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Considering Local Buckling Effects for the Optimization of Stiffened Composite Panels

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IUTAM Symposium on Optimization of Mechanical Systems

Part of the book series: Solid Mechanics and its Applications ((SMIA,volume 43))

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Abstract

The present paper addresses the optimal layout of stiffened fibre composite plates (Fig. 1) considering buckling constraints; these plates are increasingly applied in many fields of engineering (air- and spacecraft technology, automotive industries, boatbuilding etc.)

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References

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Author information

Authors and Affiliations

  1. Research Center for Multidisciplinary Analyses and Applied Structural Optimization FOMAAS, University of Siegen, D-57068, Siegen, Germany

    Hans A. Eschenauer & Christof M. Weber

Authors
  1. Hans A. Eschenauer
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  2. Christof M. Weber
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Editor information

Editors and Affiliations

  1. Department of Machine Dynamics, Technical University of Cottbus, Germany

    D. Bestle

  2. Institute B of Mechanics, University of Stuttgart, Germany

    W. Schiehlen

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© 1996 Kluwer Academic Publishers

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Eschenauer, H.A., Weber, C.M. (1996). Considering Local Buckling Effects for the Optimization of Stiffened Composite Panels. In: Bestle, D., Schiehlen, W. (eds) IUTAM Symposium on Optimization of Mechanical Systems. Solid Mechanics and its Applications, vol 43. Springer, Dordrecht. https://doi.org/10.1007/978-94-009-0153-7_10

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  • DOI: https://doi.org/10.1007/978-94-009-0153-7_10

  • Publisher Name: Springer, Dordrecht

  • Print ISBN: 978-94-010-6555-9

  • Online ISBN: 978-94-009-0153-7

  • eBook Packages: Springer Book Archive

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