The Proceedings of the Dynamics & Design Conference
Online ISSN : 2424-2993
2003
Session ID : 513
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513 Dynamic Buckling Analysis of Laminated Composite Shells of Revolution
Hiroshi OHYA
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CONFERENCE PROCEEDINGS FREE ACCESS

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Abstract
The finite element method is applied to the nonlinear axisymmetric dynamic buckling analysis of laminated composite shells of revolution. The coupling effect of general laminates is considered in the stress-strain relation. The effects of shell geometrical parameter and coupling on the axisymmetric dynamic buckling pressure of shallow spherical shells are investigated.
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© 2003 The Japan Society of Mechanical Engineers
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