Response of perforated composite tubes subjected to axial compressive loading

Author:

Taheri-Behrooz Fathollah,Esmaeel Ramadan A.,Taheri Farid

Publisher

Elsevier BV

Subject

Mechanical Engineering,Building and Construction,Civil and Structural Engineering

Reference22 articles.

1. Anonymous. Buckling of thin-walled circular cylinders. NASA Space Vehicle Design Criteria, NASA SP-8007, 1965.

2. Huhne C, Raimund R, Tessmer J. A new Approach for robust design of composite cylindrical shells under axial compression. European Conference on Spacecraft Structures, Materials and Mechanical Testing, Nordwijk, The Netherland, 10–12 May 2005.

3. Koiter WT, Elishako I, Li YW, Starnes JH. Buckling of an axially compressed imperfect cylindrical shell of variable thickness. Proceedings of the 35th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, Hilton Head, SC, 1994. AIAA Paper No. 94-1339.

4. Effects of imperfections on the buckling response of compression-loaded composite shells;Hilburger;International Journal of Non-Linear Mechanics,2002

5. Effects of imperfections of the buckling response of composite shells;Hilburger;Thin-Walled Structure,2004

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