References
- Hoof, J. V. (1999). Modeling of Impact Induced Delamination in Composite Materials. PhD Thesis, Carleton University.
- Ji, K. H. and Kim, S. J. (2006). Direct numerical simulation of composite laminates under low velocity impact. Journal of the Korean Society for Composite Materials, 19, 1-8.
- Jung, W. K., Ahn, S. H., Lee, W. I., Kim, H. J., and Kwon, J. W. (2006). Fracture mechanism of ceramic/glass-fiberreinforced-composite laminate by high velocity impact. Journal of the Korean Society of Precision Engineering, 23, 170-176.
- Kong, C. D., Kim, Y. K., and Lee, S. H. (2007). Comparative study on low-velocity impact behavior of graphite/epoxy composite laminate and steel plate. Journal of the Korean Society for Composite Materials, 20, 1-6.
- Lee, B. W., Lee, S. H., Kim, S. G., Yoon, B. I., and Paik, J. G. (2008). A study on the low speed impact response and frictional characteristic of shear thickening fluid impregnated Kevlar fabrics. Journal of the Korean Society for Composite Materials, 21, 15-24.
- Lee, B. L., Walsh, T. F., Won, S. T., Patts, H. M., Song, J. W., and Mayer, A. H. (2001). Penetration failure mechanisms of armor-grade fiber composites under impact. Journal of Composite Materials, 35, 1605-1633. https://doi.org/10.1106/YRBH-JGT9-U6PT-L555
- Liu, D. (2004). Characterization of impact properties and damage process of glass/epoxy composite laminates. Journal of Composite Materials, 38, 1425-1442. https://doi.org/10.1177/0021998304042741
- Livermore Software Technology Corporation (2007). LSDYNA Keyword User Manual. Livermore, CA: Livermore Software Technology Corporation.
- Livermore Software Technology Corporation (2006). LSDYNA Theory Manual. Livermore, CA: Livermore Software Technology Corporation.
- Niu, M. (2005). Composite airframe structures. Hong Kong: Hong Kong Conmilit Press, Ltd.
- Park, I. J., Jung, S. N., Kim, D. H., and Yun, C. Y. (2009). General purpose cross-section analysis program for composite rotor blades. International Journal of Aeronautical and Space Sicences, 10, 77-85. https://doi.org/10.5139/IJASS.2009.10.2.077
- Park, J. B., Kim, D. R., Kim, H. G., and Hwang, T. K. (2008). Evaluation of residual strength of CFRP pressure vessel after low velocity impact. Journal of the Korean Society for Composite Materials, 21, 9-17.
- Schweizerhof, K., Weimar, K., Munz, T., and Rottner, T. (1998). Crashworthiness analysis with enhanced composite material in ls-dyna-material and limits. Proceedings of the 5th LS-DYNA World Conference, Southfield, MI.
- Tabiei, A. and Chen, Q. (2001). Micromechanics based composite material model for crash worthiness explicit finite element simulation. Journal of Composite Materials, 14, 264-289.
- Tabiei, A. and Ivanov, I. (2002). Computational micromechanical model of flexible woven fabric for finite element impact simulation. International Journal for Numerical Methods in Engineering, 53, 1259-1276. https://doi.org/10.1002/nme.321
- Unosson, M. and Buzaud, E. (2000). Scalar and Vectorized User Defined Material Routine in LS-DYNA. Methodology Report. Tumba: FOA Defence Research Establishment.
- Yen, C. F. (2002). Ballistic impact modeling of composite materials. Proceedings of the 7th International LS-DYNA Users Conference, Detroit, MI.
Cited by
- Ballistic Performance of Multi-layered Fabric Composite Plates Impacted by Different 7.62mm Calibre Projectiles vol.88, 2014, https://doi.org/10.1016/j.proeng.2014.11.146
- NiTi SMA Wires Coupled with Kevlar Fabric: a Real Application of an Innovative Aircraft LE Slat System in SMAHC Material 2017, https://doi.org/10.1007/s10443-017-9618-4
- An experimental and numerical investigation on ballistic performance of advanced composites vol.51, pp.25, 2017, https://doi.org/10.1177/0021998317691810
- Effect of Projectile Geometry on the Deformation Behavior of Kevlar Composite Armors Under Ballistic Impact vol.07, pp.03, 2015, https://doi.org/10.1142/S1758825115500398