NASA NTRS ยท 19820007250
Indentation law for composite laminates
Abstract
Static 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.
Keep this discovery
Explore connections, maps & timelines
Yang, S. H.. 1981-07-31. Indentation law for composite laminates. https://ntrs.nasa.gov/citations/19820007250
Cite the original work for its findings. Save a collection to share your selection of sources.