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Optimization of thin shell structures subjected to thermal loading

  • Li, Qing (Department of Aeronautical Engineering, Building J07, Engineering Faculty, University of Sydney) ;
  • Steven, Grant P. (Department of Aeronautical Engineering, Building J07, Engineering Faculty, University of Sydney) ;
  • Querin, O.M. (Department of Aeronautical Engineering, Building J07, Engineering Faculty, University of Sydney) ;
  • Xie, Y.M. (Faculty of Engineering and Science, Victoria University of Technology)
  • Published : 1999.04.25

Abstract

The purpose of this paper is to show how the Evolutionary Structural Optimization (ESO) algorithm developed by Xie and Steven can be extended to optimal design problems of thin shells subjected to thermal loading. This extension simply incorporates an evolutionary iterative process of thermoelastic thin shell finite element analysis. During the evolution process, lowly stressed material is gradually eliminated from the structure. This paper presents a number of examples to demonstrate the capabilities of the ESO algorithm for solving topology optimization and thickness distribution problems of thermoelastic thin shells.

Keywords

References

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