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Failure mechanics in low-velocity impacts on thin composite platesEight-ply quasi-isotropic composite plates of Thornel 300 graphite in Narmco 5208 epoxy resin (T300/5208) were tested to establish the degree of equivalence between low-velocity impact and static testing. Both the deformation and failure mechanics under impact were representable by static indentation tests. Under low-velocity impacts such as tool drops, the dominant deformation mode of the plates was the first, or static, mode. Higher modes are excited on contact, but they decay significantly by the time the first-mode load reaches a maximum. The delamination patterns were observed by X-ray analysis. The areas of maximum delamination patterns were observed by X-ray analysis. The areas of maximum delamination coincided with the areas of highest peel stresses. The extent of delamination was similar for static and impact tests. Fiber failure damage was established by tensile tests on small fiber bundles obtained by deplying test specimens. The onset of fiber damage was in internal plies near the lower surface of the plates. The distribution and amount of fiber damage was similar fo impact and static tests.
Document ID
19830016291
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Elber, W.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
May 1, 1983
Subject Category
Composite Materials
Report/Patent Number
NASA-TP-2152
NAS 1.60:2152
L-15588
Report Number: NASA-TP-2152
Report Number: NAS 1.60:2152
Report Number: L-15588
Accession Number
83N24562
Funding Number(s)
PROJECT: RTOP 506-53-23-05
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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