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A shear deformable theory of laminated composite shallow shell-type panels and their response analysis II: Static response

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In the second part of this paper, by using the static counterparts of the governing equations derived in [1], the static response of shallow composite shell-type panels subjected to a sinusoidal transverse load is investigated. The numerical applications, encompassing a large number of boundary conditions and various lamination schemes, allow one to obtain some conclusions which are formulated in the paper.

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Reference

  1. Librescu, L., Khdeir, A. A., Frederick, D.: A shear deformable theory of laminated composite shallow shell-type panels and their response analysis. Part I: Free vibration and buckling. Acta Mechanica76, 1–33 (1989).

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Authors and Affiliations

  1. Department of Engineering Science and Mechanics, Virginia Polytechnic Institute and State University, 24061, Blacksburg, VA, USA

    A. A. Khdeir, L. Librescu & D. Frederick

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  1. A. A. Khdeir
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  2. L. Librescu
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  3. D. Frederick
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Khdeir, A.A., Librescu, L. & Frederick, D. A shear deformable theory of laminated composite shallow shell-type panels and their response analysis II: Static response. Acta Mechanica 77, 1–12 (1989). https://doi.org/10.1007/BF01379740

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  • DOI: https://doi.org/10.1007/BF01379740

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