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Finite Element Model for Layered Plates/Shells

In: Numerical Techniques for Engineering Analysis and Design

Author

Listed:
  • M. G. Rajendran

    (Psg College of Technology)

  • S. Rajasekaran

    (Psg College of Technology)

  • K. Jawahar Reddy

    (Psg College of Technology)

  • S. Valliammai

    (Psg College of Technology)

Abstract

Summary The sixteen term complete 3rd order Hermitian polynomial initiated by Bogner, Fox and Schmit [3] is used to develop the finite element model for static and classical buckling analyses of layered rectangular plates made of composite materials. The concept of Isoparametric elements with independent rotational and transverse degrees of freedom originally introduced by Ahmad, Irons and Zienkiewicz [1], is extended to develop the finite element models for static and classical buckling analyses of layered axisymmetric shells as well as layered plate/shell. Computer programs for the above models suitable for microcomputer have been developed and some practical problems have been solved and compared with the available results.

Suggested Citation

  • M. G. Rajendran & S. Rajasekaran & K. Jawahar Reddy & S. Valliammai, 1987. "Finite Element Model for Layered Plates/Shells," Springer Books, in: G. N. Pande & J. Middleton (ed.), Numerical Techniques for Engineering Analysis and Design, chapter 0, pages 485-492, Springer.
    • Handle: RePEc:spr:sprchp:978-94-009-3653-9_54
    DOI: 10.1007/978-94-009-3653-9_54
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