NASA NTRS · 19860012129
Modeling the curing process of thick-section autoclave cured composites
Abstract
Temperature gradients are significant during cure of large area, thick-section composites. Such temperature gradients result in nonuniformly cured parts with high void contents, poor ply compaction, and variations in the fiber/resin distribution. A model was developed to determine the temperature distribution in thick-section autoclave cured composites. Using the model, long with temperature measurements obtained from the thick-section composites, the effects of various processing parameters on the thermal response of the composites were examined. A one-dimensional heat transfer model was constructed for the composite-tool assembly. The governing differential equations and associated boundary conditions describing one-dimensional unsteady heat-conduction in the composite, tool plate, and pressure plate are given. Solution of the thermal model was obtained using an implicit finite difference technique.
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Loos, A. C., Dara, P. H.. 1985-04-01. Modeling the curing process of thick-section autoclave cured composites. https://ntrs.nasa.gov/citations/19860012129
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