NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Indentation law for composite laminatesStatic indentation tests are described for glass/epoxy and graphite/epoxy composite laminates with steel balls as the indentor. Beam specimens clamped at various spans were used for the tests. Loading, unloading, and reloading data were obtained and fitted into power laws. Results show that: (1) contact behavior is not appreciably affected by the span; (2) loading and reloading curves seem to follow the 1.5 power law; and (3) unloading curves are described quite well by a 2.5 power law. In addition, values were determined for the critical indentation, alpha sub cr which can be used to predict permanent indentations in unloading. Since alpha sub cr only depends on composite material properties, only the loading and an unloading curve are needed to establish the complete loading-unloading-reloading behavior.
Document ID
19820007250
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Yang, S. H.
(Purdue Univ. West Lafayette, IN, United States)
Date Acquired
September 4, 2013
Publication Date
July 31, 1981
Subject Category
Composite Materials
Report/Patent Number
CML-81-1
NASA-CR-165460
Report Number: CML-81-1
Report Number: NASA-CR-165460
Accession Number
82N15123
Funding Number(s)
PROJECT: RTOP 505-33-62
CONTRACT_GRANT: NSG-3185
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available