Affiliation:
1. Department of Aeronautics and Astronautics Stanford University, Stanford, CA 94305
Abstract
By using the Lee-Springer filament winding model temperatures, degrees of cure, viscosities, stresses, strains, fiber tensions, fiber motions, and void diameters were calculated in graphite-epoxy composite cylinders during the winding and subsequent cur ing. The results demonstrate the type of information which can be generated by the model. It is shown, in reference to these results, how the model, and the corresponding WIND- THICK code, can be used to select the appropriate process variables.
Subject
Materials Chemistry,Mechanical Engineering,Mechanics of Materials,Ceramics and Composites
Cited by
35 articles.
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