Affiliation:
1. Department of Aeronautics and Astronautics Stanford University, Stanford, CA 94305
Abstract
A model was developed which describes the filament winding process of composite cylinders. The model relates the significant process variables such as winding speed, fiber tension, and applied temperature to the thermal, chemical and mechanical be havior of the composite cylinder and the mandrel. Based on the model, a user friendly code was written which can be used to calculate (1) the temperature in the cylinder and the mandrel, (2) the degree of cure and viscosity in the cylinder, (3) the fiber tensions and fiber positions, (4) the stresses and strains in the cylinder and in the mandrel, and (5) the void diameters in the cylinder.
Subject
Materials Chemistry,Mechanical Engineering,Mechanics of Materials,Ceramics and Composites
Reference18 articles.
1. A model of filament-wound thin cylinders
2. Springer, G.S. 1983. "A Model of the Curing Process of Epoxy Matrix Composites ", in Progress in Science and Engineering of Composites. T. Hayashi. K. Kawaka and S. Umekawa, eds. Japan Society for Composite Materials, pp. 23-35.
3. Curing of Epoxy Matrix Composites
4. Filament Winding Cylinders
5. Heat of Reaction, Degree of Cure, and Viscosity of Hercules 3501-6 Resin
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