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Investigating compression failure mechanisms in composite laminates with a transient fiberglass-epoxy birefringent materialAn experimental study is reported in which a nondestructive technique involving the use of a transparent fiberglass-epoxy composite birefringent material has been used to investigate compression failure mechanisms in graphite-epoxy laminates. It is shown that the birefringency and transparency of the fiberglass-epoxy material permits regions of high stress to be located and the mechanisms of local failure propagation to be identified within the laminate. The material may also be useful for studying stress fields and for identifying failure initiation and propagation mechanisms in a wide variety of composite-structure problems.
Document ID
19850031781
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Shuart, M. J.
(NASA Langley Research Center Hampton, VA, United States)
Williams, J. G.
(NASA Langley Research Center Structures and Dynamics Div., Hampton, VA, United States)
Date Acquired
August 12, 2013
Publication Date
November 1, 1984
Publication Information
Publication: Experimental Techniques
Volume: 8
ISSN: 0732-8818
Subject Category
Composite Materials
Accession Number
85A13932
Distribution Limits
Public
Copyright
Other

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