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Near-tip dual-length scale mechanics of mode-I cracking in laminate brittle matrix compositesThis paper presents the preliminary results of an on-going study of the near-tip mechanics of mode-I cracking in brittle matrix composite laminates. A finite element model is developed within the context of two competing characteristic lengths present in the composite: the microstructural length (the thickness of the layers) and a macro-length (crack-length, uncracked ligament size, etc.). For various values of the parameters which describe the ratio of these lengths and the constituent properties, the stresses ahead of a crack perpendicular to the laminates are compared with those predicted by assuming the composite is homogeneous orthotropic. The results can be used to determine the conditions for which homogenization can provide a sufficiently accurate description of the stresses in the vicinity of the crack-tip.
Document ID
19920051959
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Ballarini, R.
(NASA Lewis Research Center Cleveland, OH, United States)
Islam, S.
(Case Western Reserve University Cleveland, OH, United States)
Charalambides, P. G.
(Michigan Technological University Houghton, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1992
Subject Category
Structural Mechanics
Report/Patent Number
AIAA PAPER 92-2491
Meeting Information
Meeting: AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
Location: Dallas, TX
Country: United States
Start Date: April 13, 1992
End Date: April 15, 1992
Accession Number
92A34583
Funding Number(s)
CONTRACT_GRANT: NSF MSS-91-57090
CONTRACT_GRANT: NAG3-856
Distribution Limits
Public
Copyright
Other

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