Affiliation:
1. Department of Aeronautics and Astronautics Stanford University Stanford, CA 94305
Abstract
Teas were conducted measuring the deformations of composite open cylindrical shells subjected to temperature changes. The cylindrical shells were made of 16 plies of Fiberite T300/934 unidirectional graphite-epoxy tape arranged as cither [02/902]2, or [902/02)2,. The measured deformations were compared to the results of a higher order shell theory. It is shown that terms representing extensional strain in the thickness direction must be considered for the analysis to represent the data accurately.
Subject
Materials Chemistry,Mechanical Engineering,Mechanics of Materials,Ceramics and Composites
Cited by
6 articles.
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