Author:
Lakshmikantham C.,Gerard G.
Abstract
SummaryIn this paper a generalised presentation for symmetrically stiffened orthotropic cylinders under compression is developed, based on a linear orthotropic stability theory of cylinders. Similarities and differences in the minimum weight behaviour of stiffened cylindrical shells and flat transversely-stiffened wide columns are investigated in some detail to provide a satisfactory physical picture. The concluding results provide a comparative evaluation of various forms of stiffening systems for cylindrical shells under compression.
Publisher
Cambridge University Press (CUP)
Reference11 articles.
1. Minimum weight design of symmetrically stiffened orthotropic cylinders under axial compression;Gerard,1966
2. Optimum structural design concepts for aerospace vehicles.
3. General instability of orthotropically stiffened cylinders under axial compression;Milligan;AIAA Journal,1966
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