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Matrix resin effects in composite delamination - Mode I fracture aspects

Authors :
Hunston, Donald L
Moulton, Richard J
Johnston, Norman J
Bascom, Willard D
Publication Year :
1987
Publisher :
United States: NASA Center for Aerospace Information (CASI), 1987.

Abstract

A number of thermoset, toughened thermoset, and thermoplastic resin matrix systems were characterized for Mode I critical strain energy release rates, and their composites were tested for interlaminar critical strain energy release rates using the double cantilever beam method. A clear correlation is found between the two sets of data. With brittle resins, the interlaminar critical strain energy release rates are somewhat larger than the neat resin values due to a full transfer of the neat resin toughness to the composite and toughening mechanisms associated with crack growth. With tougher matrices, the higher critical strain energy release rates are only partially transferred to the composites, presumably because the fibers restrict the crack-tip deformation zones.

Subjects

Subjects :
Composite Materials

Details

Language :
English
Database :
NASA Technical Reports
Publication Type :
Report
Accession number :
edsnas.19870061261
Document Type :
Report