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For such reasons, CNTs are used in some areas of the defense industry, especially in rocket, aerospace and aviation industries, where high-precision computations are required [ 6 , 7 , 8 ]. Among various problems is the linear and nonlinear vibration behavior of composite shell structures involving the presence of different distributions of CNTs. Composite shells, indeed, can include uniform or nonuniform patterns of CNTs, depending on the desired mechanical properties of the structures [ 9 , 10 , 11 , 12 , 13 , 14 , 15 , 16 , 17 , 18 , 19 , 20 , 21 , 22 , 23 , 24 ].

In this framework, a pioneering work on the nonlinear vibrations of composite shell structures was represented by [ 9 ], which considered a linear distribution of CNTs within the material. Following this work, some linear and nonlinear free vibration problems were proposed in [ 10 , 11 , 12 , 13 , 14 , 15 , 16 , 17 ] and [ 18 , 19 , 20 , 21 , 22 , 23 , 24 ], respectively, for unconstrained shallow shells and panels reinforced by CNTs, while proposing different numerical methods to solve the related problems.

The technological evolution of artificial materials and their manufacturing has expanded the application areas for such materials, improving the interest towards even more complicated and coupled problems, as well as the possible interactions of a structural member with its surrounding medium.

Composite CNT-based shell structures resting on elastic foundations can be found in different civil and mechanical engineering applications, in nuclear power plants, etc. Among different possibilities to model an elastic foundation, the Pasternak and Winkler models are two common ways of describing its mechanical behavior, based on a different number of input parameters [ 25 , 26 ].

When modeling the vibrations of structural members containing CNTs, it is important to study the effect of the reinforcement phase and elastic foundations on the frequency—amplitude relationships. Up to date, most works from the literature have been devoted to the solution of linear vibration problems, by means of different numerical techniques [ 27 , 28 , 29 , 30 , 31 , 32 , 33 , 34 , 35 ].

More specifically, Tornabene et al. The same numerical approach was successfully proposed in [ 28 ] to study the vibration response of functionally graded carbon nanotube reinforced composite FG-CNTRC spherical shells on an elastic foundation. Shen and He [ 31 ] performed a large amplitude vibration analysis of FG-CNTRC double-curved panels on elastic foundation by applying a two-step perturbation approach, as also implemented in [ 32 ] to analyze the large amplitude vibration of FG shallow arches on a nonlinear elastic foundation.

A further linear formulation was proposed by Sobhy and Zenkour [ 33 ] to study the vibrations of FG graphene platelet reinforced composite double-curved shallow shells on an elastic foundation; Sofiyev et al.

Despite the considerable attention paid by the scientific literature to the linear vibration of shell structures, the nonlinear vibrations of CNT shallow shells resting on elastic foundations have not been adequately investigated.

In this context, this paper aims to study the nonlinear free vibration behavior of thin-walled shell structures reinforced with CNTs and resting on an elastic Winkler- or Pasternak-type foundation, while proposing a Grigolyuk method to handle the problem. The organization of the rest of the paper is as follows: Section 2 recalls the basic theoretical aspects for both the shell-foundation interaction and nonlinear structural problem.

Section 3 illustrates the analytical methodology applied to solve the problem, whose numerical investigation is presented and discussed in Section 4 , while Section 5 closes the work with main comments and remarks.

Let us consider a composite spherical and hyperbolic paraboloidal hypar shallow shell reinforced with CNTs with length a , width b , thickness h and curvature radii R 1 and R 2 , respectively see Figure 1 a,b. The Cartesian coordinate system x 1 , x 2 , x 3 is here assumed to define the shell geometry in its length, width and thickness direction, respectively.

As also shown in Figure 1 , both the spherical and hypar shallow shells are immersed in an elastic WPF, here modeled as follows [ 25 , 26 ]:. The density can be defined as. The strain field on the reference surface is governed by the following kinematic relations [ 36 ]. By using relations 1 , 2 , 5 and 6 , the nonlinear governing equations for doubly curved shallow shells reinforced with a linear pattern of CNTs and resting on a WPF, attain the following form.

Moreover, u i j are defined as. In what follows, we provide an analytical solution to the problem of a simply-supported doubly-curved shell. Thus, the structural deflection can be approximated as [ 21 , 36 ]. By substitution of Equation 13 into Equation 9 , we get the following expression for the stress function F. Thus, by applying the Grigolyuk method [ 37 ], one obtains. After integrating this last relation, we obtain the following nonlinear amplitude—frequency dependence.

As visible from Table 1 , our results match very well predictions from [ 38 ], for both spherical and hypar shell members; this proves the reliability and consistency of the proposed formulation.

Table 2 summarizes the results based on different approaches, with a consistent agreement between our formulation and findings from [ 39 , 40 ]. The influence of different CNT patterns is more pronounced for unconstrained hypar shells, with the largest difference being approximately 1. A pronounced effect of CNT patterns is also observed for both shallow shells in the presence, or not, of a PF, which is quantified as a percentage by 4.

It is also noticeable that this ratio becomes higher for hypar shells with and without the PF, as spherical and hypar shells are compared. The most pronounced increase seems to be approximately equal to 2. A monotonic decrease is differently observed for hypar shells. Once the basic relations for composite shallow shells reinforced by CNTs on WPFs are established, the partial differential equations of nonlinear motion are derived, taking into account the von Karman nonlinearity.

These equations are solved here by means of the Galerkin and Grigolyuk methods in terms of linear and nonlinear free vibrations for inhomogeneous nanocomposite construction members such as plates, panels, spherical and hyperbolic paraboloidal hypar shallow shells. The accuracy of the results in the current study has been confirmed by means of a successful comparison with reliable predictions from the literature. After this preliminary validation, a detailed numerical analysis is performed, including the effect of nonlinearity, CNT patterns and volume fraction on the nonlinear frequency response.

Based on a large systematic investigation, the analytical results could serve as valid benchmark solutions for further computational studies on the topic, as well as for design purposes.

Among the most useful insights, it is found that the variation rate of NLFVFs for both shallow shells with linearly patterned CNTs decreases, while remaining constant for different elastic foundations with an increased stiffness. Conceptualization, A.

All authors have read and agreed to the published version of the manuscript. Nanomaterials Basel. Published online Aug Yang Tse Cheng, Academic Editor. Author information Article notes Copyright and License information Disclaimer. Received Jul 21; Accepted Aug This article has been cited by other articles in PMC. Abstract In this work, we discuss the free vibration behavior of thin-walled composite shell structures reinforced with carbon nanotubes CNTs in a nonlinear setting and resting on a Winkler—Pasternak Foundation WPF.

Keywords: CNT, elastic foundations, nonlinear free vibration, nonlinear frequency, shallow shell structures. Introduction The fast development of nanotechnology in recent years has encouraged the production of nanotubes, increasing their application in many engineering areas.

Theoretical Formulation 2. Description of Shell-Foundation Interaction Model Let us consider a composite spherical and hyperbolic paraboloidal hypar shallow shell reinforced with CNTs with length a , width b , thickness h and curvature radii R 1 and R 2 , respectively see Figure 1 a,b. Open in a separate window. Figure 1. Figure 2. Solution Procedure In what follows, we provide an analytical solution to the problem of a simply-supported doubly-curved shell.

Figure 3. Figure 4. Figure 5. Figure 6. Author Contributions Conceptualization, A. Funding This research received no external funding.

Conflicts of Interest The authors declare no conflict of interest. References 1. Iijima S. Single-shell carbon nanotubes of 1-nm diameter. Cell Biol.

Xie S. Mechanical and physical properties on carbon nanotube. Curtin W. CNT-reinforced ceramics and metals. Esawi A. Carbon nanotube reinforced composites: Potential and current challenges.

Sofiyev A. Silvestre J. Polymer nanocomposites for structural applications: Recent trends and new perspectives. Park S. Recent Patents Nanotechnol. Liew K. Participating sites will be required to sign on at EST and be prepared to go to p. We will validate connectivity as part of the site slate process. A Community based group with representation from the Emergency Management disciplines. Exercise Documents: Exercise documents for this event will be provided to the lead remote site POC as soon as the final list is announced.

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