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Civil-Comp Proceedings
ISSN 1759-3433 CCP: 83
PROCEEDINGS OF THE EIGHTH INTERNATIONAL CONFERENCE ON COMPUTATIONAL STRUCTURES TECHNOLOGY Edited by: B.H.V. Topping, G. Montero and R. Montenegro
Paper 163
Parametric Instability Analysis of Stringer Stiffened Circular Cylindrical Shells under Axial Compression and External Hydrostatic Pressure M.R. Khedmati1, M.J. Mazaheri1 and A.R. Karimi2
1Faculty of Marine Technology, Amirkabir University of Technology, Tehran, Iran
M.R. Khedmati, M.J. Mazaheri, A.R. Karimi, "Parametric Instability Analysis of Stringer Stiffened Circular Cylindrical Shells under Axial Compression and External Hydrostatic Pressure", in B.H.V. Topping, G. Montero, R. Montenegro, (Editors), "Proceedings of the Eighth International Conference on Computational Structures Technology", Civil-Comp Press, Stirlingshire, UK, Paper 163, 2006. doi:10.4203/ccp.83.163
Keywords: instability, stringer stiffened shell, axial compression, hydrostatic pressure.
Summary
About three-fourths of the earth's surface is covered by water. It is believed
that during the twenty-first century, the interest in exploring and using the ocean sea bed will
increase, for both military and commercial purposes. Submarines and offshore
structures comprising of shell structures stiffened with other structural elements, will
be the first structures that are used for such purposes. In this context, a better
understanding of the behaviour and strength of such a type of stiffened shell is of
paramount importance.
Different methods may be applied in order to capture buckling behaviour and the strength of shell structures [2,3]. Analytical solutions [4] as well as numerical and experimental ones have already been developed for estimation of the buckling strength and behaviour of unstiffened and stiffened shells. Many years of designing and testing, ensure that submarines are not prone to buckling when subjected to high external underwater pressure. A balance is required between over designing to prevent buckling and avoiding a weight gain penalty. Finite element analyses assist in determining this balance by predicting if buckling will occur. Linear buckling analyses predict the critical modes of collapse. Non-linear load-displacement analyses predict collapse pressures for critical modes of collapse, taking into account plasticity and realistic imperfections formed during manufacturing processes. Non-linear analyses are required because failure can occur by buckling at pressures which may be considerably lower than those predicted by linear buckling analysis. The focus of this study lies on the subject of buckling analysis of stiffened shells. In line with this research requirement, the commercial finite element code ANSYS [1] is utilised to simulate the collapse of stringer stiffened shells. Different parameters are considered in the finite element models. References
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