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Experimental evaluation of the tensor polynomial criterion for designing composite structuresA comprehensive experimental and analytical evaluation of the tensor polynomial failure criterion was undertaken to determine its capability for predicting the ultimate strength of a composite limina subject to a plane stress state. Results are presented demonstrating that a quadratic formulation is too conservative and a cubic representation is required. Strength comparisons with test data derived from glass/epoxy and graphite/epoxy tubular specimens are also provided to validate the cubic strength criterion. Environmental effects including ambient temperature, exposure to vacuum, length of post-cure time, and rate of cool down were also investigated. Behavior changes associated with polymer (epoxy) matrix composites were determined in terms of variations in stiffness and tensile strength.
Document ID
19780002273
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Tennyson, R. C.
(Toronto Univ. Ontario)
Date Acquired
September 3, 2013
Publication Date
October 1, 1977
Subject Category
Composite Materials
Report/Patent Number
NASA-CR-155219
Report Number: NASA-CR-155219
Accession Number
78N10216
Funding Number(s)
CONTRACT_GRANT: NSG-7219
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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