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Parametric analytical study of instability-related delamination growthThe effect of various parameters on instability-related delamination growth was studied analytially. The configuration studied consisted of a thick composite laminate with a single through-width delamination located near one surface. Both mechanical and thermal loads were considered. All conclusions were based on the assumption that GI and GII govern delamination growth. An approximate superposition stress analysis was developed which gives closed form expressions for GI and GII. The simplicity of the analysis permitted examination of numerous configurations. Both GI and GII were found to be very sensitive to delamination length and location through the thickness. The magnitude of GI was also very sensitive to initial imperfections, which might be the results of an inclusion of finite thickness in the delamination. Critical loads for delamination growth were calculated based on three growth criteria. Large differences in the predictions highlight the need for a verified mixed-mode delamination growth criterion.
Document ID
19860046455
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Whitcomb, J. D.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1986
Publication Information
Publication: Composites Science and Technology
Volume: 25
Issue: 1, 19
ISSN: 0266-3538
Subject Category
Composite Materials
Accession Number
86A31193
Distribution Limits
Public
Copyright
Other

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