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Dynamic Design of Compound Shell Structures of Revolution Under Nonstationary Loads*

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International Applied Mechanics Aims and scope

A technique for solving dynamic problems of the behavior of compound shell structures (solving the equations of motion subject to appropriate boundary and initial conditions) is developed. The structurally orthotropic model of a three-layer shell structure with a cellular core is used, for which the integral values of the elastic modulus and Poisson’s ratios are determined experimentally. Numerical algorithms are developed, and the corresponding problems of mathematical theory of elasticity are solved. The numerical results are analyzed.

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Authors and Affiliations

  1. S. P. Timoshenko Institute of Mechanics, National Academy of Sciences of Ukraine, 3 Nesterova Str., Kyiv, 03057, Ukraine

    P. Z. Lugovoi, V. F. Meish, Yu. A. Meish & S. P. Orlenko

Authors
  1. P. Z. Lugovoi
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  2. V. F. Meish
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  3. Yu. A. Meish
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  4. S. P. Orlenko
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Corresponding author

Correspondence to P. Z. Lugovoi.

Additional information

Translated from Prikladnaya Mekhanika, Vol. 56, No. 1, pp. 32–43, January–February 2020.

* This study was sponsored by the budget program “Support for Priority Areas of Scientific Research” (KPKVK 6541230).

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Lugovoi, P.Z., Meish, V.F., Meish, Y.A. et al. Dynamic Design of Compound Shell Structures of Revolution Under Nonstationary Loads*. Int Appl Mech 56, 22–32 (2020). https://doi.org/10.1007/s10778-020-00993-0

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  • DOI: https://doi.org/10.1007/s10778-020-00993-0

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