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Residual thermal and moisture influences on the strain energy release rate analysis of edge delaminationA laminated plate theory analysis is developed to calculate the strain energy release rate associated with edge delamination growth in a composite laminate. The analysis includes the contribution of residual thermal and moisture stresses to the strain energy released. The strain energy release rate, G, increased when residual thermal effects were combined with applied mechanical strains, but then decreased when increasing moisture content was included. A quasi-three-dimensional finite element analysis indicated identical trends and demonstrated these same trends for the individual strain energy release rate components, G sub I and G sub II, associated with interlaminar tension and shear. An experimental study indicated that for T300/5208 graphite-epoxy composites, the inclusion of residual thermal and moisture stresses did not significantly alter the calculation of interlaminar fracture toughness from strain energy release rate analysis of edge delamination data taken at room temperature, ambient conditions.
Document ID
19860060306
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Obrien, T. K.
(NASA Langley Research Center; U.S. Army, Aerostructures Directorate, Hampton VA, United States)
Raju, I. S.
(Analytical Services and Materials, Inc. Hampton, VA, United States)
Garber, D. P.
(Kentron International, Inc. Aerospace Technologies, Div., Hampton, VA, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1986
Publication Information
Publication: Journal of Composites Technology and Research
Volume: 8
ISSN: 0885-6804
Subject Category
Composite Materials
Accession Number
86A45044
Distribution Limits
Public
Copyright
Other

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