NASA NTRS ยท 19770003306
Residual stresses in polymer matrix composite laminates
Abstract
Residual stresses in composites are induced during fabrication and by environmental exposure. The theory formulated can describe the shrinkage commonly observed after a thermal expansion test. Comparison between the analysis and experimental data for laminates of various material systems indicates that the residual stress-free temperature can be lower than the curing temperature, depending on the curing process. Effects of residual stresses on ply failure including the acoustic emission characteristics are discussed.
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Hahn, H. T.. 1976-01-01. Residual stresses in polymer matrix composite laminates. https://ntrs.nasa.gov/citations/19770003306
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