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Ten deg off-axis tensile test for intralaminar shear characterization of fiber compositesA combined theoretical and experimental investigation was conducted to assess the suitability of the 10 deg off-axis tensile test specimen for the intralaminar shear characterization of unidirectional composites. Composite mechanics, a combined-stress failure criterion, and a finite element analysis were used to determine theoretically the stress-strain variation across the specimen width and the relative stress and strain magnitudes at the 10 deg plane. Strain gages were used to measure the strain variation across the specimen width at specimen midlength and near the end tabs. Specimens from Mod-I/epoxy, T-300/epoxy, and S-glass/epoxy were used in the experimental program. It was found that the 10 deg off-axis tensile test specimen is suitable for intralaminar shear characterization and it is recommended that it should be considered as a possible standard test specimen for such a characterization.
Document ID
19760015226
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Chamis, C. C.
(NASA Lewis Research Center Cleveland, OH, United States)
Sinclair, J. H.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 3, 2013
Publication Date
April 1, 1976
Subject Category
Composite Materials
Report/Patent Number
E-8577
NASA-TN-D-8215
Report Number: E-8577
Report Number: NASA-TN-D-8215
Accession Number
76N22314
Funding Number(s)
PROJECT: RTOP 506-17
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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