LAYER-WISE SHELL THEORY FOR POSTBUCKLING OF LAMINATED CIRCULAR CYLINDRICAL-SHELLS Academic Article

abstract

• The layer-wise shell theory of Reddy is used to study the postbuckling response of circular cylindrical shells. The Rayleigh-Ritz method is used to solve the equations by assuming a double Fourier expansion of the displacements with trigonometric coordinate functions. Numerical results for postbuckling response of axially compressed multilayer cylinders with simply supported edge conditions are presented for different values of shell imperfections. 1992 American Institute of Aeronautics and Astronautics, Inc., All rights reserved.

authors

• Reddy, Junuthula

published proceedings

• AIAA JOURNAL

author list (cited authors)

• REDDY, J. N., & SAVOIA, M.

citation count

• 49

complete list of authors

• REDDY, JN||SAVOIA, M

publication date

• August 1992

publisher

• American Institute of Aeronautics and Astronautics (AIAA)  Publisher

keywords

• 40 Engineering
• 4001 Aerospace Engineering
• 4012 Fluid Mechanics And Thermal Engineering

Digital Object Identifier (DOI)

• 10.2514/3.11193

start page

• 2148

end page

• 2154

volume

• 30

issue

• 8

URL

• http://dx.doi.org/10.2514/3.11193