A method is presented for calculating the stress-strain relations in a muiti-layer composite made up of materials whose individual stress-strain characteristics are non-linear and possibly different. The method is applied to the case of asymmetric tubes in tension, and comparisons with experimentally measured data are given.
Non-Linear Cord-Rubber Composites
Sae Technical Papers
Aerospace Technology Conference and Exposition ; 1989
1989-09-01
Aufsatz (Konferenz)
Englisch
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