The interlaminar stresses in laminated composite cylindrical shell strips under dynamic transverse loading are studied here within the purview of a first order shear deformation theory. The dynamic equations of equilibrium are solved by a combination of Navier's approach and a Laplace transform tech
Analysis of cylindrical shells under patch loading
β Scribed by Lin, J. S. ;Hourani, M. ;Gould, P. L. ;Harmon, T. G. ;Han, K. J.
- Publisher
- Wiley (John Wiley & Sons)
- Year
- 1986
- Tongue
- English
- Weight
- 549 KB
- Volume
- 2
- Category
- Article
- ISSN
- 0748-8025
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β¦ Synopsis
The object of this study is to predict the peak values of the stress resultants and couples in a relatively thick cylindrical shell under a concentrated local loading in order to guide the design of a large-scale reinforced concrete test specimen. Four finite element programs, SHORE-111, two versions of RONALD, and ANSYS, were employed here. The SHORE-I11 and RONALD analyses considered a complete cantilevered cylinder, while the ANSYS model treated a cylindrical panel free along the curved edge and constrained in various ways along the longitudinal edge. Comprehensive comparative results are provided for the linear elastic loading case, which indicate the magnitude and attenuation of concentrated loading effects on cylindrical shells and panels.
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## Abstract The accuracy of stability analysis depends on the accuracy of both the element stiffness matrix and geometry stiffness matrix. Therefore, when carrying out the stability analysis of thin cylindrical shells using the finite element methods will require, firstly, a refined nonβconforming
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