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A damage tolerant design parameter for graphite/epoxy laminated compositesThe results of an extensive experimental investigation of the fracture behavior of notched graphite/epoxy laminates are presented. Twenty-seven laminates with different stacking sequences and laminate thicknesses have been studied. The data presented herein suggest that a damage tolerant design parameter exists that is relatively independent of ply stacking sequence and laminate thickness.
Document ID
19860029131
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Harris, C. E.
(Texas A&M University College Station, United States)
Morris, D. H.
(Virginia Polytechnic Institute and State University Blacksburg, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1985
Publication Information
Publication: Journal of Composites Technology and Research
Volume: 7
Subject Category
Composite Materials
Accession Number
86A13869
Funding Number(s)
CONTRACT_GRANT: NAG1-343
Distribution Limits
Public
Copyright
Other

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