Comparison of toughened composite laminates using NASA standard damage tolerance tests

Abstract

The proposed application of composite materials to transport wing and fuselage structures prompted the search for tougher materials having improved resistance to impact damage and delamination. Several resin/graphite fiber composite materials were subjected to standard damage tolerance tests and the results were compared to ascertain which materials have superior toughness. In addition, test results from various company and NASA laboratories were compared for repeatability.

Authors

• Williams, J. G. NASA Langley Research Center
• Obrien, T. K. Army Structures Lab.
• Chapman, A. J., III NASA Langley Research Center