NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Evaluation of failure criterion for graphite/epoxy fabric laminatesThe development and application of the tensor polynomial failure criterion for composite laminate analysis is described. Emphasis is given to the fabrication and testing of Narmco Rigidite 5208-WT300, a plain weave fabric of Thornel 300 Graphite fibers impregnated with Narmco 5208 Resin. The quadratic-failure criterion with F sub 12=0 provides accurate estimates of failure stresses for the graphite/epoxy investigated. The cubic failure criterion was recast into an operationally easier form, providing design curves that can be applied to laminates fabricated from orthotropic woven fabric prepregs. In the form presented, no interaction strength tests are required, although recourse to the quadratic model and the principal strength parameters is necessary. However, insufficient test data exist at present to generalize this approach for all prepreg constructions, and its use must be restricted to the generic materials and configurations investigated to date.
Document ID
19850010715
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Tennyson, R. C.
(Toronto Univ. Ontario)
Wharram, G. E.
(Toronto Univ. Ontario)
Date Acquired
September 5, 2013
Publication Date
February 1, 1985
Subject Category
Composite Materials
Report/Patent Number
NAS 1.26:172547
NASA-CR-172547
Accession Number
85N19025
Funding Number(s)
CONTRACT_GRANT: NSG-7409
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available