Glass fibre reinforced polyester square flat panels were tested under impact loading conditions using drop weight testing machine capable of providing load-time plots. Three different laminates were investigated. The analysis, which is based on the finite element technique, produced good results in predicting the deflection in the panels.
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References
1.
1. Nahas, M. N.1987. "Radial Impact Strength of Fibre-Reinforced Composite Tubes,"J. of Materials Sciences, 22:657-662.
2.
2. Golovoy A. and H. Van Oene. 1985. "Impact Energy Absorption of Unidirectional Glass-Fibre Epoxy Composites,"Polymer Engineering and Science, 25:502-506.
3.
3. Farley, G. L.1983. "Energy Absorption of Composite Materials,"J. of Composite Materials, 17:267-279.
4.
4. Bishop, S. M.1985. "Mechanical Performance and Impact Behaviour of Carbon-Fibre Reinforced PEEK,"Composite Structures, 3:295-318.
5.
5. Chen, J. K. and C. T. Sun. 1985. "Dynamic Large Deflection Response of Composite Laminates Subjected to Impact,"Composite Structures, 4:59-73.
6.
6. Sun, C. T. and J. K. Chen. 1985. "On the Impact of Initially Stressed Composite Laminates,"J. of Composite Materials, 19:490-504.
7.
7. Palazotto, A., R. Perry and R. Sandhu. 1992. "Impact Response of Graphite/Epoxy Cylindrical Panels,"AIAA Journal, 30:1827-1832.
8.
8. Tsai, C. T. and A. Palazotto. 1991. "On the Finite Element Analysis of Nonlinear Vibration for Cylindrical Shells,"International J. of Nonlinear Mechanics, 26:379-388.