element (FE) code, LS-DYNA, was used to validate the experimental results. To validate the reliability of the model, the finite element results were compared to those data obtained experimentally, namely: the incident versus residual velocity relation, damage patterns and bullet residual lengths. Good agreement between experimental and FE results was achieved.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
References
Vlot A, Gunnink JW (eds) (2001) Fiber metal laminates, an introduction. Kluwer Academic Publishers, Dordrecht
Hoo Fatt MS, Lin C, Revilock DM Jr, Hopkins DA (2003) Ballistic impact of GLARETM fiber-metal laminates. Compos Struct 61:73–88
Goldsmith W, Dharan CKH, Chang H (1995) Quasi-static and ballistic perforation of carbon fiber laminates. Int J Solids Struct 32(1):89–103
Buyuk M, Kan S, Loikkanen MJ (2009) Explicit finite-element analysis of 2024-T3/T351 aluminum material under impact loading for airplane engine containment and fragment shielding. J Aero Eng 22:287–295
Seyed Yaghoubi A, Liaw B (2012) Experimental and numerical approaches on behavior of GLARE 5 Beams: influences of thickness and stacking sequence. In: IMAC XXX A conference and exposition on structural dynamics. Hyatt Regency Jacksonville Riverfront Jacksonville, FL, 30 Jan–2 Feb 2012
Sevkat E, Liaw B, Delale F, Raju BB (2009) A combined experimental and numerical approach to study ballistic impact response of S2-glass fiber/toughened epoxy composite beams. Compos Sci Technol 69(7–8):965–982
Data sheets. Aviation Equipment Structures, Inc., Costa Mesa, CA, 1998
QA Reports B0319B-2, B1008B-1, B0904A-3. Structural Laminates Company, New Kensington, Pennsylvania, 1994
Alloy 7475 Plate and Sheet, ACRP-053-B. Alcoa Mill Products, Bettendorf, Iowa
Lambert JP, Jonas GH (1976) Towards standardization of in terminal ballistics testing: velocity representation. Ballistic Research Laboratories, Aberdeen Proving Ground, Maryland, Report No. BRL-R-1852
Acknowledgments
The authors would like to thank the supports from NASA Faculty Award for Research (FAR) under Grant No. NAG3-2259 and from PSC-CUNY under Grants 63168-00 41 and 64543-00 42. Dr. Kenneth J. Bowles and Dr. John P. Gyekenyesi were the Technical Monitors of the NASA grant. Part of the equipment was procured through ARO Grant No. DAAD19-03-1-0086, of which Dr. Bruce LaMattina was the Program Manager.
Author information
Authors and Affiliations
Corresponding author
Editor information
Editors and Affiliations
Rights and permissions
Copyright information
© 2013 The Society for Experimental Mechanics, Inc.
About this paper
Cite this paper
Yaghoubi, A.S., Liaw, B. (2013). Thickness Effect on Cross-Ply GLARE 5 FML Beams Subjected to Ballistic Impact. In: Ventura, C., Crone, W., Furlong, C. (eds) Experimental and Applied Mechanics, Volume 4. Conference Proceedings of the Society for Experimental Mechanics Series. Springer, New York, NY. https://doi.org/10.1007/978-1-4614-4226-4_45
Download citation
DOI: https://doi.org/10.1007/978-1-4614-4226-4_45
Published:
Publisher Name: Springer, New York, NY
Print ISBN: 978-1-4614-4225-7
Online ISBN: 978-1-4614-4226-4
eBook Packages: EngineeringEngineering (R0)