journal article·2009-06

A combined experimental and numerical approach to study ballistic impact response of S2-glass fiber/toughened epoxy composite beams

Ercan Sevkat, Benjamin Liaw, Feridun Delale, Basavaraju B. Raju

Composites Science and Technology· Volume 69· Issue 7-8
Publisher page

Abstract

Abstract A combined experimental and 3D dynamic nonlinear finite element (FE) approach was adopted to study damage in composite beams subject to ballistic impact using a high-speed gas gun. The time-histories of dynamic strains induced during impact were recorded using strain gages mounted on the front of the composite beam specimen. During ballistic impact tests, the impact velocity was also measured. The commercially available 3D dynamic nonlinear FE code, LS-DYNA, modified with a proposed user-defined nonlinear-orthotropic damage model, was then used to simulate the experimental results. In addition, LS-DYNA with the Chang–Chang linear-orthotropic damage model was also used for comparison. Good agreement between experimental and FE results was found from the comparisons of dynamic strain and damage patterns. Once the proposed nonlinear-orthotropic damage model was verified by experimental results, further FE simulations were conducted to predict the ballistic limit velocity (V50) using either the number of damaged layer approach or a numerically established relation between the projectile impact velocity versus residual velocity or energy similar to the classical Lambert–Jonas equation for metals.
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Research context

OpenAlex topics: High-Velocity Impact and Material Behavior · Mechanical Behavior of Composites · Structural Response to Dynamic Loads

SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.

References (34)

Show source-provided references
1. Knoell · 1975 · vol. 7
2. Skudra · 1991
3. Karal M. AST Composite Wing Program – Executive Summary. NASA CR 2001-210650; 2001.
4. A three-dimensional modeling of the dynamic behavior of composite rotors10.1155/S1023621X02000179 ↗
5. Wang K. Vibration analysis of cracked composite bending-torsion beams for damage diagnosis. PhD dissertation, Virginia Polytechnic Institute and State University, Blacksburg, VA; 2004.
6. The mechanics of Z-fiber reinforcement10.1016/S0263-8223(96)00053-0 ↗
7. Dow MB, Dexter HB. Development of stitched, braided and woven composite structures in the ACT program and at Langley Research Center (1985–1997) – Summary and Bibliography. NASA/TP-97-206234; 1997.
8. Investigation of mechanical behavior of transverse stitched T-joints with PR520 resin in flexure and tension10.1016/S0263-8223(01)00023-X ↗
9. Damping analysis of composite materials and structures10.1016/j.compstruct.2007.10.024 ↗
10. Longitudinal and transverse damping of unidirectional fibre composites10.1016/j.compstruct.2006.02.006 ↗
11. Experimental methods for terminal ballistics impact physics
12. Estimation of the V50 using semi-empirical (1-point) procedures10.1016/S1359-8368(97)00032-2 ↗
13. The behaviour of laminated composite plates as armour10.1016/S0924-0136(96)00032-5 ↗
14. Perforation of 12mm thick steel plates by 20mm diameter projectiles with flat, hemispherical and conical noses Part I: experimental study10.1016/S0734-743X(01)00034-3 ↗
15. A simple model to predict residual velocities of thick composite laminates subjected to high velocity impact10.1016/0734-743X(96)89053-1 ↗
16. On the Lambert–Jonas approximation for ballistic impact10.1016/S0093-6413(02)00246-X ↗
17. Ballistic perforation dynamics10.1115/1.3636566 ↗
18. Lambert JP, Jonas GH. Towards standardization of in-terminal ballistic testing: velocity representation. Ballistic Research Laboratory, Aberdeen, MD, Report No. BRL-R-1852; 1976.10.21236/ADA021389 ↗
19. Finite-element modeling of the ballistic impact of fabric armor10.1016/S0734-743X(02)00031-3 ↗
20. Finite element analysis to predict penetration and perforation of thick FRP laminates struck by projectiles10.1016/j.ijimpeng.2006.11.008 ↗
21. LS-DYNA 971, Livermore Software Technology Corporation (LSTC), Livermore, CA; 2007. .
22. Finite element calculation of 4-step 3-dimensional braided composite under ballistic perforation10.1016/j.compositesb.2004.01.001 ↗
23. Post-failure analysis of bolted composite joints in tension or shear-out mode failure10.1177/002199838702100903 ↗
24. A progressive damage model for laminated composites containing stress concentrations10.1177/002199838702100904 ↗
25. Cheung CK, Long X, Liaw BM, Delale F, Walser AD, Raju BB. Composite strips with a circular stress concentration under tension. In: Proceedings of the SEM X international congress & exposition on experimental and applied mechanics, Section 89: Composites, Paper No. 387, Costa Mesa, CA, June 7–10; 2004.
26. Liaw BM, Cheung CK, Delale F, Walser AD, Raju BB. Tension-induced damages of S2 glass/toughened epoxy composites at room and elevated temperatures. In: Proceedings of the 13th annual advanced composite conference & exposition, ACCE’98, Mechanics Session, Paper No. 3, Cobo Center, Detroit, MI, September 28–29; 1998.10.1115/IMECE1999-0502 ↗
27. Adams · 2003
28. Test methods
29. High-strength medium-temperature thermoset matrix composites. In: Reinhart TJ et al., editors. Composites, engineered materials handbook, vol. 1. ASM International, Metals Park (OH); 1987.
30. On the crack extension in plates under plane loading and transverse shear10.1115/1.3656897 ↗
31. Strain-energy-density factor applied to mixed mode crack problems10.1007/BF00035493 ↗
32. Laursen · 2002
33. Thomson · 1997
34. Vinson · 2002