Thermomechanical postbuckling of composite laminated cylindrical shells with local geometric imperfections (Q1303086)
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scientific article; zbMATH DE number 1342517
| Language | Label | Description | Also known as |
|---|---|---|---|
| English | Thermomechanical postbuckling of composite laminated cylindrical shells with local geometric imperfections |
scientific article; zbMATH DE number 1342517 |
Statements
Thermomechanical postbuckling of composite laminated cylindrical shells with local geometric imperfections (English)
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22 September 1999
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The author examines the effect of local geometric imperfection (imperfection in shape) on the buckling and postbuckling of laminated cylindrical shells subjected to axial loading and uniform temperature change. The boundary layer type theory is used to obtain the load-deflection curve. It is shown that, in many cases, under thermal loading the cylindrical shell is insensitive to imperfections.
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boundary layer theory
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local geometric imperfection
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buckling
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postbuckling
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laminated cylindrical shells
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axial loading
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uniform temperature change
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load-deflection curve
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thermal loading
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0.96473336
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0.9349636
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0.9239617
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0.90507936
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0.90100336
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0.89805937
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0.8961677
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