On the Feasibility of Using Thermal Gradients for Active Control of Interlaminar Stresses in Laminated Composites

Author:

Kim T.1,Steadman D.2,Hanagud S. V.2,Atluri S. N.2

Affiliation:

1. Boeing Commercial Airplane Group, PO. Box 3707 MS 67-HM, Seattle, WA 98124-2207

2. FAA Center of Excellence for Computational Modeling of Aircraft Structures, Georgia Institute of Technology, Atlanta, GA 30332-0356

Abstract

In this paper, a method is proposed to actively control interlaminar stresses near the free edges of laminated composites by through-thickness thermal gradients. Theoretical solutions are given for optimal steady-state through-thickness temperature distributions under uniaxial loading that are required to elmininate or reduce the interlaminar stresses below a prescribed level. The optimal solutions are obtained by minimizing appropriate performance indices that are functions of the far-field properties, with respect to the through-thickness temperature differences. In the second part, an experimental investigation is conducted on a glass/epoxy cross-ply laminate with embedded piezoelectric sensors and a thermal heater. Through the experiment, the feasiblity of the thermal control of interlaminar stresses is demonstrated.

Publisher

SAGE Publications

Subject

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

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