The effect of different geometrical imperfection of buckling of composite cylindrical shells subjected to axial loading

Author:

Shahrjerdi A.,Bahramibabamiri B.

Publisher

Springer Science and Business Media LLC

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science

Reference29 articles.

1. Almroth, BO, & Holmes, AM. (1972). Buckling of shells with cutouts. Experimental and analysis. Journal of Solids Structures, 8, 1057–1566.

2. Bisagni, C. (2000). Numerical analysis and experimental correlation of composite shell buckling and post-buckling. Composite: Part B, 31, 655–667.

3. Card, MF. (1969). The sensitivity of buckling of axially compressed fibre-reinforced cylindrical shells to small geometric imperfections, NASA TMX-61914.

4. B. Geier, H. Klein and R. Zimmermann, Buckling tests with axially compressed unstiffened cylindrical shells made from CFRP, in: Buckling of shell structures, on land, in the sea and in the air, Proceedings of the International Conference, J.F. Jullien, ed., INSA Lyon, Elsevier Applied Science, London, New York (September 1991), pp. 498-507

5. Geier, B, Meyer-Piening, HR, & Zimmermann, R. (2002). On the influence of laminate stacking on buckling of composite cylindrical shells subjected to axial compression. Composite Structures, 55, 467–474.

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