Boundary layer theory for the buckling and postbuckling of an anisotropic laminated cylindrical shell, Part III: Prediction under torsion
Author:
- Hui-Shen ShenHSHui-Shen Shen
- 1 February 2008
- journal article
- research article
- Published by Elsevier in Composite Structures
- Vol. 82 (3) , 371-381
Abstract
No abstract availableKeywords
This publication has 12 references indexed in Scilit:
- Boundary layer theory for the buckling and postbuckling of an anisotropic laminated cylindrical shell. Part I: Prediction under axial compressionComposite Structures, 2008
- Stability of Cylindrical Composite Shells under TorsionInternational Applied Mechanics, 2005
- The effect of extension/twist anisotropy on compression buckling in cylindrical shellsComposites Part B: Engineering, 2003
- The effect of flexural/twist anisotropy on compression buckling of quasi-isotropic laminated cylindrical shellsComposite Structures, 2002
- Anisotropic effects in the compression buckling of laminated composite cylindrical shellsComposites Science and Technology, 2002
- Torsional Buckling Analysis of Composite CylindersAIAA Journal, 2001
- Buckling Analysis of Thick-Walled Composite Pipe Under TorsionJournal of Pressure Vessel Technology, 1997
- Buckling of moderately thick, laminated cylindrical shells under torsionAIAA Journal, 1994
- Postbuckling behavior of circular cylindrical shells under torsionArchive of Applied Mechanics, 1976
- Buckling of Initially Imperfect Cylindrical Shells Subject to TorsionJournal of Applied Mechanics, 1957