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Characterization of Mode 1 and Mode 2 delamination growth and thresholds in graphite/peek compositesComposite materials often fail by delamination. The onset and growth of delamination in AS4/PEEK, a tough thermoplastic matrix composite, was characterized for mode 1 and mode 2 loadings, using the Double Cantilever Beam (DCB) and the End Notched Flexure (ENF) test specimens. Delamination growth per fatigue cycle, da/dN, was related to strain energy release rate, G, by means of a power law. However, the exponents of these power laws were too large for them to be adequately used as a life prediction tool. A small error in the estimated applied loads could lead to large errors in the delamination growth rates. Hence strain energy release rate thresholds, G sub th, below which no delamination would occur were also measured. Mode 1 and 2 threshold G values for no delamination growth were found by monitoring the number of cycles to delamination onset in the DCB and ENF specimens. The maximum applied G for which no delamination growth had occurred until at least 1,000,000 cycles was considered the threshold strain energy release rate. Comments are given on how testing effects, facial interference or delamination front damage, may invalidate the experimental determination of the constants in the expression.
Document ID
19880013563
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Martin, Roderick H.
(NASA Langley Research Center Hampton, VA, United States)
Murri, Gretchen B.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 5, 2013
Publication Date
April 1, 1988
Subject Category
Composite Materials
Report/Patent Number
AVSCOM-TM-88-B-011
NAS 1.15:100577
NASA-TM-100577
Report Number: AVSCOM-TM-88-B-011
Report Number: NAS 1.15:100577
Report Number: NASA-TM-100577
Accession Number
88N22947
Funding Number(s)
PROJECT: DA PROJ. 1L1-61102-AH-45-C
PROJECT: RTOP 505-63-01-05
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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