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Effect of impact damage and open holes on the compression strength of tough resin/high strain fiber laminatesStructural damage and design-based inclusions such as cutouts can reduce significantly the strength of graphite-epoxy laminates. One composite mechanics research activity at the Langley Research Center is to assess and improve the performance of composite structures in strength are common to both tension and compression loaded laminates; however, the problem associated with compression performance is the most illusive to solve. Compression failure involves both shear crippling and delamination modes. Several graphite-epoxy material systems proposed for improved damage-tolerance were studied. Material parameters included both tough resin formulations and high strain fibers.
Document ID
19840012582
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Williams, J. G.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
February 1, 1984
Subject Category
Composite Materials
Report/Patent Number
NAS 1.15:85756
NASA-TM-85756
Report Number: NAS 1.15:85756
Report Number: NASA-TM-85756
Meeting Information
Meeting: Tough Mater. Composite Workshop
Location: Hampton, VA
Country: United States
Start Date: May 24, 1983
End Date: May 26, 1983
Accession Number
84N20650
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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