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Effects of partial interlaminar bonding on impact resistance and loaded-hole behavior of graphite/epoxy quasi-isotropic laminatesA partial-bonding interlaminar toughening concept was evaluated for resistance to impact and for behavior of a loaded hole. Perforated Mylar sheets were interleaved between all 24 plies of a graphite/epoxy quasi-isotropic lay-up. Specimens were impacted by aluminum spheres while under tensile or compressive loads. Impact-failure thresholds and residual strengths were obtained. Loaded-hole specimens were tested in three configurations that were critical in bearing, shear, or tension. Partial bonding reduced the tensile and compressive strengths of undamaged specimens by about one-third. For impact, partial bonding did not change the threshold for impact failure under tensile preload. However, under compressive preload, partial bonding caused serious degradation of impact resistance. Partial bonding reduced the maximum load-carrying capacity of all three types of loaded-hole specimens. Overall, partial bonding degraded both impact resistance and bearing strength of holes.
Document ID
19860017956
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Illg, W.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 5, 2013
Publication Date
July 1, 1986
Subject Category
Composite Materials
Report/Patent Number
NAS 1.15:87678
NASA-TM-87678
L-16088
Report Number: NAS 1.15:87678
Report Number: NASA-TM-87678
Report Number: L-16088
Accession Number
86N27428
Funding Number(s)
PROJECT: RTOP 506-43-11-04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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