Compressive Strength of Damaged and Repaired Composite Plates

Author:

Finn Scott R.1,He Yi-Fei1,Springer George S.1,Lee Hung-Joo2

Affiliation:

1. Department of Aeronautics and Astronautics Stanford University Stanford, CA 94305

2. Korean Military Academy Nowonku, Seoul, Korea

Abstract

Tests were performed assessing the effectiveness of repair in restoring the mechanical properties of damaged, solid composite plates made either of Fiberite T300/976 graphite-epoxy, Fiberite IM7/977-2 graphite-toughened epoxy, or ICI APC-2 graphite-PEEK. The plate length, the layup and the amount of damage were also varied. Damage was introduced in the plates either by impacting them with a solid projectile or by applying a transverse static load. Some (75 % ) or all (100 % ) of the damaged zone was then cut out, and the plate was repaired by plugging and patching the hole. The effec tiveness of the repair was evaluated by measuring the compressive strengths of undamaged plates, damaged plates with no cutout, damaged plates with a cutout, and repaired plates. The data at an intermediate stage of repair (damaged plates with a cutout) provide informa tion on the effect of each repair step on the compressive strength. The results indicated that for the solid plates used in these tests, the repair methods used herein did not improve the compressive strength of already damaged plates.

Publisher

SAGE Publications

Subject

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

Reference6 articles.

1. A New Approach toward Understanding Damage Mechanisms and Mechanics of Laminated Composites Due to Low-Velocity Impact: Part I—Experiments

2. Residual Strength of a Carbon/Epoxy Composite Material Subjected to Repeated Impact

3. Ilcewicz, L.B., E.F. Dost and R.L. Coggeshall . 1989. "A Model for Compression after Impact Strength Evaluation," Advanced Materials: The Big Payoff, Wegman, et al., ed. Society for the Advancement of Materials and Process Engineering, pp. 130-140.

4. Damage Tolerance of Laminated Composites Containing an Open Hole and Subjected to Compressive Loadings: Part II—Experiment

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