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. 2025 Jan 3;20(1):e0315505. doi: 10.1371/journal.pone.0315505

Noether and partial Noether approach for the nonlinear (3+1)-dimensional elastic wave equations

Akhtar Hussain 1,*, M Usman 2, Fiazuddin Zaman 1, Ahmed M Zidan 3, Jorge Herrera 4
Editor: Timon Idema5
PMCID: PMC11698396  PMID: 39752464

Abstract

The Lie group method is a powerful technique for obtaining analytical solutions for various nonlinear differential equations. This study aimed to explore the behavior of nonlinear elastic wave equations and their underlying physical properties using Lie group invariants. We derived eight-dimensional symmetry algebra for the (3+1)-dimensional nonlinear elastic wave equation, which was used to obtain the optimal system. Group-invariant solutions were obtained using this optimal system. The same analysis was conducted for the damped version of this equation. For the conservation laws, we applied Noether’s theorem to the nonlinear elastic wave equations owing to the availability of a classical Lagrangian. However, for the damped version, we cannot obtain a classical Lagrangian, which makes Noether’s theorem inapplicable. Instead, we used an extended approach based on the concept of a partial Lagrangian to uncover conservation laws. Both techniques account for the conservation laws of linear momentum and energy within the model. These novel approaches add an application of variational calculus to the existing literature. This offers valuable insights and potential avenues for further exploration of the elastic wave equations.

1 Introduction

Elasticity [1] is a fundamental concept in many areas of science and engineering such as solid mechanics, material science, and structural engineering. Common examples of elastic media include rubber, metals, springs, and many other materials that can undergo temporary deformation and restore their original shapes when subjected to mechanical loads. In an elastic medium, when stress (force per unit area) is applied, the material undergoes reversible and recoverable deformation, which means that it can return to its initial state after the force is removed. In the case of small deformations, the relationship between the stress and strain (rate of deformation) is linear. However, when the deformations are not small, for example, in the case of hyper-or hypoelasticity, this relationship does not hold.

Elastic wave equations have attracted the interest of numerous researchers owing to their significance in various fields. The Lie group methods have been successfully applied to the study of a variety of elastic wave equations. For instance, Bokhari et al. [2] discussed the Lie group’s approach to the elastic wave equation. Mustafa and Masood [3] adopted the same tool over the third-order elastic wave equation with harmonic correction. Usman et al. [4, 5] conducted a Lie group analysis of the (1+1) and (2+1) elastic wave equations, adding valuable insights to this domain. In addition, many other authors [6, 7] have also been drawn to explore this area, contributing to the growing body of knowledge in the study of elasticity equations. The application of Lie group methods [811] has proven to be a useful approach for understanding the symmetries and properties of these equations, making it an essential tool for researchers in this field.

The linear theory of elasticity posits that the strain tensor ϰij is linearly dependent on the displacement vector Ui according to the equation

ϰij=12(Ui,j+Uj,i) (1)

The non-linear elastic model, in contrast, is founded on the concept of non-linear strain, which is represented by

ϰij=12(Ui,j+Uj,i+Uk,iUk,j). (2)

In the case of a nonlinear strain, the stress is given by the strain rate of a potential function. Among the choices of such a potential functions, the Murnaghan potential appears suitable [1]. This potential is denoted by W(ϰik), is expressed as follows

W(ϰik)=12λ(ϰmm)2+μ(ϰik)2+13a1ϰikϰimϰkm+a2(ϰik)2ϰmm+13a1(ϰmm)3, (3)

where λ and μ represent Lame’s coefficients and a1, a2 are constants. The stress tensor, denoted by τnm, can be calculated using the partial derivatives of the Murnaghan potential for the displacement components

τnm=WUm,n· (4)

The Cauchy equation of motion, in the absence of body forces, is given by

τij,i=ρU¨j. (5)

In this context, Uj symbolizes the displacement vector, τij stands for the stress tensor, and ρ represents the density of the body.

These equations play a fundamental role in describing the mechanical behavior of elastic materials under the influence of stress and displacement dynamics. The Murnaghan potential represents the elastic energy associated with strain components, while the stress tensor and Cauchy equation of motion help understand the relationship between the stress, displacement, and acceleration of particles within the elastic body.

Considering three-dimensional motion in (x1, x2, x3) and U1 = U, the strain tensor components ϰij for this case are given by

ϰ11=Ux1+12Ux12,ϰ22=12Ux22,ϰ33=12Ux32, (6)
ϰ12=ϰ21=12(Ux2+Ux1Ux2),ϰ13=ϰ31=12(Ux3+Ux1Ux3),ϰ23=ϰ32=12Ux2Ux3. (7)

For the three-dimensional case, the Murnaghan potential (3) takes the form

W=12λ(ϰ11+ϰ22+ϰ33)2+μ(ϰ112+ϰ222+ϰ332+ϰ122+ϰ212+ϰ132+ϰ312+ϰ232+ϰ322)+13a1(ϰ113+3ϰ11ϰ122+3ϰ11ϰ132+3ϰ33ϰ132+ϰ333+3ϰ33ϰ322+6ϰ12ϰ13ϰ32+ϰ223+ϰ22ϰ122+3ϰ22ϰ322)+a2(ϰ112+ϰ222+ϰ332+ϰ122+ϰ212+ϰ132+ϰ312+ϰ232+ϰ322)(ϰ11+ϰ22+ϰ33)+13a3(ϰ11+ϰ22+ϰ33)3. (8)

This leads to the following expression for W

W=(λ2+μ)Ux12+(λ2+μ+a13+a1+a33)Ux13+μ2(Ux22+Ux32)+(λ2+μ+a14+a22)(Ux1Ux22+Ux1Ux32). (9)

The stress components can be calculated using the Eq (4) and are given by

τ11=(λ+2μ)Ux1+3(λ2+μ+a13+a1+a33)Ux12+(λ2+μ+a14+a22)(Ux22+Ux32),τ21=μUx2+(λ+2μ+a12+a1)Ux1Ux2,τ31=μUx3+(λ+2μ+a12+a1)Ux1Ux3. (10)

The Cauchy equation of motion (5) takes the following form in the three-dimensional case

τ11,1+τ21,2+τ31,3=ρUττ, (11)

and the components of the potential are given by

τ11,1=(λ+2μ)Ux1x1+6(λ2+μ+a13+a1+a13)Ux1Ux1x1+2(λ2+μ+a14+a12)(Ux2Ux1x2+Ux3Ux1x3),τ21,2=μUx2x2+(λ+2μ+a12+a1)(Ux2Ux1x2+Ux1Ux2x2),τ31,3=μUx3x3+(λ+2μ+a12+a2)(Ux1Ux3x3+Ux3Ux1x3). (12)

Lastly, by utilizing Eq (10), we derive the (3+1)-dimensional nonlinear elastic wave equation as follows

Uττ-AUx1x1-B(Ux2x2+Ux3x3)-CUx1Ux1x1-D(Ux1Ux2x2+Ux1Ux3x3+2Ux2Ux1x2+2Ux3Ux1x3)=0. (13)

In (13), A=λ+2μρ, B=μρ, C=3(λ+2μ)+2(a1+3a2+a3)ρ, D=1ρ(λ+2μ+a12+a2).

In Eq (13), λ and μ are Lame’s coefficients and a1, a2, and a3 are the Murnaghan constants. These expressions provide essential insights into the behavior of the (3+1)-nonlinear elastic wave equation and the underlying physical properties of the elastic medium under consideration. The aim of this study was to investigate the underlying properties of elastic media. The Lie group method [1215] was used to study these properties.

This paper is organized into several sections. In Section 2, we conduct a group analysis and establish an optimal system for the (3+1)-nonlinear elastic wave equation. Section 3 explores group-invariant solutions using the identified optimal system. In Section 4, the authors introduce Noether’s approach for formulating conservation laws and present Noether’s symmetry generators. In Section 5, the focus is shifted to the Lie group and the optimal system of the damped version of the considered equation. This paper proceeds to Section 6, in which symmetry reductions are discussed. Section 7 discusses the partial Lagrangian approach employed to investigate conservation laws. A graphical analysis of the obtained results is presented in Section 8. Finally, in Section 9, we conclude the paper and highlight potential future research directions.

2 Group analysis of the Eq (13)

This section presents a comprehensive Lie symmetry analysis of (13). For this purpose, we consider the vector field given by [16]

Λ=δ1x1+δ2x2+δ3x3+δ4τ+ΨU·

Since the equation under consideration is of second order, we prolong our vector field as follows

Λ[2]=δ1x1+δ2x2+δ3x3+δ4τ+ΨU+Ψ[x1]Ux1+Ψ[x2]Ux2+Ψ[x3]Ux3+Ψ[τ]Uτ+Ψ[x1x1]Ux1x1+Ψ[x1x2]Ux1x2+Ψ[x2x2]Ux2x2+Ψ[x1x3]Ux1x3+Ψ[x2x3]Ux2x3+Ψ[x3x3]Ux3x3+Ψ[x1τ]Ux1τ+Ψ[x2τ]Ux2τ+Ψ[x3τ]Ux3τ+Ψ[ττ]Uττ,

where, Ψ[x1],Ψ[x2],Ψ[x3],Ψ[τ],Ψ[x1x1],Ψ[x1x2],Ψ[x2x2],Ψ[x1x3],Ψ[x2x3],Ψ[x3x3],Ψ[x2τ],Ψ[x2τ],Ψ[x3τ] and Ψ[ττ] are given as follows

Ψ[x1]=Dx1Ψ-Ux1Dx1δ1-Ux2Dx1δ2-Ux3Dx1δ3-UτDx1δ4Ψ[x2]=Dx2Ψ-Ux1Dx2δ1-Ux2Dx2δ2-Ux3Dx2δ3-UτDx2δ4Ψ[x3]=Dx3Ψ-Ux1Dx3δ1-Ux2Dδ2-Ux3Dx3δ3-UτDx3δ4Ψ[τ]=DτΨ-Ux1Dτδ1-Ux2Dτδ2-Ux3Dτδ3-UτDτδ4Ψ[x1x1]=Dx1Ψ[x1]-Ux1x1Dx1δ1-Ux1x2Dx1δ2-Ux1x3Dx1δ3-Ux1τDx1δ4Ψ[x2x2]=Dx2Ψ[x2]-Ux1x2Dx2δ1-Ux2x2Dx2δ2-Ux2x3Dx2δ3-Ux2τDx2δ4Ψ[x3x3]=Dx3Ψ[x3]-Ux1x3Dx3δ1-Ux2x3Dx3δ2-UττDx3δ3-Ux3τDx3δ4Ψ[ττ]=DτΨ[τ]-Ux1τDτδ1-Ux2τDτδ2-Ux3τDτδ3-UττDτδ4Ψ[x1x2]=Dx2Ψ[x1]-Ux1x1Dx2δ1-Ux1x2Dx2δ2-Ux1x3Dx2δ3-Ux1τDx2δ4Ψ[x1τ]=DτΨ[x1]-Ux1x1Dτδ1-Ux1x2Dτδ2-Ux1x3Dτδ3-Ux1τDτδ4Ψ[x2τ]=DτΨ[x2]-Ux1x2Dτδ1-Ux2x2Dτδ2-Ux2x3Dτδ3-Ux2τDτδ4Ψ[x1x3]=Dx3Ψ[x1]-Ux1x1Dx3δ1-Ux1x2Dx3δ2-Ux1x3Dx3δ3-Ux1τDx3δ4Ψ[x2x3]=Dx3Ψ[x2]-Ux1x2Dx3δ1-Ux2x2Dx3δ2-Ux2x3Dx3δ3-Ux2τDx3δ4Ψ[x3τ]=DτΨ[x3]-Ux1x3Dτδ1-Ux2x3Dτδ2-UττDτδ3-Unu3τDτδ4, (14)

where Dα denotes the total derivative of α.

The invariance criterion of PDE is

Λ[2](Uττ-AUx1x1-B(Ux2x2+Ux3x3)-CUx1Ux1x1-D(Ux1Ux2x2+Ux1Ux3x3)-2D(Ux2Ux1x2+Ux3Ux1x3))|(13)=0. (15)

The invariance condition (15) which lead to the following after some calculations. After performing some calculations we get,

δ1x1=δ2x2=δ3x3=δ4τ=ΨU,δ1x2=δ1x3=δ1τ=δ1U=0,δ4x1=δ4x2=δ4x3=δ4U=0,δ2x1=δ2τ=δ2U=0,δ3x1=δ3τ=δ3U=0,Ψx1=Ψx2=Ψx3=0,δ4ττ=0,δ2x3x3=0,Ψττ=0,δ3x2+δ2x3=0. (16)

So the infinitesimals are

δ1=C1x1+C2,δ2=C1x2+C3x3+C4,δ3=C1x3-C3x2+C5,δ4=C1τ+C6,Ψ=C1U+C7τ+C8. (17)

We obtain the following symmetry algebra

Λ1=τ,Λ2=U,Λ3=x1,Λ4=x2,
Λ5=x3,Λ6=τU,Λ7=x3x2-x2x3,
Λ8=x1x1+x2x2+x3x3+ττ+UU·

Table 1 shows the commutator relation for the symmetry algebra (2). The adjoint representations of the symmetry algebra (15) are presented in Tables 2 and 3.

Table 1. Commutator table.

i, Λj] Λ1 Λ2 Λ3 Λ4 Λ5 Λ6 Λ7 Λ8
Λ1 0 0 0 0 0 Λ2 0 Λ1
Λ2 0 0 0 0 0 0 0 Λ2
Λ3 0 0 0 0 0 0 0 Λ3
Λ4 0 0 0 0 0 0 −Λ5 Λ4
Λ5 0 0 0 0 0 0 Λ4 Λ5
Λ6 −Λ2 0 0 0 0 0 0 0
Λ7 0 0 0 Λ5 −Λ4 0 0 0
Λ8 −Λ1 −Λ2 −Λ3 −Λ4 5 0 0 0

Table 2. Adjoint table.

Ad(eϵ) Λ1 Λ2 Λ3 Λ4
Λ1 Λ1 Λ2 Λ3 Λ4
Λ2 Λ1 Λ2 Λ3 Λ4
Λ3 Λ1 Λ2 Λ3 Λ4
Λ4 Λ1 Λ2 Λ3 Λ4
Λ5 Λ1 Λ2 Λ3 Λ4
Λ6 Λ1 + ϵΛ2 Λ2 Λ3 Λ4
Λ7 Λ1 Λ2 Λ3 cos(ϵ4 − sin(ϵ5
Λ8 eϵΛ1 eϵΛ2 eϵΛ3 eϵΛ4

Table 3. Adjoint table.

Ad(eϵ) Λ5 Λ6 Λ7 Λ8
Λ1 Λ5 Λ6ϵΛ2 Λ7 Λ8ϵΛ1
Λ2 Λ5 Λ6 Λ7 Λ8ϵΛ2
Λ3 Λ5 Λ6 Λ7 Λ8ϵΛ3
Λ4 Λ5 Λ6 Λ7 + ϵΛ5 Λ8ϵΛ4
Λ5 Λ5 Λ6 Λ7ϵΛ4 Λ8ϵΛ5
Λ6 Λ5 Λ6 Λ7 Λ8
Λ7 sin(ϵ4 + cos(ϵ5 Λ6 Λ7 Λ8
Λ8 eϵΛ5 Λ6 Λ7 Λ8

2.1 Optimal system

The optimal system of subalgebras is a concept in the context of Lie symmetry analysis. This was first introduced by Ibragimov [17] and then carried out by Olver [18]. When analyzing the symmetries of a differential equation using the Lie group method, we often encounter Lie algebra consisting of several infinitesimal generators. However, not all these generators are linearly independent. The optimal system of subalgebras is the maximal set of linearly independent generators that provide a complete description of the symmetries of the differential equation. It represents the minimal set of generators needed to construct all symmetries and invariant solutions of the equation. Here, we discuss the optimal system for (13):

Consider a general element Λ of Lie algebra L8 given by,

Λ=μ1Λ1+μ2Λ2+μ3Λ3+μ4Λ4+μ5Λ5+μ6Λ6+μ7Λ7+μ8Λ8, (18)

where μ denotes arbitrary constants.

Case 1: μ8 ≠ 0, μ7 ≠ 0. By the adjoint action of Λ1, Λ3 and Λ4, (18) simplifies to Λ = μ6Λ6 + μ7Λ7 + μ8Λ8. Therefore, the corresponding subalgebra is R1=Λ6+κΛ7+σΛ8 κ, σ ≠ 0.

Case 2: μ8 ≠ 0, μ7 = 0. By the adjoint action of Λ1, Λ3, Λ4 and Λ5, (18) simplifies to Λ = μ6Λ6 + μ8Λ8. Hence, the corresponding subalgebra is R2=Λ6+κΛ8 κ ≠ 0.

Case 3: μ8 ≠ 0, μ7 ≠ 0, μ6 = 0. By the adjoint action of Λ1, Λ2, Λ3 and Λ4, (18) simplifies to Λ = μ7Λ7 + μ8Λ8. Hence, the corresponding subalgebra is R3=Λ7+κΛ8 κ ≠ 0.

Case 4: μ8 ≠ 0, μ7 = 0, μ6 = 0. By the adjoint action of Λ1, Λ2, Λ3, Λ4 and Λ5, (18) simplifies to Λ = μ8Λ8. Therefore, the corresponding subalgebra is R4=Λ8.

Case 5: μ8 = 0, μ7 ≠ 0, μ3 ≠ 0. From the adjoint action of Λ1, Λ4, Λ5 and Λ8, Eq (18) simplifies to Λ = μ1Λ1 + μ3Λ3 + eϵμ6Λ6 + eϵμ7Λ7. Therefore, the corresponding subalgebra is R5=Λ1+κΛ3±Λ6±Λ7 κ ≠ 0.

Case 6: μ8 = 0, μ7 ≠ 0, μ6 = 0, μ3 ≠ 0. By the adjoint action of Λ4, Λ5, Λ6 and Λ8, (18) simplifies to Λ = μ1Λ1 + μ3Λ3 + eϵμ7Λ7. Therefore, the corresponding subalgebra is R6=Λ1+κΛ3±Λ7, and κ ≠ 0.

Case 7: μ8 = 0, μ7 = 0, μ6 ≠ 0, μ3 ≠ 0. By the adjoint action of Λ6, Λ7 and Λ8, (18) simplifies to Λ = μ1Λ1 + μ3Λ3 + eϵμ6Λ6. Therefore, the corresponding subalgebra is R7=Λ1+κΛ3±Λ6, and κ ≠ 0.

Case 8: μ8 = 0, μ7 = 0, μ6 = 0, μ3 ≠ 0. By the adjoint action of Λ6 and Λ7, (18) simplifies to Λ = μ1Λ1 + μ3Λ3. Therefore, the corresponding subalgebra is R8=Λ1+κΛ3, and κ ≠ 0.

Case 9: μ8 = 0, μ7 = 0, μ6 = 0, μ5 = 0, μ4 ≠ 0, μ3 ≠ 0. By the adjoint action of Λ6, (18) simplifies to Λ = μ1Λ1 + μ3Λ3 + μ4Λ4. Thus, R9=Λ1+κΛ3+σΛ4 κ, σ ≠ 0.

Case 10: μ8 = 0, μ7 = 0, μ6 = 0, μ1 = 0, μ5 = 0, μ4 ≠ 0, μ3 ≠ 0. Then, (18) is simplified to Λ = μ2Λ2 + μ3Λ3 + μ4Λ4. Thus, R10=Λ2+κΛ3+σΛ4, κ, σ ≠ 0.

Case 11: μ8 = 0, μ6 = 0, μ3 = 0. By the adjoint action of Λ4, Λ5, Λ6 and Λ8, (18) reduces to Λ = μ1Λ1 + eϵμ7Λ7. Therefore, R11=Λ1±Λ7.

Case 12: μ8 = 0, μ6 = 0, μ1 = 0, μ3 ≠ 0. By the adjoint action of Λ4, Λ5 and Λ8 Eq (18) reduces to Λ = μ2Λ2 + μ3Λ3 + eϵμ7Λ7. Therefore, R12=Λ2+κΛ3±Λ7,κ0.

Case 13: μ8 = 0, μ6 = 0, μ1 = 0, μ2 = 0, μ3 ≠ 0. By the adjoint action of Λ4, Λ5 and Λ8 (18), reduces to Λ = μ3Λ3 + eϵμ7Λ7. Therefore, R13=Λ3±Λ7.

Case 14: μ8 = 0, μ6 = 0, μ1 = 0, μ2 ≠ 0, μ3 = 0. By the adjoint action of Λ4, Λ5 and Λ8, (18) reduces to Λ = μ2Λ2 + eϵμ7Λ7. Therefore, R14=Λ2±Λ7.

Case 15: μ8 = 0, μ1 = 0, μ3 ≠ 0. By the adjoint action of Λ1, Λ4, Λ5 and Λ8 Eq (18) is reduced to Λ = μ3Λ3 + eϵμ6Λ6 + eϵμ7Λ7. Thus, R15=Λ3±Λ6±Λ7.

Case 16: μ8 = 0, μ7 = 0, μ1 = 0, μ3 ≠ 0. By the adjoint action of Λ1, Λ7 and Λ8, (18) reduces to Λ = μ3Λ3 + eϵμ6Λ6. Therefore, R16=Λ3±Λ6.

Case 17: μ8 = 0, μ7 = 0, μ4 = 0, μ1 = 0, μ5 ≠ 0. By the adjoint action of Λ1 and Λ8 Eq (18) reduces to Λ = μ3Λ3μ5Λ5 + eϵμ6Λ6. Therefore, R17=Λ3+κΛ5±Λ6,κ0.

Case 18: μ8 = 0, μ7 = 0, μ6 = 0, μ1 = 0, μ4 = 0, μ2 = 0, μ5 ≠ 0. Then, (18) is reduced to Λ = μ3Λ3 + μ5Λ5. Therefore, R18=Λ3+κΛ5,κ0.

Case 19: μ8 = 0, μ7 = 0, μ6 = 0, μ1 = 0, μ5 = 0, μ2 = 0, μ4 ≠ 0. Then, (18) is reduced to Λ = μ3Λ3 + μ4Λ4. Therefore, R19=Λ3+κΛ4,κ0.

Case 20: μ8 = 0, μ7 = 0, μ5 = 0, μ1 = 0, μ4 ≠ 0. By the adjoint action of Λ1 and Λ8 Eq (18) reduces to Λ = μ3Λ3 + μ4Λ4 + eϵμ6Λ6. Therefore, R20=Λ3+κΛ4±Λ6,κ0.

Case 21: μ8 = 0, μ7 = 0, μ4 = 0, μ3 = 0, μ1 = 0, μ5 ≠ 0. By the adjoint action of Λ1 and Λ8, (18) reduces to Λ = μ5Λ5 + eϵμ6Λ6. Therefore, R21=Λ5±Λ6.

Case 22: μ8 = 0, μ7 = 0, μ4 = 0, μ3 = 0, μ1 = 0, μ5 = 0. By the adjoint action of Λ1, (18) is reduced to Λ = μ6Λ6. Thus, R22=Λ6.

Case 23: μ8 = 0, μ7 = 0, μ4 = 0, μ3 = 0, μ1 = 0, μ6 = 0, μ2 = 0. Then, (18) is reduced to Λ = μ5Λ5. Therefore, R23=Λ5.

Case 24: μ8 = 0, μ7 ≠ 0, μ3 = 0, μ1 = 0. By the adjoint action of Λ1, Λ4 and Λ5, (18) reduces to Λ = μ6Λ6 + μ7Λ7. Therefore, R24=Λ6+κΛ7,κ0.

Case 25: μ8 = 0, μ7 ≠ 0, μ6 = 0, μ3 = 0μ2 = 0, μ1 = 0. By the adjoint action of Λ4 and Λ5, Eq (18) is reduced to Λ = μ7Λ7. Thus, R25=Λ7.

Case 26: μ8 = 0, μ7 = 0, μ5 = 0, μ4 = 0, μ3 = 0. By the adjoint action of Λ1 and Λ8, Eq (18) is reduced to Λ = μ1Λ1 + eϵμ6Λ6. Therefore, R26=Λ1±Λ6.

Case 27: μ8 = 0, μ7 = 0, μ6 = 0, μ5 = 0, μ4 = 0, μ3 = 0. By the adjoint action of Λ6, (18) reduces to Λ = μ1Λ1. Thus, R27=Λ1.

Case 28: μ8 = 0, μ7 = 0, μ5 = 0, μ3 = 0, μ1 = 0, μ6 ≠ 0. By the adjoint action of Λ1 and Λ8, Eq (18) is reduced to Λ = μ4Λ4 + eϵμ6Λ6. Therefore, R28=Λ4±Λ6.

Case 29: μ8 = 0, μ7 = 0, μ5 = 0, μ3 = 0, μ1 = 0, μ6 = 0, μ2 = 0. Then, (18) is reduced to Λ = μ4Λ4. Thus, R29=Λ4.

Case 30: μ8 = 0, μ7 = 0, μ6 = 0, μ4 = 0, μ3 ≠ 0, μ5 ≠ 0. From the adjoint action of Λ6 and Λ8, Eq (18) reduces to Λ = μ1Λ1 + μ3Λ3 + μ5Λ5. Thus, R30=Λ1+κΛ3+σΛ5,κ,σ0,

Case 31: μ8 = 0, μ7 = 0, μ6 = 0, μ4 = 0, μ3 = 0, μ5 ≠ 0. By the adjoint action of Λ6, Eq (18) is reduced to Λ = μ1Λ1 + μ5Λ5. Therefore, R31=Λ1+κΛ5,κ0.

Case 32: μ8 = 0, μ7 = 0, μ6 = 0, μ4 = 0, μ1 = 0, μ3 ≠ 0, μ5 ≠ 0. Then, (18) is reduced to Λ = μ2Λ2 + μ3Λ3 + μ5Λ5. Thus, R32=Λ2+κΛ3+σΛ5,κ,σ0,

Case 33: μ8 = 0, μ7 = 0, μ6 = 0, μ4 = 0, μ1 = 0, μ3 ≠ 0, μ5 = 0. Then, (18) is reduced to Λ = μ2Λ2 + μ3Λ3. Therefore, R33=Λ2+κΛ3,κ0.

Case 34: μ8 = 0, μ7 = 0, μ6 = 0, μ4 = 0, μ1 = 0, μ3 = 0, μ5 ≠ 0. Then, (18) is reduced to Λ = μ2Λ2 + μ5Λ5. Therefore, R34=Λ2+κΛ5,κ0.

Case 35: μ8 = 0, μ7 = 0, μ6 = 0, μ4 = 0, μ1 = 0, μ3 = 0, μ5 = 0. Then, (18) is reduced to Λ = μ2Λ2. Thus, R35=Λ2.

Case 36: μ8 = 0, μ7 = 0, μ6 = 0, μ4 = 0, μ1 = 0, μ2 = 0, μ5 = 0. Then, (18) is reduced to Λ = μ3Λ3. Thus, R36=Λ3.

Case 37: μ8 = 0, μ7 = 0, μ6 = 0, μ5 = 0, μ3 = 0, μ4 ≠ 0. By the adjoint action of Λ6, Eq (18) is reduced to Λ = μ1Λ1 + μ4Λ4. Therefore, R37=Λ1+κΛ4,κ0.

Case 38: μ8 = 0, μ7 = 0, μ6 = 0, μ5 = 0, μ3 = 0, μ1 = 0, μ4 ≠ 0. Then, (18) is reduced to Λ = μ2Λ2 + μ4Λ4. Therefore, R38=Λ2+κΛ4,κ0.

Hence, the one-dimensional optimal system for Eq (13) is given by,

R1=Λ6+κΛ7+σΛ8,κ,σ0R2=Λ6+κΛ8,κ0R3=Λ7+κΛ8,κ0R4=Λ8R5=Λ1+κΛ3±Λ6±Λ7,κ0R6=Λ1+κΛ3±Λ7,κ0R7=Λ1+κΛ3±Λ6,κ0R8=Λ1+κΛ3,κ0R9=Λ1+κΛ3+σΛ4,κ,σ0R10=Λ2+κΛ3+σΛ4,κ,σ0R11=Λ1±Λ7R12=Λ2+κΛ3±Λ7,κ0R13=Λ3±Λ7R14=Λ2±Λ7R15=Λ3±Λ6±Λ7R16=Λ3±Λ6R17=Λ3+κΛ5±Λ6,κ0R18=Λ3+κΛ5,κ0R19=Λ3+κΛ4,κ0R20=Λ3+κΛ4±Λ6,κ0R21=Λ5±Λ6R22=Λ6R23=Λ5R24=Λ6+κΛ7,κ0R25=Λ7R26=Λ1±Λ6R27=Λ1R28=Λ4±Λ6R29=Λ4R30=Λ1+κΛ3+σΛ5,κ,σ0R31=Λ1+κΛ5,κ0R32=Λ2+κΛ3+σΛ5,κ,σ0R33=Λ2+κΛ3,κ0R34=Λ2+κΛ5,κ0R35=Λ2R36=Λ3R37=Λ1+κΛ4,κ0R38=Λ2+κΛ4,κ0

3 Group invariant solutions

Invariant solutions [19] are the solutions to differential equations that remain unchanged under the action of a given symmetry group. In the context of the Lie group method, invariant solutions are those that are preserved by the symmetry transformations generated by the infinitesimal generators of the group. In this section, we focus on investigating the invariant solutions of (13).

Invariant Solutions by Using R27=Λ1.

First, let us consider the infinitesimal generator Λ1=τ·

The characteristic equation associated with Λ1 is given by

dx10=dx20=dx30=dτ1=dU0·

From the characteristic equation, we can deduce that x1 = α, x2 = β, x3 = λ, U = X(α, β, λ). Using these invariant variables, (13) is transformed into the equation given by

(-CXα-A)Xαα+(-DXα-B)Xββ+(-DXα-B)Xλλ-2D(XβXαβ+XλXαλ)=0, (19)

Infinitesimals of (19) are written as

δα=c2α+c5,δβ=-c1λ+c2β+c6,δλ=c1β+c2λ+c3,ΨX=c2X+c4. (20)

Case 1: By taking c3 = 1 and all other constants zero, the characteristic equation associated with (20) is

dα0=dβ0=dλ1=dX0,

which implies that α = r, β = s, and X(α, β, λ) = Y(r, s). Using these invariant variables, (19) is transformed into the following equation

(-DYr-B)Yss+(-CYr-A)Yrr-2DYsYrs=0. (21)

Infinitesimals of Eq (21) becomes

δr=c1r+c4,δs=c1s+c2,ΨY=c1Y+c3. (22)

Case 1a: By taking c2 = 1, c4 = 1 and all other constants zero, the characteristic equation associated with (22) is

dr1=ds1=dY0,

which implies that −r + s = p and Y(r, s) = Z(p). Using these invariant variables, (21) is transformed into the following ODE

-Z(A+B+(-C-3D)Z)=0. (23)

If Z″ = 0, then Z(p) = c1p + c2. This implies Y(r, s) = c1(sr) + c2, this gives X(α, β, λ) = c1(βα) + c2.

So, the solution of (13) in original variables is

U(x1,x2,x3,τ)=c1(x2-x1)+c2.

Now, if Z″ ≠ 0, from (23), we have A + B + (−C − 3D)Z′ = 0 which gives Z(p)=c1+(A+B)(C+3D)p, which provides Y(r,s)=c1+(A+B)(C+3D)(s-r).

This implies,

X(α,β,λ)=c1+(A+B)(C+3D)(β-α). (24)

Hence, the solution of (13) in original variables is

U(x1,x2,x3,τ)=c1+(A+B)(C+3D)(x2-x1).

Invariant Solutions by Using R29=Λ4.

First, let us consider the infinitesimal generator Λ4=x2·

The characteristic equation associated with Λ4 is given by

dx10=dx21=dx30=dτ0=dU0·

From the characteristic equation, we can deduce that τ = α, x1 = β, x3 = λ, U = X(α, β, λ). Using these invariant variables, (13) is transformed into the equation given by

(-CXβ-A)Xββ+(-DXβ-B)Xλλ-2DXλXβλ+Xαα=0. (25)

Infinitesimals of (25) are written as

δα=c1α+c2,δβ=c1β+c6,δλ=c1λ+c5,ΨX=c1X+c3α+c4. (26)

Case 2: By taking c4 = 1, c5 = 1 and all other constants zero, the characteristic equation associated with (26) is

dα0=dβ0=dλ1=dX1,

which implies that α = r, β = s, and X(α, β, λ) = λ + Y(r, s). Using these invariant variables, (25) is transformed into the following equation

(-CYs-A)Yss+Yrr=0. (27)

Infinitesimals of Eq (27) becomes

δr=c1r+c2,δs=c3s+c4,ΨY=(3c3-2c1)Y-2AC(c1-c3)s+c5r+c6. (28)

Case 2a: By taking c2 = 1, c4 = 1, c6 = 1 and all other constants zero, the characteristic equation associated with (28) is

dr1=ds1=dY1,

which implies that −r + s = p and Y(r, s) = r + Z(p). Using these invariant variables, (27) is transformed into the following ODE

-Z(CZ+A-1)=0. (29)

If Z″ = 0, then Z(p) = c1p + c2. This implies Y(r, s) = c1(sr) + c2 + r, this gives X(α, β, λ) = c1(βα) + c2 + α + λ.

So, the solution of (13) in original variables is

U(x1,x2,x3,τ)=c1(x1-τ)+c2+τ+x3.

Now, if Z″ ≠ 0, then from (29), we have CZ′ + A − 1 = 0 which gives Z(p)=c1-(A-1)Cp, which provides Y(r,s)=c1+r-(A-1)C(s-r).

This implies,

X(α,β,λ)=c1+α+λ-(A-1)C(β-α). (30)

Hence, the solution of (13) in original variables is

U(x1,x2,x3,τ)=c1+τ+x3-(A-1)C(x1-τ).

Invariant Solutions by Using R23=Λ5.

First, let us consider the infinitesimal generator Λ5=x3·

The characteristic equation associated with Λ5 is given by

dx10=dx20=dx31=dτ0=dU0·

From the characteristic equation, we can deduce that τ = α, x1 = β, x2 = λ, U = X(α, β, λ). Using these invariant variables, (13) is transformed into the equation given by

(-CXβ-A)Xββ+(-DXβ-B)Xλλ-2DXλXβλ+Xαα=0. (31)

Infinitesimals of (31) are written as

δα=c1α+c2,δβ=c1β+c6,δλ=c1λ+c5,ΨX=c1X+c3α+c4. (32)

Case 3: By taking c2 = 1, c4 = 1 and all other constants zero, the characteristic equation associated with (32) is

dα1=dβ0=dλ0=dX1,

which implies that β = r, λ = s, and X(α, β, λ) = α + Y(r, s). Using these invariant variables, (31) is transformed into the following equation

(-DYr-B)Yss+(-CYr-A)Yrr-2DYsYrs=0. (33)

Infinitesimals of Eq (33) becomes

δr=c1r+c4,δs=c1s+c2,ΨY=c1Y+c3. (34)

Case 3a: By taking c4 = 1 and all other constants zero, the characteristic equation associated with (34) is

dr1=ds0=dY0,

which implies that s = p and Y(r, s) = Z(p). Using these invariant variables, (33) is transformed into the following ODE

-BZ=0. (35)

This implies Z(p) = c1p + c2, this gives Y(r, s) = c1s + c2,

This implies,

X(α,β,λ)=c1λ+c2+α, (36)

So, the solution of (13) in original variables is

U(x1,x2,x3,τ)=c1x2+c2+τ.

Invariant Solutions by Using R8=Λ1+κΛ3.

First, let us consider the infinitesimal generator Λ1+κΛ3=τ+κx1·

The characteristic equation associated with Λ1 + κΛ3 is given by

dx1κ=dx20=dx30=dτ1=dU0·

From the characteristic equation, we deduce that x2=α,x3=β,τ-x1κ=λ,U=X(α,β,λ). Using these invariant variables, (13) is transformed into the equation given by

-Bκ3Xαα-Bκ3Xββ+κ2DXλXαα+κ2DXλXββ+2κ2DXβXβλ+2κ2DXαXαλ+κ3Xλλ-κAXλλ+CXλXλλ=0, (37)

Infinitesimals of (37) are written as

δα=c1β+c2α+c3,δβ=-c1α+c2β+c6,δλ=c2λ+c5,ΨX=c2X+c4. (38)

Case 4: By taking c3 = 1, c6 = 1 and all other constants zero, the characteristic equation associated with (38) is

dα1=dβ1=dλ0=dX0,

which implies that λ = r, βα = s and X(α, β, λ) = λ + Y(r, s). Using these invariant variables, (37) is transformed into the following equation

(κ3-κA+CYr)Yrr+(-2Bκ3+2Dκ2Yr)Yss+4Dκ2YsYrs=0, (39)

Infinitesimals of Eq (39) becomes

δr=c1r+c4,δs=c1s+c2,ΨY=c1Y+c3. (40)

Case 4a: By taking c2 = 1, c3 = 1, c4 = 1 and all other constants zero, the characteristic equation associated with (40) is

dr1=ds1=dY1,

which implies that −r + s = p, Y(r, s) = r + Z(p). Using these invariant variables, (39) is transformed into the following ODE

-Z((6Dκ2+C)Z+(2B-1)κ3-2Dκ2+κA-C)=0, (41)

If Z″ = 0, then Z(p) = c1p + c2. This implies Y(r, s) = c1(sr) + c2 + r, this gives X(α, β, λ) = c1(βα − λ) + c2 + 2λ.

So, the solution of (13) in original variables is

U(x1,x2,x3,τ)=c1(x3-x2-(τ-x1κ))+c2+2(τ-x1κ).

Now, if Z″ ≠ 0, then from (41), we have (62 + C)Z′ + (2B − 1)κ3 − 22 + κAC = 0, which yields Z(p)=(2Dκ2-κA+C-(2B-1)κ3)p6Dκ2+C+c1, which provides Y(r,s)=(2Dκ2-κA+C-(2B-1)κ3)(s-r)6Dκ2+C+c1+r.

This implies,

X(α,β,λ)=(2Dκ2-κA+C-(2B-1)κ3)(β-α-λ)6Dκ2+C+c1+2λ. (42)

Hence, the solution of (13) in original variables is

U(x1,x2,x3,τ)=(2Dκ2-κA+C-(2B-1)κ3)(x3-x2-(τ-x1κ))6Dκ2+C+c1+2(τ-x1κ).

Invariant Solutions by Using R16=Λ3+Λ6.

First, let us consider the infinitesimal generator Λ3+Λ6=x1+τU·

The characteristic equation associated with Λ3 + Λ6 is given by

dx11=dx20=dx30=dτ0=dUτ·

From the characteristic equation, we can deduce that τ = α, x2 = β, x3 = λ, U = x1τ + X(α, β, λ). Using these invariant variables, (13) is transformed into the equation given by

(-αD-B)Xββ+(-αD-B)Xλλ+Xαα=0, (43)

Infinitesimals of (43) are written as

δα=2(αD+B)((c2β+c4)D+92c1λ)3D2,δβ=29D2c2(αD+B)3+c22β2+c4β+92Dc1βλ-c22λ2-c3λ+c13,δλ=-94Dc1β2+(c2λ+c3)β+94Dc1λ2+c4λ+c5+c1(α+BD)3,ΨX=13Dea3λea2β(3Dc7(c11(ea3λ)2+c12)((ea2β)2c9+c10)AiryAi(-(αD+B)(-D(a2+a3))13D)+3Dc8(c11(ea3λ)2+c12)((ea2β)2c9+c10)AiryBi(-(αD+B)(-D(a2+a3))13D)-2ea2βea3λX((c2β-32c6)D+92c1λ)). (44)

Case 5: By taking c13 = 1 and all other constants zero, the characteristic equation associated with (44) is

dα0=dβ0=dλ1=dX0,

which implies that α = r, β = s, X(α, β, λ) = Y(r, s). Using these invariant variables, (43) is transformed into the following equation

(-rD-B)Yss+Yrr=0. (45)

Infinitesimals of Eq (45) becomes

δr=(rD+B)(c7D-4c1s)D,δs=-43D2c1(rD+B)3-3c1s2+32Dc7s+c8,ΨY=1ea2s(c3(c5(ea2s)2+c6)AiryAi(-(-a2D)13(rD+B)D)+c4(c5(ea2s)2+c6)AiryBi(-(-a2D)13(rD+B)D)+ea2sY(c1s+c2)). (46)

Case 5a: By taking c7 = 1 and all other constants zero, the characteristic equation associated with (46) is

dr(rD+B)=ds32sD=dY0,

which implies that s(rD+B)32=p and Y(r, s) = Z(p). Using these invariant variables, (45) is transformed into the following ODE

9D2p2Z+15D2pZ-4Z=0. (47)

This implies,

Z(p)=c1+hypergeom([12,56],[32],94D2p2)c2p, (48)

which gives,

Y(r,s)=c1+hypergeom([12,56],[32],94D2s2(rD+B)3)c2s(rD+B)32, (49)

this gives,

X(α,β,λ)=c1+hypergeom([12,56],[32],94D2β2(αD+B)3)c2β(αD+B)32, (50)

So, the solution of (13) in original variables is

U(x1,x2,x3,τ)=c1+x1τ+hypergeom([12,56],[32],94D2x22(τD+B)3)c2x2(τD+B)32. (51)

Invariant Solutions by Using R7=Λ1+κΛ3+Λ6.

First, let us consider the infinitesimal generator Λ1+κΛ3+Λ6=τ+κx1+τU·

The characteristic equation associated with Λ1 + κΛ3 + Λ6 is given by

dx1κ=dx20=dx30=dτ1=dUτ·

From the characteristic equation, we deduce that x2=α,x3=β,τ-x1κ=λ,U=2κx1τ-x122κ2+X(α,β,λ). Using these invariant variables, (13) is transformed into the equation given by

(κ3-Aκ+CXλ-Cλ)Xλλ+κ2(DXλ-Bκ-Dλ)Xββ+κ2(DXλ-Bκ-Dλ)Xαα+2Dκ2XαXαλ+2Dκ2XβXβλ+Aκ-CXλ+Cλ=0, (52)

Infinitesimals of (52) are written as

δα=c1β+c2,δβ=-c1α+c5,δλ=c3,ΨX=c3λ+c4. (53)

Case 6: By taking c3 = 1 and all other constants zero, the characteristic equation associated with (53) is

dα0=dβ0=dλ1=dXλ,

which implies that α = r, β = s, and X(α,β,λ)=λ22+Y(r,s). Using these invariant variables, (52) is transformed into the following equation

-κ3(BYss+BYrr-1)=0. (54)

Infinitesimals of Eq (54) becomes

δr=B(F4(s-Ir)+F6(s+Ir))-c2s+c12r+c4,δs=-BI(-F6(s+Ir)+F4(s-Ir))+c12s+c2r+c3,ΨY=c1Y+F3(s-Ir)+rF4(s-Ir)+F5(s+Ir)+rF6(s+Ir). (55)

Case 6a: By taking c3 = 1, c4 = 1 and all other constants zero, the characteristic equation associated with (55) is

dr1=ds1=dY0,

which implies that −r + s = p, Y(r, s) = Z(p). Using these invariant variables, (54) is transformed into the following ODE

-2Bκ3Z+κ3=0. (56)

This implies,

Z(p)=14Bp2+c1p+c2, (57)

which yields,

Y(r,s)=14B(-r+s)2+c1(-r+s)+c2, (58)

this gives,

X(α,β,λ)=λ22+14B(-α+β)2+c1(-α+β)+c2. (59)

So, the solution of (13) in original variables is

U(x1,x2,x3,τ)=2κx1τ-x122κ2+(τ-x1κ)22+14B(-x2+x3)2+c1(-x2+x3)+c2. (60)

4 Noether’s approach

Let us contemplate a differential system of m-th order

G(x,U,Uτ,U(1),U(2),U(m))=0, (61)

where xi with i = 1, 2, ⋯, n represents independent variables, and Uα with α = 1, 2, ⋯, m symbolizes the dependent variables. Additionally, the notation Um signifies the m th-order partial derivative.

The Lie-Bäcklund operator is defined as follows

Λ1=δixi+ΨϖUϖ+s1Ψi1isϖUi1isϖ, (62)

where Ψi1isϖ is defined by

Ψiϖ=Di(Ψϖ)-UjϖDi(δj),Ψi1isϖ=Dis(Ψi1is-1ϖ)-Uji1is-1ϖDis(δj),s>1,

In this context, Di denotes the total derivative operator.

The Lie-Bäcklund operator (62), when expressed in characteristic form, takes on the following representation

Λ=δixi+WϖUϖ+Di(Wϖ)Uiϖ+DiDj(Wϖ)Uijϖ+, (63)

where,

Wϖ=Ψδ-δjUjϖ,ϖ=1,2,,m,

constitute Lie characteristic functions.

The Noether operators linked with a Lie-Bäcklund operator Λ are given by

Ni=Ψi+WϖδδUiϖ+s1Di1Dis(Wϖ)δδUij1jsϖ,i=1,2,,n, (64)

where δδUiϖ denotes the Euler-Lagrange operator, which is defined as

δδUiϖ=Uiϖ+s1(-1)sDj1DjsUij1jsϖ,i=1,2,,n,ϖ=1,2,,m. (65)

Lagrangian A Lagrangian for the Eq (61) is described by a function L=L(x,U,U(1),,U(m-1)), which adheres to the Euler-Lagrange equation

δLδUα=0. (66)

Noether Symmetry Generator A Lie-Bäcklund operator Λ is considered a Noether symmetry generator of the Eq (61) with respect to a Lagrangian L if there exist gauge functions Gi=(G1,,Gm) that fulfill the condition

Λ(L)+LDi(Ψi)=Di(Gi). (67)

Noether Conserved Vectors Each Noether symmetry generator Λ associated with a given Lagrangian L that relates to the Euler-Lagrange differential equations corresponds to a vector T = (T1, T2, ⋯, Tm). The definition of each component Ti is as follows

Ti=Gi-NiL=Gi-δiL-WϖδLδUiϖ-s1Di1is(Wϖ)δLδUi1isϖ, (68)

Vector Ti serves as a conserved quantity for Eq (66). Eq (67) is employed to identify the Noether symmetries, whereas (68) provides the associated Noether conserved vectors.

4.1 Noether’s approach to Eq (13)

In this subsection, we utilize Noether’s approach [20] to determine the conservation laws of (13). We begin by determining the Noether symmetries, and then establish the corresponding conservation laws using the Noether theorem.

The Lagrangian for Eq (13) given by

L=AUx122+B2(Ux22+Ux32)+CUx136-Uτ22+D2(Ux1Ux22+Ux1Ux32). (69)

Applying the Euler operator (65) to the Eq (69), we get

δLδu=Uττ-AUx1x1-B(Ux2x2+Ux3x3)-CUx1Ux1x1-D(Ux1Ux2x2+Ux1Ux3x3)-2D(Ux2Ux1x2+Ux3Ux1x3)=0. (70)

Hence, we can deduce Noether symmetries by employing the calculated Lagrangian. These symmetries, identified through Noether’s theorem, enable us to establish the conservation laws associated with Eq (13). These conservation laws offer valuable insights into the underlying physics and behavior of the system.

4.1.1 Computation of the noether symmetries

We consider the following vector field

Λ=δ1x1+δ2x2+δ3x3+δ4τ+ΨU·

The vector field Λ is called a Noether symmetry of Eq (13) corresponding to Lagrangian (69) if it fulfills the condition

Λ[1]L+L(Dτδ4+Dx1δ1+Dx2δ2+Dx3δ3)=DτG1+Dx1G2+Dx2G3+Dx3G4, (71)

where,

Λ[1]=Λ+Ψx1Ux1+Ψx2Ux2+Ψx3Ux3+ΨτUτ,

and Gi(x1,x2,x3,τ,U),i=1,2,3,4 are gauge terms. We compare the coefficients of derivatives of U in the above equation to obtain the determining system. After performing some steps we get

Aδ2x2-Aδ1x1+Aδ3x3+Aδ4τ+2AΨU+CΨx1=0,Bδ1x1-Bδ2x2+Bδ3x3+Bδ4τ+2BΨU+DΨx1=0,Bδ1x1+Bδ2x2-Bδ3x3+Bδ4τ+2BΨU+DΨx1=0,2ΨU+δ1x1+δ2x2+δ3x3-δ4τ=0,3ΨU-2δ1x1+δ2x2+δ3x3+δ4τ=0,3ΨU-δ2x2+δ3x3+δ4τ=0,3ΨU+δ2x2-δ3x3+δ4τ=0,δ1x2=δ1x3=δ1τ=δ1U=0,δ2x1=δ2τ=δ2U=0,δ2x3+δ3x2=0,δ3x1=δ3τ=δ3U=0,δ4x1=δ4x2=δ4x3=δ4U=0,Ψx2=Ψx3=GU3=GU4=0,AΨx1-GU2=0,-Ψτ-GU1=0,Gτ1+Gx12+Gx23+Gx34=0. (72)

The following result follows

δ1=C1,δ2=C3x3+C4,δ3=-C3x2+C5,δ4=C2,Ψ=C6τ+C7,G1=-C6U+Xx1,G2=-Xτ+(-Gx2-hx3)dx1+p(x2,x3,τ),G3=g(x1,x2,x3,τ),G4=h(x1,x2,x3,τ). (73)

By taking f = g = h = p = 0.

then,

G1=-C6U,G2=G3=G4=0.

Finally, we get the following Noether symmetry generators

Λ1=x1,Λ2=x2,Λ3=x3,Λ4=τ,Λ5=U,
Λ6=x3x2-x2x3,Λ7=τU,andG1=-U.

4.1.2 Conserved vectors

For Λ1, δ1 = 1, δ2 = δ3 = δ4 = Ψ = 0 and G1=G2=G3=G4=0. Then by Eq (68) we get

Tτ=G1-Lδ4-(Ψ-Ux1δ1-Ux2δ2-Ux3δ3-Uτδ4)LUτ·

This leads to

Tτ=-Ux1Uτ
Tx1=G2-Lδ1-(Ψ-Ux1δ1-Ux2δ2-Ux3δ3-Uτδ4)LUx1,

simplifying the above equation, we get

Tx1=A2Ux12+C3Ux13+Uτ22-B2Ux22-B2Ux32,
Tx2=G3-Lδ2-(Ψ-Ux1δ1-Ux2δ2-Ux3δ3-Uτδ4)LUx2,

this leads to

Tx2=BUx1Ux2+DUx12Ux2
Tx3=G4-Lδ3-(Ψ-Ux1δ1-Ux2δ2-Ux3δ3-Uτδ4)LUx3,

we obtain

Tx3=BUx1Ux3+DUx12Ux3·

For Λ2, δ2 = 1, δ1 = δ3 = δ4 = Ψ = 0 and G1=G2=G3=G4=0. The conserved vector associated with Λ2 represents the conserved quantities associated with ether symmetry Λ2 of the equation. These conserved quantities remain constant over time due to the symmetry provided by Λ2 and follow from Eq (68)

Tτ=-Ux2Uτ,Tx1=AUx1Ux2+C2Ux12Ux2+D2(Ux23+Ux2Ux32),Tx2=-A2Ux12-C6Ux13+Uτ22+B2(Ux22-Ux32)+D2(Ux1Ux22-Ux1Ux32),Tx3=Ux2(BUx3+DUx1Ux3). (74)

For Λ3, δ3 = 1, δ1 = δ2 = δ4 = Ψ = 0 and G1=G2=G3=G4=0. From Eq (68), the conserved vector associated with Λ3 becomes

Tτ=-Ux3Uτ,Tx1=AUx1Ux3+C2Ux12Ux3+D2(Ux22Ux3+Ux33),Tx2=Ux2(BUx3+DUx1Ux3),Tx3=-A2Ux12-C6Ux13+Uτ22+B2(-Ux22+Ux32)+D2(-Ux1Ux22+Ux1Ux32). (75)

For Λ4, we consider δ4 = 1, δ1 = δ2 = δ3 = Ψ = 0 and G1=G2=G3=G4=0. From Eq (68), the conserved vector associated with Λ4 becomes

Tτ=-A2Ux12-C6Ux13-Uτ22-B2(Ux22+Ux32)-D2(Ux1Ux22+Ux1Ux32),Tx1=AUx1Uτ+C2Ux12Uτ+D2(Ux22Uτ+Ux32Uτ),Tx2=Ux2(BUτ+DUx1Uτ),Tx3=Ux3(BUτ+DUx1Uτ). (76)

For Λ5, we follow Ψ = 1, δ1 = δ2 = δ3 = δ4 = 0 and G1=G2=G3=G4=0. From Eq (68), the conserved vector associated with Λ5 becomes

Tτ=Uτ,Tx1=-AUx1-C2Ux12-D2(Ux22+Ux32),Tx2=-(BUx2+DUx1Ux2),Tx3=-(BUx3+DUx1Ux3). (77)

For Λ6, we have δ2 = x3, δ3 = −x2, δ1 = δ4 = 0 and G1=G2=G3=G4=0. From Eq (68), the conserved vector associated with Λ6 becomes

Tτ=(-x3Ux2+x2Ux3)Uτ,Tx1=(AUx1+C2Ux12+D2(Ux22+Ux32))(x3Ux2-x2Ux3),Tx2=-x3(A2Ux12+C6Ux13-Uτ22-B2(Ux22-Ux32)-D2(Ux1Ux22-Ux1Ux32))-yUx2Ux3(B+DUx1),Tx3=x2(A2Ux12+C6Ux13-Uτ22+B2(Ux22-Ux32)+D2(Ux1Ux22-Ux1Ux32))+x3Ux2Ux3(B+DUx1). (78)

For Λ7, we have Ψ = τ, δ1 = δ2 = δ3 = δ4 = 0 and G1=-U,G2=G3=G4=0. From Eq (68), the conserved vector associated with Λ7 becomes

Tτ=-U+τUτ,Tx1=-τ(AUx1+C2Ux12+D2(Ux22+Ux32)),Tx2=-τ(BUx2+DUx1Ux2),Tx3=-τ(BUx3+DUx1Ux3). (79)

5 Damped elastic wave equation

The addition of the damping term Uτ to the non-linear elastic wave Eq (13) transforms it into a non-linear damped elastic wave equation given by

Uττ-AUx1x1-B(Ux2x2+Ux3x3)-CUx1Ux1x1-D(Ux1Ux2x2+Ux1Ux3x3)-2D(Ux2Ux1x2+Ux3Ux1x3)+γUτ=0, (80)

where γ is the damping parameter.

In this section, we present a comprehensive Lie symmetry analysis of the nonlinear damped elastic wave Eq (80).

We assume the following form of the vector field

Λ=δ1x1+δ2x2+δ3x3+δ4τ+ΨU·

The invariance condition for the Eq (80) is

Λ[2](Uττ-AUx1x1-B(Ux2x2+Ux3x3)-CUx1Ux1x1-D(Ux1Ux2x2+Ux1Ux3x3)-2D(Ux2Ux1x2+Ux3Ux1x3)+γUτ)|(6.1)=0. (81)

Upon comparing the coefficients of derivatives of U in the given expressions, we get a set of determining system and solving it, we obtain

δ1x1=δ1x2=δ1x3=δ1τ=δ1U=0,δ4x1=δ4x2=δ4x3=δ4τ=δ4U=0,δ2x1=δ2x2=δ2τ=δ2U=0,δ3x1=δ3x3=δ3τ=δ3U=0,Ψx1=Ψx2=Ψx3=ΨU=0,δ3x2+δ2x3=0,Ψττ+γΨτ=0,δ2x3x3=0, (82)

The infinitesimals we obtain here are given by

δ1=C1,δ2=C2x3+C3,δ3=-C2x2+C4,δ4=C5,Ψ=C6+C7e-γτ.

We follow the following symmetry algebra given by

Λ1=τ,Λ2=U,Λ3=x1,Λ4=x2,Λ5=x3,Λ6=e-γτU,Λ7=x3x2-x2x3·

Table 4 lists the commutator relation for the generators of symmetry algebra (5).

Table 4. Commutator table.

i, Λj] Λ1 Λ2 Λ3 Λ4 Λ5 Λ6 Λ7
Λ1 0 0 0 0 0 γΛ6 0
Λ2 0 0 0 0 0 0 0
Λ3 0 0 0 0 0 0 0
Λ4 0 0 0 0 0 0 - Λ5
Λ5 0 0 0 0 0 0 Λ4
Λ6 γΛ6 0 0 0 0 0 0
Λ7 0 0 0 Λ5 −Λ4 0 0

Following a similar procedure, we obtain the optimal system of symmetry algebra of Eq (80) given by,

R1=Λ1R2=Λ1+κΛ2,κ0R3=Λ1+κΛ3,κ0R4=Λ2R5=Λ3R6=Λ1+κΛ2+σΛ3,κ,σ0R7=Λ1+κΛ2+σΛ4,κ,σ0R8=Λ1+κΛ4,κ0R9=Λ1+κΛ5,κ0R10=Λ1+κΛ7,κ0R11=Λ4R12=Λ5R13=Λ1+Λ2+κΛ3+σΛ4,κ,σ0R14=Λ2+κΛ3,κ0R15=Λ2+κΛ4,κ0R16=Λ2+κΛ5,κ0R17=Λ2+κΛ6,κ0R18=Λ2+κΛ7,κ0R19=Λ3+κΛ4,κ0R20=Λ3+κΛ5,κ0R21=Λ±Λ6R22=Λ6R23=Λ1+κΛ3+σΛ4,κ,σ0R24=Λ7R25=Λ1+Λ2+κΛ3+σΛ5,κ,σ0R26=Λ1+Λ2+κΛ3+σΛ7,κ,σ0R27=Λ4±Λ6R28=Λ2+Λ3+κΛ5+σΛ7,κ,σ0R29=Λ1+κΛ3+σΛ5,κ,σ0R30=Λ1+κΛ2+σΛ5,κ,σ0R31=Λ1+κΛ2+σΛ7,κ,σ0R32=Λ3+κΛ7,κ0R33=Λ5±Λ6R34=Λ6±Λ7R35=Λ1+κΛ3+σΛ7,κ,σ0,

6 Group invariant solutions

Invariant Solutions by Using R1=Λ1.

First, let us consider the infinitesimal generator Λ1=τ·

The characteristic equation associated with Λ1 is given by

dx10=dx20=dx30=dτ1=dU0·

From the characteristic equation, we can deduce that x1 = α, x2 = β, x3 = λ, U = X(α, β, λ). Using these invariant variables, (80) is transformed into the equation given by

(-CXα-A)Xαα+(-DXα-B)Xββ+(-DXα-B)Xλλ-2D(XβXαβ+XλXαλ)=0. (83)

Infinitesimals of (83) are written as

δα=c2α+c5,δβ=-c1λ+c2β+c6,δλ=c1β+c2λ+c3,ΨX=c2X+c4. (84)

Case 1: By taking c5 = 1, c6 = 1 and all other constants zero, the characteristic equation associated with (84) is

dα1=dβ1=dλ0=dX0,

which implies that λ = r, βα = s and X(α, β, λ) = Y(r, s). Using these invariant variables, (83) is transformed into the following equation

((C+3D)Ys-A-B)Yss+(DYs-B)Yrr+2DYrYrs=0. (85)

Infinitesimals of Eq (85) becomes

δr=c1r+c2,δs=c1s+c4,ΨY=c1Y+c3. (86)

Case 1a: By taking c3 = 1, c4 = 1 and all other constants zero, the characteristic equation associated with (86) is

dr0=ds1=dY1,

which implies that r = p and Y(r, s) = s + Z(p). Using these invariant variables, (85) is transformed into the following ODE

-Z(B-D)=0. (87)

This implies,

Z(p)=c1p+c2, (88)

which provides,

Y(r,s)=c1r+c2+s, (89)

this implies,

X(α,β,λ)=c1λ+c2+(β-α). (90)

So, the solution of (80) in original variables is

U(x1,x2,x3,τ)=c1x3+c2+(x2-x1). (91)

Invariant Solutions by Using R5=Λ3.

First, let us consider the infinitesimal generator Λ3=x1·

The characteristic equation associated with Λ3 is given by

dx11=dx20=dx30=dτ0=dU0·

From the characteristic equation, we can deduce that τ = α, x2 = β, x3 = λ, U = X(α, β, λ). Using these invariant variables, (80) is transformed into the equation given by

Xαα-BXββ-BXλλ+γXα=0. (92)

Infinitesimals of (92) are written as

δα=c2Bλ-2γc4β+c13,δβ=-c1λ-2γc4Bα+c12,δλ=c1β+c2α+c3,ΨX=1ea2β(2(c10sin(a2B-a1λB)+c11cos(a2B-a1λB))(e-αγ2+4a12c7+eαγ2+4a12c6)B((ea2β)2c8+c9)e-αγ2+2ea2β((c4β+c5)B-c22γλ)X). (93)

Case 2: By taking c3 = 1 and all other constants zero, the characteristic equation associated with (93) is

dα0=dβ0=dλ1=dX0,

which implies that α = r, β = s, and X(α, β, λ) = Y(r, s). Using these invariant variables, (92) is transformed into the following equation

Yrr-BYss+γYr=0. (94)

Infinitesimals of Eq (94) becomes

δr=-2γc1s+c5,δs=-2γBc1r+c6,ΨY=(c1s+c2)Y+c3(e-a12B(Br+s)4Ba1+γ)4ea1γ(Br+s)4Ba1+γ(eγa1B(-sB+r)8Ba1+2γ)2c4. (95)

Case 2a: By taking c5 = 1, c6 = 1 and all other constants zero, the characteristic equation associated with (95) is

dr1=ds1=dY0,

which implies that −r + s = p and Y(r, s) = s + Z(p). Using these invariant variables, (94) is transformed into the following ODE

Z-BZ-γZ=0. (96)

This implies,

Z(p)=c1+c2e-γpB-1, (97)

which provides,

Y(r,s)=c1+c2e-γ(s-r)B-1, (98)

this implies,

X(α,β,λ)=c1+c2e-γ(β-α)B-1. (99)

So, the solution of (80) in original variables is

U(x1,x2,x3,τ)=c1+c2e-γ(x2-τ)B-1. (100)

Invariant Solutions by Using R12=Λ5.

First, let us consider the infinitesimal generator Λ5=x3·

The characteristic equation associated with Λ5 is given by

dx10=dx20=dx31=dτ0=dU0·

From the characteristic equation, we can deduce that τ = α, x1 = β, x2 = λ, U = X(α, β, λ). Using these invariant variables, (80) is transformed into the equation given by

(-CXβ-A)Xββ+(-DXβ-B)Xλλ-2DXλXβλ+γXα+Xαα=0. (101)

Infinitesimals of (101) are written as

δα=c3,δβ=c4,δλ=c5,ΨX=c1+c2e-αγ. (102)

Case 3: By taking c2 = 1, c5 = 1 and all other constants zero, the characteristic equation associated with (102) is

dα0=dβ0=dλ1=dXe-αγ,

which implies that α = r, β = s, and X(α, β, λ) = λeαγ + Y(r, s). Using these invariant variables, (101) is transformed into the following equation

(-CYs-A)Yss+γYr+Yrr=0. (103)

Infinitesimals of Eq (94) becomes

δr=c3,δs=c1s+c2,ΨY=3c1Y+2ACc1s+c4+c5e-γr. (104)

Case 3a: By taking c2 = 1, c5 = 1 and all other constants zero, the characteristic equation associated with (104) is

dr0=ds1=dYe-γr,

which implies that r = p and Y(r, s) = seγr + Z(p). Using these invariant variables, (103) is transformed into the following ODE

Z+γZ=0. (105)

This implies,

Z(p)=c1+c2e-γp, (106)

which provides,

Y(r,s)=c1+(c2+s)e-γr, (107)

this implies,

X(α,β,λ)=c1+(c2+β)e-γα+λe-αγ, (108)

So, the solution of (80) in original variables is

U(x1,x2,x3,τ)=c1+(c2+x1)e-γτ+x2e-x1γ. (109)

Invariant Solutions by Using R15=Λ2+κΛ4.

First, let us consider the infinitesimal generator Λ2+κΛ4=U+κx2·

The characteristic equation associated with Λ2 + κΛ4 is given by

dx10=dx2κ=dx30=dτ0=dU1·

From the characteristic equation, we can deduce that τ=α,x1=β,x3=λ,U=yκ+X(α,β,λ). Using these invariant variables, (80) is transformed into the equation given by

(-CXβ-A)Xββ+(-DXβ-B)Xλλ-2DXλXβλ+γXα+Xαα=0. (110)

Infinitesimals of (110) are written as

δα=c3,δβ=c4,δλ=c5,ΨX=c1+c2e-αγ. (111)

Case 4: By taking c3 = 1, c4 = 1 and all other constants zero, the characteristic equation associated with (111) is

dα1=dβ1=dλ0=dX0,

which implies that λ = r, −α + β = s and X(α, β, λ) = Y(r, s). Using these invariant variables, (110) is transformed into the following equation

(-CYs-A+1)Yss+(-DYs-B)Yrr-2DYrYrs-γYs=0. (112)

Infinitesimals of Eq (112) becomes

δr=c2,δs=c3,ΨY=c1. (113)

Case 4a: By taking c1 = 1, c3 = 1 and all other constants zero, the characteristic equation associated with (113) is

dr0=ds1=dY1,

which implies that r = p, Y(r, s) = s + Z(p). Using these invariant variables, (112) is transformed into the following ODE

(-B-D)Z-γ=0. (114)

This implies,

Z(p)=-γ2(B+D)p2+c1p+c2, (115)

which provides,

Y(r,s)=-γ2(B+D)r2+c1r+c2+s, (116)

this implies,

X(α,β,λ)=-γ2(B+D)λ2+c1λ+c2+(β-α), (117)

So, the solution of (80) in original variables is

U(x1,x2,x3,τ)=yκ+-γ2(B+D)x32+c1x3+c2+(x1-τ). (118)

Invariant Solutions by Using R6=Λ1+κΛ2+σΛ3.

First, let us consider the infinitesimal generator Λ1+κΛ2+σΛ3=τ+κU+σx1·

The characteristic equation associated with Λ1 + κΛ2 + σΛ3 is given by

dx1σ=dx20=dx30=dτ1=dUκ·

From the characteristic equation, we can deduce that x2=α,x3=β,τ-x1σ=λ,U=κσx1+X(α,β,λ). Using these invariant variables, (80) is transformed into the equation given by

(σ3-Aσ+CXλ-Cκ)Xλλ+σ2((-Bσ+DXλ-κD)Xββ+(-Bσ+DXλ-κD)Xαα+σγXλ+2DXαXαλ+2DXβXβλ)=0, (119)

Infinitesimals of (119) are written as

δα=c1β+c2,δβ=-c1α+c5,δλ=c4,ΨX=c3. (120)

Case 5: By taking c3 = 1, c5 = 1 and all other constants zero, the characteristic equation associated with (120) is

dα0=dβ1=dλ0=dX1,

which implies that α = r, λ = s, and X(α, β, λ) = β + Y(r, s). Using these invariant variables, (119) is transformed into the following equation

(σ3-Aσ+CYs-κC)Yss+2((D2Ys-B2σ-D2κ)Yrr+DYrYrs+σ2γYs)σ2=0. (121)

Infinitesimals of Eq (121) becomes

δr=c2,δs=c3,ΨY=c1. (122)

Case 5a: By taking c1 = 1, c3 = 1 and all other constants zero, the characteristic equation associated with (113) is

dr0=ds1=dY1,

which implies that r = p, Y(r, s) = s + Z(p). Using these invariant variables, (121) is transformed into the following ODE

-((σB+D(κ-1))Z-γσ)σ2=0, (123)

This implies,

Z(p)=-γσ2(σB+D(κ-1))p2+c1p+c2, (124)

which provides,

Y(r,s)=-γσ2(σB+D(κ-1))r2+c1r+c2+s, (125)

this implies,

X(α,β,λ)=-γσ2(σB+D(κ-1))α2+c1α+c2+λ+β, (126)

So, the solution of (80) in original variables is

U(x1,x2,x3,τ)=κσx1+-γσ2(σB+D(κ-1))x22+c1x2+c2+τ-x1σ+x3. (127)

7 Partial noether approach

In cases in which the standard Lagrangian is either unavailable or challenging to ascertain, an alternative approach involves the use of a partial Lagrangian. Conservation laws are then derived using the partial Noether approach, which was introduced by Kara and Mahomed [21].

Partial Lagrangian The mth order differential system (61) can be expressed as follows

Hα=Hα0+Hα1=0, (128)

A function L=L(x,U,U(1),,U(n)),nm, is referred to as a partial Lagrangian of the system (61) if the system (61) can be represented in the form

δLδUα=fαβHβ1

subject to the condition that Hβ10 for a certain β. Here, (fαβ) denotes an invertible matrix.

Partial Noether Symmetries The operator Λ as defined in (62), which fulfills the condition

Λ(L)+L(DiΨi)=Di(Gi)+(Ψϖ-ΨjUjϖ)δLδUϖ,i=1,2,,n,ϖ=1,2,,m, (129)

is classified as a partial Noether symmetry generator, corresponding to the partial Lagrangian L.

Conserved Vectors To find the conserved vector related to the system described by Eq (61), which is associated with a symmetry generator (partial Noether) Λ corresponding to the partial Lagrangian L, we utilize Eq (68).

7.1 Partial Noether approach to Eq (80)

In this subsection, we utilize Noether’s partial approach [21] to derive the conservation laws of Eq (80). Initially, we identify the partial Noether symmetries, which are infinitesimal transformations preserving Eq (80). Subsequently, we established associated conservation laws corresponding to these symmetries. The partial Noether’s approach is a powerful method for uncovering conserved quantities. We assume the partial Lagrangian for Eq (80)

L=AUx122+B2(Ux22+Ux32)+CUx136-Uτ22+D2(Ux1Ux22+Ux1Ux32). (130)

By using the Euler operator (65), we get

δLδU=-γUτ·

7.2 Partial Noether symmetries

The vector field

Λ=δ1x1+δ2x2+δ3x3+δ4τ+ΨU,

is referred to as a partial Noether symmetry of Eq (80) concerning the partial Lagrangian (130) if it fulfills the condition

Λ[1]L+L(Dτδ4+Dx1δ1+Dx2δ2+Dx3δ3)=(Ψ-δ1Ux1-δ2Ux2-δ3Ux3-δ4Uτ)δLδU+DτG1+Dx1G2+Dx2G3+Dx3G4, (131)

where,

Λ[1]=Λ+Ψx1Ux1+Ψx2Ux2+Ψx3Ux3+ΨτUτ,

and Gi(x1,x2x3,τ,U),i=1,2,3,4 are gauge terms. We compare the coefficients of derivatives of U in the above equation, we obtain the determining system, and then solving this system gives

Aδ2x2-Aδ1x1+Aδ3x3+Aδ4τ+2AΨU+CΨx1=0,Bδ1x1-Bδ2x2+Bδ3x3+Bδ4τ+2BΨU+DΨx1=0,Bδ1x1+Bδ2x2-Bδ3x3+Bδ4τ+2BΨU+DΨx1=0,2ΨU+δ1x1+δ2x2+δ3x3-δ4τ+2γδ4=0,3ΨU-2δ1x1+δ2x2+δ3x3+δ4τ=0,3ΨU-δ2x2+δ3x3+δ4τ=0,3ΨU+δ2x2-δ3x3+δ4τ=0,δ1x2=δ1x3=δ1U=0,δ2x1=δ2U=0,δ2x3+δ3x2=0,δ3x1=δ3U=0,δ4x1=δ4x2=δ4x3=δ4U=0,Ψx2=Ψx3=GU3=GU4=0,AΨx1-GU2=0,γΨ-Ψτ-GU1=0,-γδ1+δ1τ=0,-γδ2+δ2τ=0,-γδ3+δ3τ=0,Gτ1+Gx12+Gx23+Gx34=0. (132)

The solution of the above system follows

δ1=C1eγτ,δ2=(C2x3+C3)eγτ,δ3=(-C2x2+C4)eγτ,δ4=0,Ψ=C5+C6eγτ
G1=C5γU-Xx2+(-hx1-Gx3)dt+p(x1,x2,x3),G2=h(x1,x2,x3,τ),
G3=Xτ,G4=g(x1,x2,x3,τ).

By taking f = g = h = p = 0,

we get,

G1=C5γU,G2=G3=G4=0.

Finally, we had the following partial Noether symmetry generators

Λ1=eγτx1,Λ2=eγτx2,Λ3=eγτx2,Λ4=eγτ(x3x2-x2x3),
Λ5=eγτU,Λ6=U,andG1=γU.

7.3 Conserved vectors

For Λ1, we have δ1 = eγτ, δ2 = δ3 = δ4 = Ψ = 0 and G1=G2=G3=G4=0, we follow from Eq (68)

Tτ=G1-Lδ4-(Ψ-Ux1δ1-Ux2δ2-Ux3δ3-Uτδ4)LUτ·

This lead to the component of the conserved vector given by,

Tτ=-eγtUx1Uτ
Tx1=G2-Lδ1-(Ψ-Ux1δ1-Ux2δ2-Ux3δ3-Uτδ4)LUx1,

we get

Tx1=eγτ(A2Ux12+C3Ux13+Uτ22-B2Ux22-B2Ux32),
Tx2=G3-Lδ2-(Ψ-Ux1δ1-Ux2δ2-Ux3δ3-Uτδ4)LUx2,

this implies

Txy=eγτ(BUx1Ux2+DUx12Ux2),
Tx3=G4-Lδ3-(Ψ-Ux1δ1-Ux2δ2-Ux3δ3-Uτδ4)LUx3,

we obtain the result

Tx3=eγτ(BUx1Ux3+DUx12Ux3).

For Λ2, δ2 = eγτ, δ1 = δ3 = δ4 = Ψ = 0 and G1=G2=G3=G4=0. From Eq (68), the conserved vector associated with Λ2 becomes

Tτ=-eγτUx2Uτ,Tx1=eγτ(AUx1Ux2+C2Ux12Ux2+D2(Ux23+Ux2Ux32)),Tx2=eγτ(-A2Ux12-C6Ux13+Uτ22+B2(Ux22-Ux32)+D2(Ux1Ux22-Ux1Ux32)),Tx3=eγτUx2(BUx3+DUx1Ux3). (133)

For Λ3, δ3 = eγτ, δ1 = δ2 = δ4 = Ψ = 0 and G1=G2=G3=G4=0. From Eq (68), the conserved vector associated with Λ3 becomes

Tτ=-eγτUx3Uτ,Tx1=eγτ(AUx1Ux3+C2Ux12Ux3+D2(Ux22Ux3+Ux33)),Tx2=eγτUx2(BUx3+DUx1Ux3),Tx3=eγτ(-A2Ux12-C6Ux13+Uτ22+B2(-Ux22+Ux32)+D2(-Ux1Ux22+Ux1Ux32)). (134)

For Λ4, we have δ2 = x3eγτ, δ3 = −x2eγτ, δ1 = δ4 = Ψ = 0 and G1=G2=G3=G4=0. From Eq (68), the conserved vector associated with Λ4 becomes

Tτ=(-x3Ux2+x2Ux3)eγτUτ,Tx1=eγτ(zUx2-x2Ux3)(AUx1+C2Ux12+D2(Ux22+Ux32)),Tx2=-x3eγτ(A2Ux12+C6Ux13-Uτ22-B2(Ux22-Ux32)-D2(Ux1Ux22-Ux1Ux32))-yUx2Ux3eγτ(B+DUx1),Tx3=x2eγτ(A2Ux12+C6Ux13-Uτ22+B2(Ux22-Ux32)+D2(Ux1Ux22-Ux1Ux32))+zUx2Ux3eγτ(B+DUx1). (135)

For Λ5, Ψ = eγτ, δ1 = δ2 = δ3 = δ4 = 0 and G1=G2=G3=G4=0. From Eq (68), the conserved vector associated with Λ5 becomes

Tτ=eγτUτ,Tx1=eγτ(-AUx1-C2Ux12-D2(Ux22+Ux32)),Tx2=-eγτ(BUx2+DUx1Ux2),Tx3=-eγτ(BUx3+DUx1Ux3). (136)

For Λ6, we have Ψ = 1, δ1 = δ2 = δ3 = δ4 = 0 and G1=γU,G2=G3=G4=0. From Eq (68), the conserved vector associated with Λ6 becomes

Tτ=γU+Uτ,Tx1=-(AUx1+C2Ux12+D2(Ux22+Ux32)),Tx2=-(BUx2+DUx1Ux2),Tx3=-(BUx3+DUx1Ux3). (137)

8 Graphical analysis

In this section, we explore the graphical analysis of the nonlinear elastic wave equations, which proves crucial when dealing with exact solutions. This analysis helps us grasp the intricate nature of complex physical phenomena. Figures labeled as Figs 14 exemplify the interplay of two and three-dimensional motion of elastic waves. Notably, Figs 1 and 2 validate the presence of exponential within the elastic wave equations. These figures are based on specific parameter values, providing valuable insights into the behavior of the elastic waves.

Fig 1. Behaviour of three-dimensional elastic motion by (100) with parameters c1 = 1, c2 = 3, B = 2 and γ = 1.

Fig 1

Fig 4. Behaviour of two-dimensional elastic motion by (109) with parameters c1 = 1, c2 = 2 and γ = 1.

Fig 4

Fig 2. Behaviour of two-dimensional elastic motion by (100) with parameters c1 = 1, c2 = 3, B = 2 and γ = 1.

Fig 2

Fig 3. Behaviour of three-dimensional elastic motion by (109) with parameters c1 = 1, c2 = 2 and γ = 1.

Fig 3

9 Conclusions

In this study, our main objective was to investigate the (3+1)-dimensional elasticity wave equations using the widely employed Lie group method. This research is novel because no previous studies have applied the Lie group method to these equations. Our exploration provides unique analytical solutions that are invariant under certain transformations or symmetry generators, highlighting the novelty of our results. Additionally, we derived the conservation laws of linear momentum and energy within the model. To achieve this, we formulated classical and partial Lagrangians for the elasticity wave equation and its damped version, respectively. This exploration of conservation laws using Noether’s theorem is presented for the first time in the literature for the (3+1)-dimensional elasticity wave equations, as is the application of the partial Lagrangian approach to these models. Our results demonstrate the effectiveness of the partial Lagrangian approach when a classical Lagrangian is unavailable, extending the applications of variational principles.

We accomplished this goal by thoroughly discussing both Noether’s approach and partial Noether’s approach to elasticity equations, resulting in the successful derivation of conserved vectors. The soundness of the Lie group method was confirmed through our analysis. Furthermore, we found that our adopted technique was also suitable for exploring group invariant solutions. The promising results have motivated us to further research and study additional classes within the elasticity medium. These findings pave the way for future investigations in the field of elasticity equations.

Acknowledgments

The authors extend their appreciation to the Deanship of Scientific Research at King Khalid University for funding this work through large group Research Project under grant number RGP.2/16/45.

Data Availability

All relevant data are within the paper.

Funding Statement

The author(s) received no specific funding for this work.

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Data Availability Statement

All relevant data are within the paper.


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