Numerical implementation of Richardson extrapolation for dynamic problems of multilayer cylindrical shells
DOI:
https://doi.org/10.15587/1729-4061.2025.345897Keywords:
multilayer shells, forced vibrations, unsteady loading, numerical methods, Richardson extrapolationAbstract
This study considers forced vibrations of a heterogeneous elastic structure in the form of a multilayer cylindrical shell consisting of rigidly connected layers and reinforced with discrete ring elements.
A mathematical model of vibrations of an elastic heterogeneous structure under the action of a non-stationary load has been constructed. The stressed-strained state of a multilayer cylindrical shell with discrete ring ribs was investigated using the geometrically nonlinear theory of Timoshenko-type shells and rods. The presence of a complex right-hand side and discontinuous coefficients in the spatial coordinates in the hyperbolic equations of vibrations of a heterogeneous elastic cylindrical shell (at the locations of the reinforcing ribs) necessitated the use of numerical methods for solving them. A numerical algorithm using Richardson extrapolations has been proposed for studying the constructed model.
For example, a three-layer reinforced cylindrical shell is considered, taking into account the discreteness of the ribs' placement under dynamic loading with rigidly clamped ribs. The proposed numerical algorithm has made it possible to investigate the stressed-strained state of a three-layer reinforced elastic structure of a cylindrical type at any given moment in time. A comparative analysis of the numerical results of the calculations revealed that, according to the standard approach, the discrepancy in the deflection values for n = 40 and n = 160 reached 31%, for n = 80 and n = 160 it was about 5%, according to Richardson's approach for n = 40 ÷ 80 and the standard approach for n = 160, this difference was about 1%.
A distinctive feature of this study is the use of Richardson extrapolation to identify the stressed-strained state of a three-layer reinforced cylindrical shell, which made it possible to increase the accuracy of the solution to the dynamic problem without reducing the calculation step.
The study's results reported in this work could be used for investigating unsteady vibrations of shell structures at research and engineering organizations
References
- Ismoil, S., Muhsin, T., Isroil, K., Nurali, E. (2025). Non-axisymmetric stationary waves in a viscoelastic three-layered cylindrical shell. Journal of Engineering Mathematics, 151 (1). https://doi.org/10.1007/s10665-025-10440-z
- Ellouz, H., Jrad, H., Bouhamed, A., Wali, M., Dammak, F. (2024). Non-linear Behavior of Smart Magneto-Electro-Elastic Hyperboloid Shell. Advances in Materials, Mechanics and Manufacturing III, 1–10. https://doi.org/10.1007/978-3-031-57324-8_1
- Zhao, T., Bayat, M. J., kalhori, A., Asemi, K. (2024). Free vibration analysis of functionally graded multilayer hybrid composite cylindrical shell panel reinforced by GPLs and CNTs surrounded by Winkler elastic foundation. Engineering Structures, 308, 117975. https://doi.org/10.1016/j.engstruct.2024.117975
- Heidari, Y., Irani Rahaghi, M., Arefi, M. (2022). Buckling analysis of FG cylindrical nano shell integrated with CNTRC patches. Waves in Random and Complex Media, 35 (4), 7287–7308. https://doi.org/10.1080/17455030.2022.2086320
- Meish, V. F., Meish, Yu. A., Arnauta, N. V. (2019). Numerical Analysis of Nonstationary Vibrations of Discretely Reinforced Multilayer Shells of Different Geometry. International Applied Mechanics, 55 (4), 426–433. https://doi.org/10.1007/s10778-019-00962-2
- Meish, V. F., Meish, Yu. A., Belova, M. A. (2020). Nonstationary Dynamics of Elliptic Isotropic Conical Shells Under Distributed Loads*. International Applied Mechanics, 56 (4), 424–431. https://doi.org/10.1007/s10778-020-01026-6
- Meish, Y., Belova, M., Maiborodina, N., Gerasymenko, V. (2024). Determining the effect of longitudinal stiffeners on the deformation of multilayer ellipsoidal shells under non-stationary loads. Eastern-European Journal of Enterprise Technologies, 4 (7 (130)), 78–88. https://doi.org/10.15587/1729-4061.2024.310241
- Semenyuk, N. P., Zhukova, N. B. (2020). Stability of a Sandwich Cylindrical Shell with Core Subject to External Pressure and Pressure in the Inner Cylinder*. International Applied Mechanics, 56 (1), 40–53. https://doi.org/10.1007/s10778-020-00995-y
- Avramov, K., Uspensky, B. (2022). Nonlinear vibrations of doubly curved composite sandwich shells with FDM additively manufactured flexible honeycomb core. Acta Mechanica, 234 (3), 1183–1210. https://doi.org/10.1007/s00707-022-03426-w
- Attia, A., Berrabah, A. T., Bourada, F., Bousahla, A. A., Tounsi, A., Ghazwani, M. H., Alnujaie, A. (2024). Bending Analysis of Laminated Composite and Sandwich Cylindrical Shells Using Analytical Method and Ansys Calculations. Mechanics of Composite Materials, 60 (1), 33–48. https://doi.org/10.1007/s11029-024-10173-7
- Zhang, H., Gao, Y., He, D., Yang, W. (2022). Free vibration and buckling analysis of composite laminated shells using the refined zigzag theory. Journal of Theoretical and Applied Mechanics, 435–448. https://doi.org/10.15632/jtam-pl/150847
- Gao, Y., Zhang, H., Yang, W., He, D. (2022). A new bending model for composite laminated shells based on the refined zigzag theory. Archive of Applied Mechanics, 92 (10), 2899–2915. https://doi.org/10.1007/s00419-022-02210-5
- Salenko, O., Drahobetskyi, V., Symonova, A., Onishchenko, E., Kostenko, A., Tsurkan, D., Vasiukov, D. (2024). Damage Behavior of Multilayer Axisymmetric Shells Obtained by the FDM Method. Journal of Engineering Sciences, 11 (1), D27–D35. https://doi.org/10.21272/jes.2024.11(1).d4
- Smetankina, N. V., Merkulova, A. I., Postnyi, O. V., Merkulov, D. O., Misura, S. Yu. (2021). Optimal Design of Layered Cylindrical Shells with Minimum Weight Under Impulse Loading. 2021 IEEE 2nd KhPI Week on Advanced Technology (KhPIWeek), 506–509. https://doi.org/10.1109/khpiweek53812.2021.9569982
- Litot, O., Man’ko, T. (2021). Methods of graphic construction of the process of manufacturing the power shell of composite fuel tanks. Journal of Rocket and Space Technology, 28 (4), 75–81. https://doi.org/10.15421/452010
- Senkoua, Y., Ngak, F. P. E., Meuyou, H. H., Ntamack, G. E. (2024). Numerical Investigation of the Vibroacoustic Behavior of Carbon Nanotube Reinforced Doubly-Curved Multilayer Composite Shells. Mechanics of Solids, 59 (8), 4003–4026. https://doi.org/10.1134/s0025654424605093
- Ma, J., Gao, H. (2024). Free vibration analysis of hybrid laminated thin-walled cylindrical shells containing multilayer FG-CNTRC plies. Acta Mechanica, 235 (12), 7711–7731. https://doi.org/10.1007/s00707-024-04082-y
- Kjelgaard Mikkelsen, C. C., López-Villellas, L. (2025). The Need for Accuracy and Smoothness in Numerical Simulations. Parallel Processing and Applied Mathematics, 3–16. https://doi.org/10.1007/978-3-031-85697-6_1
- Prince, P. A., Govindarao, L., Elango, S. (2025). Richardson Extrapolation for Singularly Perturbed Fredholm Integro Differential Equations. International Journal of Mathematical, Engineering and Management Sciences, 10 (6), 2023–2039. https://doi.org/10.33889/ijmems.2025.10.6.094
Downloads
Published
How to Cite
Issue
Section
License
Copyright (c) 2025 Yuliia Meish, Maryna Belova, Nataliia Arnauta, Nataliia Maiborodina, Vіacheslav Gerasymenko

This work is licensed under a Creative Commons Attribution 4.0 International License.
The consolidation and conditions for the transfer of copyright (identification of authorship) is carried out in the License Agreement. In particular, the authors reserve the right to the authorship of their manuscript and transfer the first publication of this work to the journal under the terms of the Creative Commons CC BY license. At the same time, they have the right to conclude on their own additional agreements concerning the non-exclusive distribution of the work in the form in which it was published by this journal, but provided that the link to the first publication of the article in this journal is preserved.
A license agreement is a document in which the author warrants that he/she owns all copyright for the work (manuscript, article, etc.).
The authors, signing the License Agreement with TECHNOLOGY CENTER PC, have all rights to the further use of their work, provided that they link to our edition in which the work was published.
According to the terms of the License Agreement, the Publisher TECHNOLOGY CENTER PC does not take away your copyrights and receives permission from the authors to use and dissemination of the publication through the world's scientific resources (own electronic resources, scientometric databases, repositories, libraries, etc.).
In the absence of a signed License Agreement or in the absence of this agreement of identifiers allowing to identify the identity of the author, the editors have no right to work with the manuscript.
It is important to remember that there is another type of agreement between authors and publishers – when copyright is transferred from the authors to the publisher. In this case, the authors lose ownership of their work and may not use it in any way.





