Dynamic response of a composite wing-shaped plate under impact loading = Đáp ứng của tấm composite dạng cánh máy bay dưới tác động của tải trọng va đạp

Abstract

This paper presents an analysis of the response of a composite wing-shaped plate subjected to impact loading. The study investigates the effects of geometric configurations, material properties and impact location on the transient deflection response. The computational model is based on Mindlin's plate theory. A numerical simulation program is developed in Matlab, employing an eight-node isoparametric plate element with five degrees of freedom per node.