A Novel Trigonometric High-Order Shear Deformation Theory for Free Vibration and Buckling Analysis of Carbon Nanotube Reinforced Beams Resting on a Kerr Foundation ^†

Abstract

This research is concerned with the free vibration and buckling analysis of carbon nanotube-reinforced beams (CNT-RBs) using a novel high-order shear deformation theory (HSDT). The current HSDT is modeled by a trigonometric function without a shear correction factor, and the displacement field has only four variables. Several different carbon nanotube distributions, including two uneven CNT distributions (X-CNT and O-CNT), are considered. The mixture rule is applied to express the effective material properties of carbon nanotube-reinforced beams. The CNTR beams are rested on two springs and a shear layer (Kerr foundation). Hamilton’s principle is employed to derive the governing equations, which are then solved using the Navier technique. The current theory and several parameter effects are studied and validated in comparison to benchmark studies and theories. The main purpose of this study is to enhance understanding of high-order shear theories, such as third order, sinusoidal, exponential, etc. In this context, our theory yields excellent results when compared to other theories. The difference between our theory and the exact solution is so minimal that it is superior to other theories. The second part of the study focuses on investigating the distribution of carbon nanotubes to enhance understanding. This knowledge can assist panel manufacturers in determining the appropriate distribution shape. Our results indicate that the third distribution (X-CNT) significantly influences mechanical behavior, unlike the first and second distributions (UD-CNT and O-CNT).

1. Introduction

Emerging materials like carbon nanotube-reinforced composites have a huge potential for use in high-tech industries, especially those like aerospace that demand advanced mechanical properties. Quality, sturdiness, dependability, and overall effectiveness can all be enhanced by adding carbon nanotubes to conventional matrices [1].

Recently, numerous research studies have focused on analyzing the behavior of beams constructed from carbon nanotube-reinforced composites. We will mention some of these studies in references [2,3,4,5,6].

In the context of advancing our understanding and obtaining results related to high-order shear deformation theories, which constitutes the primary objective of this paper, several prior theories were employed. These include the third-order theory developed by Reddy [7], the sinusoidal HSD theory by Touratier [8], the exponential HSD theory introduced by Karama et al. [9], the hyperbolic HSD theory by Kenanda et al. [10], and the trigonometric-exponential HSD theory, also developed by Kenanda et al. [11,12].

This article will concentrate solely on the key points and fundamental equations that elucidate the novelty presented in this work. Detailed specifics will not be provided in this article, as the complete scope of our work will be published in an independent journal following our participation in the conference.

2. Material Properties of CNTR Beams

Take into account the reference frame consisting of coordinates (x, y, and z) for a CNTR beam, characterized by its dimensions: width (b), length (L), and thickness (h). This beam is mounted on the Kerr foundation as depicted in Figure 1.

Based on the rule of mixture, material properties such as Young’s modulus, mass density, and Poisson’s ratio can be defined as:

$$E_{11}={\eta }_1{V}_{CNT}{E}_{11}^{CNT}+V_m{E}^m$$

(1a)

$$\frac{{\eta }_2}{E_{22}}=\frac{V_{CNT}}{E_{22}^{CNT}}+\frac{V_m}{E^m}$$

(1b)

$$\frac{{\eta }_3}{G_{22}}=\frac{V_{CNT}}{G_{12}^{CNT}}+\frac{V_m}{G^m}$$

(1c)

$$\nu =V_{CNT}{\nu }^{CNT}+V_m{\nu }^m$$

(1d)

$$\rho =V_{CNT}{\rho }^{CNT}+V_m{\rho }^m$$

(1e)

$$V_{CNT}+V_m=1$$

(1f)

where ($E_{11},E_{22},G_{22},\rho ,\nu$) are the homogenized material properties of the composite and ($V_m\begin{array}{c}\mathrm{and}\end{array}{V}_{CNT}$) are the volume fractions of matrix and carbon nanotubes, respectively. The latter is determined through the equations shown in

Table 1. The volume fraction of several patterns of CNT distribution.

Patterns of CNT Distribution	${\mathit{V}}_{\mathit{C}\mathit{N}\mathit{T}}$	${\mathit{V}}_{\mathit{C}\mathit{N}\mathit{T}}^{*}$
UD-CNT	$V_{CNT}=V_{CNT}^{*}$	$V_{CNT}^{*}=\frac{W_{CNT}}{W_{CNT}+\left({\rho }^{CNT}/{\rho }^m\right)\left(1-W_{CNT}\right)}$
O-CNT	$V_{CNT}=2\left(1-2\frac{\left|z\right|}{h}\right)V_{CNT}^{*}$
X-CNT	$V_{CNT}=4\frac{\left|z\right|}{h}{V}_{CNT}^{*}$

In which ($W_{CNT}$) denotes the mass fraction of CNT.

, according to the appropriate distribution. In addition, (${\eta }_1,{\eta }_2,{\eta }_3$) are efficiency parameters of carbon nanotubes and matrix.

3. Mathematical Formulation

Displacement and Strain Field

High-order shear deformation beam theory provides the displacements along the x and z directions as follows:

$$\begin{array}{l}u\left(x,z,t\right)=u\left(x,t\right)-z\frac{\partial w\left(x,t\right)}{\partial x}+F\left(z\right)\varphi \left(x,t\right)\\ w\left(x,z,t\right)=w\left(x,t\right)\end{array}$$

(2a)

In which

$$\varphi \left(x,t\right)=\left(\frac{\partial w}{\partial x}-\phi \right)$$

(2b)

where (u and w) are the displacements along the x and z axes of the CNTR beam, and ($\phi$) presents the rotation of the cross section. In which $F\left(z\right)$ is shape function that expresses the transverse shear stress distribution in a parabolic manner called the high-order shear theory. There are many functions that have been developed in this regard. We show the most important of them in

Table 2. Present the most important beam theories.

Theories	The Shape Function
	F(z)
Euler–Bernoulli beam theory (classical beam theory)	$F\left(z\right)=0$
Timoshenko beam theory (first-order shear theory)	$F\left(z\right)=z$
Third-order shear deformation theory [7] (high-order theory)	$F\left(z\right)=z\left(1-\frac{4z^2}{3h^2}\right)$
Sinusoidal shear deformation theory [8] (high-order theory)	$F\left(z\right)=\frac{h}{\pi }sin\left(\frac{\pi z}{h}\right)$
Exponential shear deformation theory [9] (high-order theory)	$F\left(z\right)=z\begin{array}{c}exp\end{array}\left(-2{\left(\frac{z}{h}\right)}^2\right)$
Trigonometric shear deformation theory (Present) (high-order theory)	$\begin{array}{l}F\left(z\right)=\frac{{\theta }_{1}h\left(arctan\left(sinh\left(z/h\right)\right)+sech\left(z/h\right)tanh\left(z/h\right)\right)}{2sec{h}^3\left(1/2\right)}-{\theta }_{1}z\\ {\theta }_1=\frac{sec{h}^3\left(1/2\right)}{1-sec{h}^3\left(1/2\right)}\end{array}$

.

According to Equation (2a,b), the strain field can be obtained in the following form:

$$\begin{array}{l}{\epsilon }_{xx}=\frac{\partial u}{\partial x}-z\frac{{\partial }^{2}w}{\partial x^2}+F\left(z\right)\frac{\partial \varphi }{\partial x}\\ {\gamma }_{xz}=\frac{dF}{dz}\varphi \end{array}$$

(3)

where (${\epsilon }_{xx}\begin{array}{c}\mathrm{and}\end{array}{\gamma }_{xz}$) are the components of the strain tensor.

4. Results and Discussion

In this section, our focus is on assessing the reliability and efficiency of the present trigonometric high-order shear deformation theory by contrasting it with various established theories. At the same time, we are investigating how the different CNT distributions influence the behavior of the CNRT (Carbon Nanotube Reinforced) beam. The mechanical characteristics employed in this section are outlined in

Table 3. Present the material properties of CNT and matrix.

Material Properties	CNT	Material Properties	Matrix
$E_{11}^{CNT}\left(\mathrm{GPa}\right)$	600	$E_{}^M\left(\mathrm{GPa}\right)$	2.5
$E_{22}^{CNT}\left(\mathrm{GPa}\right)$	10	${\rho }^M\left(\mathrm{GPa}\right)$	1190
$G^{CNT}\left(\mathrm{GPa}\right)$	17.2	${\nu }^M$	0.3
${\rho }^{CNT}\left(\mathrm{GPa}\right)$	1400
${\nu }^{CNT}$	0.19

.

Table 4. The first non-dimensional fundamental frequency ($\overline{\omega }=\omega L\sqrt{{\rho }^M/E^M}$) for three patterns of CNT distribution (UD-CNT, O-CNT, and X-CNT) and two values of ($V_{CNT}^{*}$) with (L/h = 15).

Theories	Patterns of CNT Distribution (${\mathit{V}}_{\mathit{C}\mathit{N}\mathit{T}}^{*}=0.17$)
	UD-CNT	O-CNT	X-CNT
Euler–Bernoulli beam theory [3]	1.3868	0.9906	1.6877
Timoshenko beam theory [3]	1.1977	0.9145	1.3796
Third-order shear deformation theory [3]	1.1983	0.9088	1.3760
Present high-order shear deformation theory	1.1988	0.9082	1.3768
	Patterns of CNT distribution (${\mathit{V}}_{\mathit{C}\mathit{N}\mathit{T}}^{*}=0.28$)
	UD-CNT	O-CNT	X-CNT
Euler–Bernoulli beam theory [3]	1.7392	1.2391	2.1153
Timoshenko beam theory [3]	1.4348	1.1176	1.6409
Third-order shear deformation theory [3]	1.4361	1.1150	1.6113
Present high-order shear deformation theory	1.4368	1.1146	1.6108

presents the first non-dimensional fundamental frequency ($\overline{\omega }=\omega L\sqrt{{\rho }^M/E^M}$) for three patterns of CNT distribution (UD-CNT, O-CNT, and X-CNT) and two values of ($V_{CNT}^{*}$) with (L/h = 15). It can be seen from the table that the results of our theory are largely consistent with the third-order shear deformation theory results. In addition, our theory gives better results than classical beam and first-order shear theories in describing mechanical behavior. We also notice from the table that the effect of the third distribution (X-CNT) affects the frequencies significantly compared to the first and second distributions (UD-CNT and O-CNT). Moreover, an increase in the value of ($V_{CNT}^{*}$) causes an increase in fundamental frequencies.

5. Conclusions

The current theory outlines a novel trigonometric function for characterizing shear stress distribution, eliminating the need for a shear correction factor. This theory successfully meets the zero traction boundary conditions on both the upper and lower surfaces of the CNTR beam. The trigonometric shear deformation theory involves only four variables in its displacement field. Compared to other shear deformation theories, the proposed hyperbolic theory offers a more comprehensive and accurate representation of transverse shear stress, resulting in superior outcomes when describing the mechanical behavior of CNTR beam.