The effect of different geometrical imperfection of buckling of composite cylindrical shells subjected to axial loading
Background: Advanced lightweight laminated composite shells are increasingly being used in modern aerospace structures to enhance their structural efficiency and performance. Such thin-walled structures are susceptible to buckling when subjected to static and dynamic compressive stresses. This paper...
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International Journal of Mechanical and Materials Engineering, University of Malaya
2015
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| Online Access: | http://www.myjurnal.my/public/article-view.php?id=95533 |