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Characterization of mode 1 and mixed-mode failure of adhesive bonds between composite adherendsA combined experimental and analytical investigation of an adhesively bonded composite joint was conducted to characterize both the static and fatigue beyond growth mechanism under mode 1 and mixed-mode 1 and 2 loadings. Two bonded systems were studied: graphite/epoxy adherends bonded with EC 3445 and FM-300 adhesives. For each bonded system, two specimen types were tested: a double-cantilever-beam specimen for mode 1 loading and a cracked-lapshear specimen for mixed-mode 1 and 2 loading. In all specimens tested, failure occurred in the form of debond growth. Debonding always occurred in a cohesive manner with EC 3445 adhesive. The FM-300 adhesive debonded in a cohesive manner under mixed-mode 1 and 2 loading, but in a cohesive, adhesive, or combined cohesive and adhesive manner under mode 1 loading. Total strain-energy release rate appeared to be the driving parameter for debond growth under static and fatigue loadings.
Document ID
19850012960
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mall, S.
(Missouri Univ. Rolla, United States)
Johnson, W. S.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 5, 2013
Publication Date
February 1, 1985
Subject Category
Composite Materials
Report/Patent Number
NASA-TM-86355
NAS 1.15:86355
Report Number: NASA-TM-86355
Report Number: NAS 1.15:86355
Meeting Information
Meeting: Symp. on Composite Mater. Testing and Design
Location: Philadelphia, PA
Country: United States
Start Date: April 2, 1984
End Date: April 4, 1984
Accession Number
85N21270
Funding Number(s)
PROJECT: RTOP 505-33-33
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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