Scale Effects in the Response and Failure of Fiber Reinforced Composite Laminates Loaded in Tension and in Flexure

Author:

Jackson Karen E.1,Kellas Sotiris2,Morton John3

Affiliation:

1. US. Army Aerostructures Directorate AVSCOM Mail Stop 495 NASA Langley Research Center Hampton, VA 23681

2. Lockheed Engineering and Sciences Company 144 Research Drive Hampton, VA 23666

3. Engineering Science and Mechanics Department Virginia Polytechnic Institute and State University Blacksburg, VA 24061

Abstract

The feasibility of using scale model testing for predicting the full-scale behavior of flat composite coupons loaded in tension and beam-columns loaded in flexure is examined. Classical laws of similitude are applied to fabricate and test replica model specimens to identify scaling effects in the load response, strength, and mode of failure. Experiments were performed on graphite-epoxy composite specimens having different laminate stacking sequences and a range of scaled sizes. From the experiments it was deduced that the elastic response of scaled composite specimens was independent of size. However, a significant scale effect in strength was observed. In addition, a transition in failure mode was observed among scaled specimens of certain laminate stacking se quences. A Weibull statistical model and a fracture mechanics based model were applied to predict the strength scale effect since standard failure criteria cannot account for the in fluence of absolute specimen size on strength.

Publisher

SAGE Publications

Subject

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

Reference35 articles.

1. Design for Dynamic Loading, The Use of Model Analysis;Davies, I.L.,1982

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