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The Effects of Temperature Change on the Residual Bending Strength of CFRP Laminates after Impact  

Ra Seung-woo (Department of Mechanical and Automotive Engineering Kongju National University)
Jung Jong-an (Division of Automotive Engineering Songwon College)
Yang In-young (Division of Mechanical Information Engineering Chosun University)
Publication Information
Journal of the Korean Society of Safety / v.20, no.1, 2005 , pp. 75-80 More about this Journal
Abstract
In this paper, when CF/EPOXY laminates for high efficiency space structure are subjected to FOD(Foreign Object Damage), the effects of temperature change on the impact damages(inter laminar separation and transverse crack) of CF/EPOXY laminates and the relationship between residual life and impact damages ale experimentally investigated. Composite laminates used in this experiment are CF/EPOXY orthotropic laminated plates, which have two-interfaces $[0^{\circ}_6/90^{\circ}_6]S$ and four-interfaces $[0^{\circ}_3/90^{\circ}_6/0^{\circ}_3]S$. CF/EPOXY specimens with impact damages caused by a steel ball launched from the air gun were observed by the scanning acoustic microscope under room and high temperatures. In this experimental results, various relations were experimentally observed including the delamination area vs. temperature change, the bending strength vs. impact energy and the residual bending strength vs. impact damage of CF/EPOXY laminates. And as the temperature of CF/PEEK laminates increases, the delaminaion areas of impact-induced damages decrease linearly. A linear relationship between the impact energy and the delamination areas were observed. As the temperature of CF/PEEK laminates increases, the delamination areas decrease because of higher initial delaminatin damage energy.
Keywords
impact damage; high temperature environment; delamination area; residual bending strength;
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