Effect of Fiber and Matrix Maximum Strain on the Energy Absorption of Composite Materials

Author:

Farley Gary L.1

Affiliation:

1. Aerostructures Directorate U.S. Army Aviation Research and Technology Activity (AVSCOM) Langley Research Center Hampton, Virginia

Abstract

Static crushing tests were conducted on graphite composite tubes to examine the in fluence of fiber and matrix maximum strain at failure on the energy absorption capability of graphite reinforced composite material. Fiber and matrix maximum strain at failure were determined to significantly effect energy absorption. The higher strain at failure composite material system, AS-4/5245, exhibited superior energy absorption capability compared to AS-4/934, T300/5245 or T300/934 composite material. Results of this in vestigation suggest that to achieve maximum energy from a composite material a matrix material that has a higher strain at failure than the fiber reinforcement should be used.

Publisher

SAGE Publications

Subject

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

Reference7 articles.

1. Cronkhite, J.D. , Hass, T.J., Berry, V.L. and Winter, R. "Investigation of the Crash Impact Characteristics of Advanced Airframe Structure," USARTL-TR-79-11 (September 1979).

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