Impact Resistance of Composite Laminated Sandwich Plates

Author:

Kim Chun-Gon1,Jun Eui-Jin2

Affiliation:

1. Department of Aerospace Engineering Korea Advanced Institute of Science and Technology Taejon 305-701, Korea

2. Composite Materials Lab. Korea Institute of Machinery and Metals P.O. Box 41 Changwon 641-600, Korea

Abstract

Investigated are the effects of face layup sequence and core density of a sandwich plate on the impact delamination area of the laminated facesheet. The sandwich plate is made of graphite/epoxy faces and Nomex honeycomb core. The size and shape of delamination due to impact at each interply location have been measured by the room tem perature deply technique. The shape of the interply delamination under impact is, in gen eral, found to be two-lobed. The shape exhibits very peculiar regularity under various ex perimental conditions. The quantitative measurement of delamination size has shown that the face layup with small relative orientation between adjacent plies and high density core are desirable in sandwich plates to reduce the impact delamination.

Publisher

SAGE Publications

Subject

Materials Chemistry,Mechanical Engineering,Mechanics of Materials,Ceramics and Composites

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