NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Comparison of toughened composite laminates using NASA standard damage tolerance testsThe 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.
Document ID
19840021903
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Williams, J. G.
(NASA Langley Research Center Hampton, VA, United States)
Obrien, T. K.
(Army Structures Lab. Hampton, VA, United States)
Chapman, A. J., III
(NASA Langley Research Center)
Date Acquired
August 12, 2013
Publication Date
August 1, 1984
Publication Information
Publication: ACEE Composite Struct. Technol.
Subject Category
Composite Materials
Accession Number
84N29972
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available