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8/3/2019 001 Cattani and Rushchitskii Int App Mechanics 2003 39 12 http://slidepdf.com/reader/full/001-cattani-and-rushchitskii-int-app-mechanics-2003-39-12 1/39 To the Beginning of the Third Millennium CUBICALLY NONLINEAR VERSUS QUADRATICALLY NONLINEAR ELASTIC WAVES: MAIN WAVE EFFECTS C. Cattani 1 and Ya. Ya. Rushchitskii 2 UDK 539.3 + 524.145 This paper is a review of studies on quadratically and cubically nonlinear elastic waves in elastic materials. The main methods for analysis of the wave equations are demonstrated. The main wave phenomena are described. The disproportion between the achievements in the analyses of quadratically and cubically nonlinear waves is pointed out—cubically nonlinear waves have been studied much less. Keywords: quadratically and cubically nonlinear elastic waves, main wave effects, wave interaction, wave triplets and quadruples, theoretical and computer analysis 1.Introduction. Themain goal of the present review is to establish the level of knowledge on elastic nonlinear waves in materials. It primarily includes various wave effects that have already been detected and described and problems and effects that have not been studied at all or adequately. The present study may be regarded as a development of [14]. As in [14], we consider nonlinear elastic waves within the framework of the modern mechanics of materials with internal structure. The authors call the reader’s attention to the great interest in nanotechnologies shown for the last ten years. Therefore, we may divide the mechanics of materials into macro-, meso-, micro-, and nanomechanics and reinterpret many results on the micromechanics of composite materials in terms of nanomechanics. Thus, the mechanics of materials is still a developing area of science; and waves occupy a significant place in this area. Because the overwhelming majority of investigations on elastic nonlinear waves are concerned with either quadratically nonlinear or cubically nonlinear waves and these latter waves are much less explored, we will chose the scheme of exposition announced in the title—cubically nonlinear waves versus quadratically nonlinear waves. Weprefertoconsiderthisreviewasthesecondpartofthereview[14].Thisrelievesusofintroducingmanypreliminary notions and facts. We will have to do with hyperelastic materials only and will express the Murnaghan elastic potential [19, 21, 23, 55] in terms of the Green strain tensor ε ik , W A B ik mm ik ik im km ik mm ( ) ( ) ( ) ( ) ε λ ε µ ε ε ε ε ε ε = + + + + 1 2 1 3 1 2 2 2 3 3 mm ( ) ε , (1.1) or in terms of the first algebraic invariants of the tensor ε ik , WI I I I I AI BI I CI ( , , ) 1 2 3 12 2 3 1 2 13 1 2 1 3 1 3 = + + + + λ µ , (1.2) where I I ik ik ik  1 2 2 3 3 = = = tr tr tr  ( ), [( ) ], [( ) ] ε ε ε ; λ and µ are the Lamé elastic constants (constants of the second order); and  A, B, and are the Murnaghan elastic constants (constants of the third order).  International Applied Mechanics, Vol. 39, No. 12, 2003 1063-7095/03/3912-1361$25.00 ©2003 Plenum Publishing Corporation 1361 1 Universita di Roma “La Sapienza,” Rome, Italy. 2 S. P. Timoshenko Institute of Mechanics, National Academy of Sciences of Ukraine, Kiev. Published in Prikladnaya Mekhanika, Vol. 39, No. 12, pp. 3–44, December 2003. Original article submitted June 2, 2003.
Transcript
Page 1: 001 Cattani and Rushchitskii Int App Mechanics 2003 39 12

8/3/2019 001 Cattani and Rushchitskii Int App Mechanics 2003 39 12

http://slidepdf.com/reader/full/001-cattani-and-rushchitskii-int-app-mechanics-2003-39-12 1/39

To the Beginning of the Third Millennium

CUBICALLY NONLINEAR VERSUS QUADRATICALLY NONLINEAR ELASTIC WAVES:

MAIN WAVE EFFECTS

C. Cattani1 and Ya. Ya. Rushchitskii2 UDK 539.3 + 524.145

This paper is a review of studies on quadratically and cubically nonlinear elastic waves in elastic

materials. The main methods for analysis of the wave equations are demonstrated. The main wave

phenomena are described. The disproportion between the achievements in the analyses of quadratically

and cubically nonlinear waves is pointed out—cubically nonlinear waves have been studied much less.

Keywords: quadratically and cubically nonlinear elastic waves, main wave effects, wave interaction, wave

triplets and quadruples, theoretical and computer analysis

1. Introduction. Themain goal of the present review is to establish the level of knowledge on elastic nonlinear waves in

materials. It primarily includes various wave effects that have already been detected and described and problems and effects that

have not been studied at all or adequately. The present study may be regarded as a development of [14]. As in [14], we consider 

nonlinear elastic waves within the framework of the modern mechanics of materials with internal structure. The authors call the

reader’s attention to the great interest in nanotechnologies shown for the last ten years. Therefore, we may divide the mechanics

of materials into macro-, meso-, micro-, and nanomechanics and reinterpret many results on the micromechanics of composite

materials in terms of nanomechanics. Thus, the mechanics of materials is still a developing area of science; and waves occupy a

significant place in this area.

Because the overwhelming majority of investigations on elastic nonlinear waves are concerned with either quadratically nonlinear or cubically nonlinear waves and these latter waves are much less explored, we will chose the scheme of 

exposition announced in the title—cubically nonlinear waves versus quadratically nonlinear waves.

We prefer to consider this review as the second part of the review [14]. This relieves us of introducing many preliminary

notions and facts. We will have to do with hyperelastic materials only and will express the Murnaghan elastic potential [19, 21,

23, 55] in terms of the Green strain tensor ε ik ,

W A Bik mm ik ik im km ik mm( ) ( ) ( ) ( )ε λ ε µ ε ε ε ε ε ε= + + + +1

2

1

3

12 2 2

33C  mm( )ε , (1.1)

or in terms of the first algebraic invariants I k  of the tensor ε ik ,

W I I I I I AI BI I CI  ( , , )1 2 3 12 2 3 1 2 13

1

2

1

3

1

3= + + + +λ µ , (1.2)

where I I I ik ik ik  1 22

33= = =tr tr tr  ( ), [( ) ] , [( ) ]ε ε ε ; λ and µ are the Lamé elastic constants (constants of the second order); and

 A, B, and C are the Murnaghan elastic constants (constants of the third order).

 International Applied Mechanics, Vol. 39, No. 12, 2003

1063-7095/03/3912-1361$25.00 ©2003 Plenum Publishing Corporation 1361

1Universita di Roma “La Sapienza,” Rome, Italy. 2S. P. Timoshenko Institute of Mechanics, National Academy of 

Sciences of Ukraine, Kiev. Published in Prikladnaya Mekhanika, Vol. 39, No. 12, pp. 3–44, December 2003. Original article

submitted June 2, 2003.

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Also, we will consider nonlinear waves in the context of the microstructural theory of elastic mixtures and discuss

two-phase elastic mixtures. This theory describes the kinematic picture of a deformation process using two partial displacement

vectorsru ( )α (as a rule, the Roman indices take the values 1, 2, and 3 and the Greek indices, 1 and 2) and, hence, includes two

different macrostrain tensors ε αik ( )

. A mixture as a whole and its internal energy are described using two different kinematic

 parameters: partial strain tensors ε αik ( )

and relative displacement vector r r rv u u= −( ) ( )1 2 (other alternatives are also possible, such

as Tiersten’s [63, 66]),

( )W W vik ik  = ε ε( ) ( )

, ,1 2 r

. (1.3)

The first modification of the Murnaghan potential follows from (1.3), where both the quadratic and cubic terms of the

 potential (i.e., the linear and quadratic terms of the constitutive equations) account for the cross-influence:

( )W vik ik   k  ik ik ik  ( , , )( ) ( ) ( ) ( ) ( )ε ε µ ε µ ε ε λα

α α δα

1 2 2

321

2= + + ( )ε λ ε εα α δ

mm mm mm( ) ( ) ( )2

3+

( ) ( )+ + +1

3

1

3

2  A B C  ik  im km mm ik  mmα

α α αα

α αα

αε ε ε ε ε ε( ) ( ) ( ) ( ) ( ) ( ) 3

+ + +1

3 23 3 3  A B C  ik  im km mm ik ik   mε ε ε ε ε ε εα δ δ δ δ α( ) ( ) ( ) ( ) ( ) ( )

( )m mm k k  v v( ) ( ) ( ) ( )α δε β β2

2 31

3+ + ′ . (1.4)

This potential includes seven elastic constants of the second order, λ µk k , , and β, and ten elastic constants of the third

order, A B C k k k , , , and ′β .

The second mixture modification of the Murnaghan potential is based on some simplification: the quadratic terms of the

 potential (the linear terms of the constitutive equations) account for the cross-influence and the cubic terms (the quadratic terms

of the constitutive equations) do not:

( )W vik ik   k  ik ik ik  ( , , )( ) ( ) ( ) ( ) ( )ε ε µ ε µ ε ε λα

α α δα

1 2 2

321

2= + + ( )ε λ ε εα α δ

mm mm mm( ) ( ) ( )2

3+

( ) ( )+ + +

1

3

1

3

2

  A B C  ik  im km mm ik  mmαα α α

αα α

αα

ε ε ε ε ε ε( ) ( ) ( ) ( ) ( ) ( ) 3

2 3

+ + ′β β( ) ( )v vk k  . (1.5)

This potential includes seven elastic constants of the second order λ µk k , , and β, and seven elastic constants of the third

order, A B C α α α, , , and ′β .

In what follows, we will discuss nonlinear elastic waves within the framework of two microstructural theories: the

theory of effective moduli (the classical nonlinear theory of elasticity) and the theory of two-phase elastic mixtures.

1.1. First Microstructural Model (Classical Nonlinear Theory of Elasticity). Let us start with the classical model,

recalling the transition from the internal-energy representation to wave equations [3, 4, 19, 55, 94].

In their pioneering studies, Goldberg [18] and Jones and Kobett [20], who initiated a large series of investigations on

nonlinear plane elastic waves (see [17, 21, 55, 94] and references therein), simplified representation (1.1), which is cubically

nonlinear with respect to the strain tensor, as follows:

( ) ( )W W u u um m i k k i= = + +( , ), , ,

2 32 21

2

1

4λ µ ( ) ( )+ + 

   

   + +µ λ

1

4

1

2

2  A u u u B u ui k m k m i m m i k  , , , , ,

( )+ + +1

12

1

2

1

3

3  Au u u Bu u u C ui k k m m i i k k i m m m m, , , , , , , . (1.6)

 Remark 1.1. The superscript (2, 3) means that the expression for the potential contains terms of the second and third

orders or, which is the same, the constitutive equations contain linear and quadratically nonlinear terms. An elastic medium may

 be called quadratically nonlinear, implying that the linear deformation mechanism is included.

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Potential (1.6) is still cubically nonlinear and still provides the quadratic nonlinearity of the basic system of equations.

However, it is nonlinear with respect to the deformation gradient rather than to the strain tensor.

Because of the nonlinearity of the Green strain tensor, the full, exact representation of the potential includes not only

terms of the second and third orders with respect to the deformation gradient but also terms of the fourth to sixth orders:

( ) ( )W u u u A u u um m i k k i i k m k m i= + + + +    

  

1

2

1

4

1

4

2 2λ µ µ, , , , , ,

( ) ( )+ + + + +1

2

1

12

1

2

12λ B u u Au u u Bu u um m i k i k k m m i i k k i m m, , , , , , , , ( )

3

3C um m,

( ) ( ) ( ) ( )+ + + + +1

4

1

4

1

8

4 2λ µu u u A u u u u u un m n i n k i k k i i m m i s k s, , , , , , , ,[ ,m

( )( ) ( ) ( )+ + + + + +u u u u u u u u u u ui k k i k m m k s i s m i m m i k m m k s i, , , , , , , , , , , ]u s k ,

( ) ( )+ + + +1

2

1

2 B u u u u u u u u u u ui k k i n i n k m m i k k i i k i k n m, , , , , , , , , , ( ) ( )n m m m n mC u u, , ,

+3

2

2 2

( ) ( ) ( )[ ( ) ( )+ + + +1

24 A u u u u u u u u u u ui k k i s i s m l k l m i m m i n i n k l  , , , , , , , , , , ( ), ,k l mu

( ) ( ) ( )] ( )+ + + + +u u u u u u B u u u u uk m m k n i n k s i s k n i n k m m i k  , , , , , , , , , ,

1

4

2 ( ) ( )k i n i n k s mu u u, , , ,

2

( ) ( ) ( ) ( )+ +1

12

1

24

4Cu u A u u u u u um m n m n i n k s i s m l k l m, , , , , , , , ( ) ( ) ( )+ +

1

8

1

24

2 2 6  B u u u C un i n k s m n m, , , , . (1.7)

Thus, potential (1.7) describes not only the quadratic nonlinearity of the constitutive equations, as in (1.6), but also

nonlinearities of the third to fifth orders. Potential (1.6) includes only the first two lines of (1.7), the other lines being neglected.

Therefore, according to (1.6), the Lamé equations of motion and the basic equations for plane polarized waves are quadratically

nonlinear. Recall the transition from potential (1.6) to these equations.

The Lamé equations of motion can be derived in two steps. We start with the simplified potential (1.6), derived from

(1.7) by discarding the above-mentioned seven lines.

Step 1. Write the formula for Kirchhoff stresses (so-called constitutive equations) according to the relationship

t W uik i k  = ∂ ∂( / ), :

( )t u u uik i k k i k k ik  = + +µ λ δ, , ,( )[ ]( )+ + + +µ 1 4 2/ , , , , , , A u u u u u ul i l k i l k l l k i l  

( ) ( ) ( )+ − +

+1 2 2 1 4

2/ ( ) /, , , , ,  B u u u Au um l ik i k l l k l l iλ δ ( ) ( )+ + +  B u u u u C ul m m l ik k i l l l l ik  , , , , ,δ δ2

2. (1.8)

Step 2. Substitute (1.8) into the equations of motion t X uik i k k  ,··+ = ρ to obtain a nonlinear analogy for the classical

Lamé equations:

ρ µ λ µ·· ( ), ,u u u F  m m kk n mn m− − + = . (1.9)

All the nonlinear terms are collected on the right-hand side:

[ ]( )  F A u u u u u ui l kk l i l kk i l i lk l k  = + + +µ / , , , , , ,4 2 [ ]( )+ + + + +λ µ A B u u u ul ik l k k lk i l  / , , , ,4

( ) ( ) [ ]+ + + + + + +λ B u u B C u u A B u u u ui kk l l k ik l l k lk l i l ik k  , , , , , , ,/2 4 ( ),l  . (1.10)

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It is common practice to start studying plane polarized waves and corresponding wave equations with the

above-mentioned pioneering papers. This procedure is described in [14] for the equations of motion in the classical theory of 

elasticity. Recall the main assumption: plane waves propagate along the abscissa axis,

{ }ru u x t  k = ( , )1 . (1.11)

Substituting (1.11) into the well-known Christoffel equation, we obtain one longitudinal plane wave ( P -wave) and two

transverse plane waves (horizontally polarized wave (SH -wave) and vertically polarized wave (SV -wave)). The correspondinglinear equations have the form

ρ λ µ·· ( ) ,u u1 1 112 0− + = , ρ µ··,u u2 2 11 0− = , ρ µ··

,u u3 3 11 0− = . (1.12)

Taking (1.12) into account, from (1.6) we obtain

( ) ( ) ( ) ( )( ) ( )( )W u u u u( , ), , , ,/ / /2 3

1 1

2

1 1

2

2 1

2

3 1

21 2 1 2 1 2= + + +

λ µ

[ ] ( ) ( ) ( ) ( ) ( ) ( )+ + + +

+ + +µ λ  A u u u u B u u u/ /, , , , , ,4 1 21 1 1 1

2

2 1

2

3 1

2

1 1 1 1

2

2( ) ( ), ,1

2

3 1

2+

u

( ) ( ) ( ) ( ) ( ) ( ) ( ) ( )( ) ( )+ + + = + +1 12 1 2 1 3 1 2 21 1

3

1 1

3

1 1

3

1 1

2

2 1/ / / /, , , , ,  A u B u C u u uλ µ µ ( )2

3 1

2

+ u ,

[ ]( ) ( )( ) ( ) ( )+ + + + + + + +

µ λ λ/ / / /, , , ,2 3 3 1 21 1

3

1 1 2 1

2

3 1

2  A B C u B u u u . (1.13)

And the constitutive equations become simpler:

( ) ( ) ( )[ ]( )t u A B C u112 3

1 1 1 1

22 3 2 2 2 3

( , ), ,/= + + + + + +λ µ λ µ [ ] ( ) ( )+ + + + +

1

22 2 2 1

2

3 1

2λ µ A B u u/ , , ,

( )[ ]t u A B u u122 3

2 1 1 1 2 11 2 2 2( , )

, , ,/ /= + + + +µ λ µ ,

( )[ ]t u A B u u132 3

3 1 1 1 3 11 2 2 2( , ), , ,/ /= + + + +µ λ µ . (1.14)

Substituting (1.14) into the equations of motion yields quadratically nonlinear wave equations for three polarized plane

elastic P -, SH -, and SV -waves:

( ) ( )ρ λ µu u N u u N u u u utt 1 1 11 1 1 11 1 1 2 2 11 2 1 3 11 3 12, , , , , , , ,− + = + + , (1.15)

( )ρ µu u N u u u utt 2 2 11 2 2 11 1 1 1 11 2 1, , , , , ,− = + , (1.16)

( )ρ µu u N u u u utt 3 3 11 2 3 11 1 1 1 11 3 1, , , , , ,− = + , (1.17)

where

( ) ( )[ ]  N A B C N A B1 23 2 2 3 21

2= + + + + = + + +λ µ λ µ, .

Let us now compare the linear wave equations (1.12) and the nonlinear equations (1.15)–(1.17). As is seen, the linear 

and quadratically nonlinear terms appear separately on the right-hand side of Eqs. (1.15)–(1.17), which is very convenient for 

further analysis.

The next section is fully devoted to quadratically nonlinear waves, including Eqs. (1.15)–(1.17).

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Continue the analysis of the exact expression (1.7) for the Murnaghan potential. Here the question naturally arises of 

whether there are sound restrictions on retaining the terms of the fourth to sixth orders in the representation of the potential. We

are not aware of such restrictions. Therefore, let the expression of the potential contain terms up to the fourth order inclusive:

( ) ( )W u u u A

u um m i k k i i k m( , , )

, , , , ,2 3 4

2 21

22

1

4 4= + + + +

    

  λ µ µ k m iu ,

( ) ( )+ + + + +1

2

1

12

1

2

12

λ B u u Au u u Bu u um m i k i k k m m i i k k i m m, , , , , , , , ( )3

3

C um m,

( ) ( )+ +1

4

1

4

4 2λ µu u un m n i n k  , , , ( ) ( )[+ + +

1

8A u u u u u ui k k i i m m i s k s m, , , , , ,

( )( )+ + + +u u u u u ui k k i k m m k s i s m, , , , , , ( ) ( ) ]u u u u u ui m m i k m m k s i s k  , , , , , ,+ +

( ) ( )+ + + +1

2

1

2 B u u u u u u u u u u ui k k i n i n k m m i k k i i k i k n m, , , , , , , , , , ( ) ( )n m m m n mC u u, , ,

+3

2

2 2(1.18)

or 

W W ( , , ) ( , )2 3 4 2 3= ( ) ( ) ( ) ( ) ( ) ( ) ( )+ + + + +1 8 1 4 1 244 2

/ / /, , , , , , ,λ µu u u A u u u u un m n i n k i k k i i m m i s[ , ,k s mu

( )( )+ + +u u u u u ui k k i k m m k s i s m, , , , , , ( ) ( ) ]+ + +u u u u u ui m m i k m m k s i s k  , , , , , ,

( ) ( )( )+ + + +1

21 2 B u u u u u u u u u ui k k i n i n k m m i k k i i k i k n m, , , , , , , , , ,/[ ] ( ) ( )u C u un m m m n m, , ,+

3

2

2 2. (1.19)

 Remark 1.2. The superscript (2, 3, 4) means that the expression for the Murnaghan potential includes terms of the fourth

order with respect to the deformation gradient in addition to the terms of the second and third orders. Therefore, the

corresponding constitutive equations include cubically nonlinear terms beside the linear and quadratically nonlinear terms. This

elastic medium may be called cubically nonlinear after its highest nonlinearity, implying that the linear and quadratically

nonlinear deformation mechanisms are included.

 Remark 1.3. It is worthy of notice that the terms of the fifth and sixth orders contain only the Murnaghan constants as

factors, whereas the terms of the second to fourth orders include only the Lamé constants.

For plane waves (1.11), potential (1.18) can be simplified considerably:

( )( ) ( ) ( ) ( )W W A B u u u( , , ) ( , ), , ,/2 3 4 2 3

1 1

2

2 1

2

3 1

2 2

1 8 2 2= + + + + + +

λ µ

( ) ( )( ) ( ) ( ) ( )+ + + + +

1 8 3 10 4 1 1

2

1 1

2

2 1

2

3 1

2/ , , , ,  A B C u u u u . (1.20)

The constitutive equations become

( ) ( )[ ]( )t t A B C u112 3 4

112 3

1 1

31 2 2 4 3

( , , ) ( , ),/= + + + + +λ µ

( ) ( )[ ] ( ) ( ) ( )+ + + + + +

1 4 2 2 5 14 4 1 1 2 1

2

3 1

2/ , , ,λ µ A B C u u u ,

( )[ ]( )t t A B u122 3 4

122 3

2 1

31 4 2 2

( , , ) ( , ),/= + + + +λ µ

( ) ( )[ ] ( ) ( ) ( ) ( )+ + + + + + + +1 4 2 2 5 14 4 1 2 3 10 42 1 1 1

2

2 1 3 1

2/ /, , , ,λ µ A B C u u A B C u u ,

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( ) [ ]( )t t A B u132 3 4

132 3

3 1

31 2 2 2

( , , ) ( , ),/= + + + +λ µ

( ) ( )[ ] ( ) ( ) ( ) ( )+ + + + + + + +1 4 2 2 5 14 4 1 4 3 10 43 1 1 1

2

3 1 2 1

2/ /, , , ,λ µ A B C u u A B C u u . (1.21)

The plane polarized wave equations, which include both quadratic and cubic nonlinearities, can be written as

( ) ( )ρ λ µu u N u u N u u u utt 1 1 11 1 1 11 1 1 2 2 11 2 1 3 11 3 12, , , , , , , ,− + = + + ( ) ( )+ + + N u u N u u u u u u3 1 11 1 1

2

4 2 11 2 1 1 1 3 11 3 1 1 1, , , , , , , , , (1.22)

( )ρ µu u N u u u utt 2 2 11 2 2 11 1 1 1 11 2 1, , , , , ,− = + ( ) ( ) ( )+ + + N u u N u u N u u4 2 11 2 1

2

5 2 11 1 1

2

6 2 11 3 1

2

, , , , , , , (1.23)

( )ρ µu u N u u u utt 3 3 11 2 3 11 1 1 1 11 3 1, , , , , ,− = + ( ) ( ) ( )+ + + N u u N u u N u u4 3 11 3 1

2

5 3 11 1 1

2

6 3 11 2 1

2

, , , , , , , (1.24)

where

( )( ) ( ) ( ) ( )[ ]  N A B C N A B C  3 43 2 2 6 3 1 2 2 2 5 14 4= + + + + = + + + +/ , /λ µ λ µ ,

( )( )  N A B N A B C  5 63 2 2 2 3 10 4= + + + = + +/ , .λ µ

1.2. Second Microstructural Model (Nonlinear Theory of Two-Phase Elastic Mixtures). Recall that the Murnaghan

 potential can be written in two forms: (1.4) and (1.5). We will discuss potential (1.5) because its expression is most simple and

concise. Our goal is to derive a system of wave equations similar to (1.15)–(1.17) (quadratically nonlinear elastic mixture) and to

(1.22)–(1.24) (cubically nonlinear elastic mixture).

We start with the general case where the expression for the potential includes all nonlinearities and is written in terms of 

the deformation gradient:

( ) ( )W u u u u um m m m m m i k k i= + + +1

2

1

4

2

31 2λ λ µα

αα

α α,

( ),

( ),

( ),

( ),

(( ) ( )( )),

( ),

( ),

( ),

( )2

31 1 2 21

2+ + +µ u u u ui k k i i k k i

( )+ + 

 

 

   + +µ λα α

α α αα α

α1

4

1

2

  A u u u B ui k m k   m i m m,( )

,( )

,( )

,( )

( )ui k ,

( )α 2+ +

1

12

1

2

 A u u u B u u ui k k m m i i k k i m mαα α α

αα α

,( )

,( )

,( )

,( )

,( )

,

( )

( ),

( )αα

α+

1

3

3C um m

( ) ( )+ + + +1

4

1

4

1

8

4 2λ µα

αα

α αα

αu u u A u un m n i n k i k k i,

( ),

( ),

( ),

( ),( )( )[ ( )

,( )

,( )

,( )

,( )α α α α α

u u u ui m m i s k  s m+

( )( )+ + + +u u u u u u ui k k i k m m k   s i s m i m,( )

,( )

,( )

,( )

,( )

,( )

,α α α α α α ( )( ) ]( )

,( )

,( )

,( )

,( )

,( )α α α α α α

+ +u u u u um i k m m k   s i s k 

( )+ + +1

2

1

2  B u u u u u ui k k i n i n k  m m i k α

α α α α α α,

( ),

( ),

( ),

( ),

( ),

(( )),

( ),

( ),

( ),

( ),

( )u u u u uk i i k i k   n m n m

α α α α α+

( ) ( ) ( )+ + +3

2

1

24

2 2C u u A u u u um m n m i k k i s iα

α αα

α α α,

( ),

( ),

( ),

( ),

( )( )( )[ s m l k l mu u,( )

,( )

,( )α α α

( )( )( )+ + +u u u u u u ui m m i n i n k l k l m k m,( )

,( )

,( )

,( )

,( )

,( )

,(α α α α α α ( )( )( )]α α α α α α)

,( )

,( )

,( )

,( )

,( )+ u u u u um k  n i n k  s i s k 

( ) ( )+ + +1

4

2  B u u u u u un i n k  m m i k k i n iα

α α α α α α,

( ),

( ),

( ),

( ),

( ),

( ) ( )u un k  s m,( )

,( )α α 2

( ) ( )+ +1

12

1

24

4C u u A u u u um m n m n i n k  s i sα

α α α α α,

( ),

( ),

( ),

( ),

( ),( )( )m l k l mu u

( ),

( ),

( )α α α

( ) ( ) ( )+ + +1

8

1

24

2 2 6 1  B u u u C u f un i n k  s m n m n nα

α α αα

α,

( ),

( ),

( ),

( ) ( )( )− un( )2

. (1.25)

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Here the summation is made over α.

The simplest case of quadratic nonlinearity in the constitutive equations follows from (1.25) when only quadratically

and cubically nonlinear terms are retained:

( )W vik ik   k  ik ik ik  ( , ) ( ) ( ) ( ) ( ) ( )

( , , )2 3 1 2 2

32ε ε µ ε µ ε εαα α δ= + ( )+ +

1

2

2

3λ ε λ ε εαα α δ

mm mm mm( ) ( ) ( )

( ) ( )+ + +

1

3

1

3

2

  A B C  ik  im km mm ik  mmα

α α α

α

α α

α

α

ε ε ε ε ε ε( ) ( ) ( ) ( ) ( ) ( ) 3

2 3

+ + ′β β( ) ( )v vk k  . (1.26)

Here we can apply procedure (1.8)–(1.11), (1.13)–(1.17), resulting in the following important relations:

(i) the nonlinear constitutive equations

( ) ( )t u u u u uik i k k i i k k i i k  ( )

,( )

,( )

,( )

,( )

,(α

αα α δ δ

αµ µ λ= + + + +3α δδ λ δ)

,( )

ik  i k  ik u+ 3 [ ]+ + + +µα αα α α α α

  A u u u u u ul i l k i l k l l k i l  / ,( )

,( )

,( )

,( )

,( )

,4 2( )( )α

( ) ( ) ( )+ − +

+1 2 2 1 4

2/ ( ) /,

( ),

( ),

( )  B u u u A um l  ik  i k l l k  α α

α α ααλ δ ,

( ),

( )l l iu

α α ( ) ( )+ + +  B u u u u C ul m m l   ik  k i l l l l   ik αα α α α

ααδ δ,

( ),

( ),

( ),

( ),

( )2

2, (1.27)

(ii) the nonlinear equations of motion

ρ µ λ µαα α α α α α α·· ( )( ),

( ),

( )u u um m kk  n mn− − + ( )− − + + − =µ λ µ βδ δ α δ α3 3 3u u u u F  m kk  n mn m m m,( )

,( ) ( ) ( ) ( )( ) , (1.28)

(iii) the components of the nonlinear partial “volume” force

[ ]  F A u u u u ui l kk l i l kk i l i l  ( )

,( )

,( )

,( )

,( )

,/α

α αα α α α

µ= + + +4 2( )k l k u( )

,( )α α [ ]( )+ + + + +λ µα α α α

α α α α  A B u u u ul ik l k k lk i l  / ,

( ),

( ),

( ),

( )4

( ) ( )+ + + + + +λα αα α

α αα α

α B u u B C u u A Bi kk l l k ik l l  ,( )

,( )

,( )

,( )

/2 4[ ]( )αα α α α

u u u uk lk l i l ik k l  ,( )

,( )

,( )

,( )+ , (1.29)

(iv) the plane wave representation

( ){ }ru u x t  k 

( ) ( ),α α= 1 , (1.30)

and

(v) the basic system of nonlinear wave equations

( ) ( )ρ λ µ λ µααα

α αα δ

u u utt 1 1 11 3 3 1 112 2,( )

,( )

,( )

− + − + = + +  N u u N u u u1 1 11 1 1 2 2 11 2 1 3 11( )

,( )

,( ) ( )

,( )

,( )

,(α α α α α α α( ))

,( )

u3 1α

, (1.31)

ρ µ µααα

αα δ α α

u u u N u utt 2 2 11 3 2 11 2 2 11 1,( )

,( )

,( ) ( )

,( )

,− − = ( )1 1 11 2 1( )

,( )

,( )α α α+ u u , (1.32)

ρ µ µααα

αα δ α α

u u u N u utt 3 3 11 3 3 11 2 3 11 1,( )

,( )

,( ) ( )

,( )

,− − = ( )1 1 11 3 1( )

,( )

,( )α α α+ u u , (1.33)

( ) ( )[ ]  N A B C N A B1 23 2 2 3 2

1

2

( ) ( )

α α α α αα

α α α αλ µ λ µ= + + + + = + + + . (1.34)

Thus, the coupled system of six equations (1.31)–(1.33) (each formula in (1.31)–(1.33) represents a coupled system of 

two equations, and Eqs. (1.31)–(1.33) are coupled through nonlinear terms) describes quadratically nonlinear plane waves in

two-phase elastic mixtures.

Let us now pass to cubically nonlinear mixtures and write the corresponding potential:

( ) ( )W v W vik ik   k  ik ik   k ( , , ) ( ) ( ) ( , ) ( ) ( )

, , , ,2 3 4 1 2 2 3 1 2ε ε ε ε= ( ) ( ) ( ) ( )+ +1 8 1 44 2

/ /,( )

,( )

,( )λ µα

αα

α αu u un m n i n k 

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( ) ( )( )+ + +1 24/ ,( )

,( )

,( )

,( )

,( )

,(

  A u u u u u ui k k i i m m i s k  s mαα α α α α α[ )

( )( )+ + +u u u u u ui k k i k m m k   s i s m,( )

,( )

,( )

,( )

,( )

,( )α α α α α α ( )( ) ]+ + +u u u u u ui m m i k m m k   s i s k ,

( ),

( ),

( ),

( ),

( ),

( )α α α α α α

( ) ( ) ( )+ + +1 2 1 2/ /,( )

,( )

,( )

,( )

,( )

,  B u u u u u ui k k i n i n k  m m i k αα α α α α ( )[ ]( )

,( )

,( )

,( )

,( )

,( )α α α α α α

u u u u uk i i k i k   n m n m+ ( ) ( ) ( )+ 3 22 2

/ ,( )

,( )

C u um m n mαα α

. (1.35)

In the case of plane waves (1.30), potential (1.35) can be written in a simpler form:

( )( ) ( ) ( )W W A B u u( , , ) ( , ),

( ),

( )/2 3 4 2 3

1 1

2

2 1

21 8 2 2= + + + + + +λ µα α α α

α α ( )u3 1

2 2

,( )α

( )( )( ) ( ) ( ) ( )+ + + + +

1 8 3 10 4 1 1

2

1 1

2

2 1

2

3 1

2/ , ,

( ),

( ),

( )  A B C u u u uα α α

α α α . (1.36)

The constitutive equations take the following form (only one third of them are written below)

( ) ( )[ ] ( )t t A B C u112 3 4

112 3

1 1

31 2 2 4 3

( , , ) ( , ),

( )/= + + + + +λ µα α α α α

α

( ) ( )[ ]( ) ( ) ( )+ + + + + +1 4 2 2 5 14 4 1 1 2 1

2

3 1

2/ ,( ) ,( ) ,( )λ µα α α α α α α α  A B C u u u ,

( )[ ]( )t t A B u122 3 4

122 3

2 1

31 4 2 2

( , , ) ( , ),

( )/= + + + +λ µα α α α

α

( )[ ] ( )+ + + + +1

42 2 5 14 4 2 1 1 1

2λ µα α α α α

α α  A B C u u,

( ),

( ) ( ) ( )+ + +1

23 10 4 2 1 3 1

2  A B C u uα α α

α α,

( ),

( ),

( )[ ]( )t t A B u132 3 4

132 3

3 1

31 4 2 2

( , , ) ( , ),

( )/= + + + +λ µα α α α

α

( )[ ] ( )+ + + + +1

42 2 5 14 4 3 1 1 1

2λ µα α α α α

α α  A B C u u,

( ),

( ) ( ) ( )+ + +1

23 10 4 3 1 2 1

2  A B C u uα α α

α α,

( ),

( ).

The coupled system of equations for plane polarized waves, which includes both quadratic and cubic nonlinearities, can

 be written as

( ) ( )ρ λ µ λ µααα

α αα δ

u u utt 1 1 11 3 3 1 112 2,( )

,( )

,( )− + − + = + +  N u u N u u u1 1 11 1 1 2 2 11 2 1 3 11

( ),

( ),

( ) ( ),

( ),

( ),

(α α α α α α α( )),

( )u3 1

α

( )+ +  N u u N u u u3 1 11 1 1

2

4 2 11 2 1 1 1( )

,( )

,( ) ( )

,( )

,( )

,( )α α α α α α α( )+ u u u3 11 3 1 1 1,

( ),

( ),

( )α α α, (1.37)

ρ µ µααα

αα δ α α

u u u N u utt 2 2 11 3 2 11 2 2 11 1,( )

,( )

,( ) ( )

,( )

,− − = ( )1 1 11 2 1( )

,( )

,( )α α α+ u u

( ) ( )+ + +  N u u N u u N  4 2 11 2 1

2

5 2 11 1 1

2

6( )

,( )

,( ) ( )

,( )

,( ) ( )α α α α α α α

( )u u2 11 3 1

2

,( )

,( )α α

, (1.38)

ρ µ µααα

αα δ α α

u u u N u utt 3 3 11 3 3 11 2 3 11 1,( )

,( )

,( ) ( )

,( )

,− − = ( )1 1 11 3 1( )

,( )

,( )α α α

+ u u

( ) ( )+ + +  N u u N u u N  4 3 11 3 1

2

5 3 11 1 1

2

6( )

,( )

,( ) ( )

,( )

,( ) ( )α α α α α α α ( )u u3 11 2 1

2

,( )

,( )α α

, (1.39)

where the constants N N N 3 4 5( ) ( ) ( )

, ,α α α

, and N 6( )α

are defined by

( )( ) ( )  N A B C  3 3 2 2 6 3( )

α α α α αλ µ= + + + + ,

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( ) ( )[ ]  N A B C  4 1 2 2 2 5 14 4( )

α α α α αλ µ= + + + + ,

( )( )  N A B N A B C  5 63 2 2 2 3 10 4( ) ( )

/ ,α

α α α αα

α α αλ µ= + + + = + + . (1.40)

Thus, we have derived the basic systems of wave equations for a quadratically nonlinear elastic medium, (1.15)–(1.17),

and for a cubically nonlinear elastic medium, (1.22)–(1.24), (the microstructural theory of the first order—the theory of effective

moduli) and the basic systems of wave equations for a quadratically nonlinear elastic medium, (1.31)–(1.33), and for a cubically

nonlinear elastic medium, (1.37)–(1.39), (the microstructural theory of the second order—the theory of two-phase mixtures).

The next section is devoted to an analysis of these systems.

2. Quadratically Nonlinear Elastic Waves. In this section, we will consider two types of quadratically nonlinear 

elastic plane waves: harmonic (periodic) waves and solitary (aperiodic) waves. Moreover, using the system of equations

obtained above, we will discuss each type of waves in the context of two different theoretical microstructural approaches: the

first-order theory of effective moduli and the second-order theory of two-phase mixtures.

2.1. Harmonic (Periodic) Waves by the Microstructural Theory of the First Order. We will start with the basic system

of wave equations (1.15)–(1.17).

According to [14], three different approaches are mainly used to analyze Eqs. (1.15)–(1.17): the method of successive

approximations, the method of slowly varying amplitudes, and the wavelet-based method. The first approach dates back to the

 pioneering studies [18] by Goldberg and [20] by Jones and Kobett on quadratically nonlinear elastic waves. It is based on the

hypothesis that nonlinearity is weak. Hence, the first approximation can be chosen as the solution of the linear system

(1.15)–(1.17) (no nonlinear terms on the right-hand side), the second approximation can easily be found from the linear solution,

and the third approximation is negligibly small. In [55], it was noted that many early results on quadratically nonlinear elastic

waves were obtained by experts in nonlinear acoustics and published in monographs on nonlinear acoustics [21, 55, 94]. Three

important results from these studies are: (i) the main nonlinear wave effect is the interaction of waves (linear waves do not

interact), (ii) the formulation and solution of three standard problems, and (iii) investigation of the interaction of three acoustic

waves (triplet problem).

A few lines of development of the classical results from [21, 94] can be seen in [28–86].

Let us formulate the above-mentioned standard problems. The first problem: a longitudinal wave enters a medium, i.e.,

an oscillation with a given frequency in the longitudinal direction is excited at the boundary of the elastic half-space. The second

 problem: a transverse wave enters a medium, i.e., a transverse oscillation is excited. The third problem: both longitudinal and

transverse waves enter a medium.

Let us consider the first problem in more detail.The basic wave equation (for a longitudinal wave u x t ( , )) has the form

( )ρ λ µu u N u utt xx xx x, , , ,− + =2 1 . (2.1)

It is usually solved by the method of successive approximations; the solution is assumed to have the form of the sum

u x t u x t u x t  ( , ) ( , ) ( , )* **= + + ... and the procedure is terminated at the second approximation. The first approximation is

assumed to be the linear solution; it satisfies the homogeneous equation (2.1) (which is linear because its right-hand side is zero)

and has a trivial form for a harmonic wave:

( )u x t u kx t  * ( , ) cos= −0 ω , (2.2)

where k is the wave number, ω is the frequency, u 0 is the amplitude, and ( )v k = = +/ ( ) /ω λ µ ρ2 is the phase velocity.

Let us compare the first problem and the one-degree-of-freedom problem on a resonance in a linear mechanical

oscillating system without friction. The equation of motion has the form [2, 27]

d x t 

dt  x t 

 F 

mpt k m

2

22 0 2

( )( ) cos ( ( / ))+ = =ω ω . (2.3)

While an external force is not switched on, the oscillations are called free or natural,

  x t A t B t  0 ( ) cos sin= +ω ω .

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An external force excites additional forced oscillations

 x t  F k 

 p pt 00 0

21( )

/

( / )cos=

− ω.

It is common practice to impose the conditions x x( ) ·( )0 0= = 0. Then the general solution is

 x t 

 F 

m p

 p

 p

t ( ) ( ) sin cos= −

− +2

2 2

0

2 2ω

ω ω

.

When p → ω, the general solution becomes

 x t  F t 

mt ( ) sin= 0

2 ωω . (2.4)

Thus, when the frequency of the external force coincides with the eigenfrequency of the system, the amplitude increases

 proportionally to the duration of oscillations. This phenomenon is called a resonance [2, 27].

 Remark 2.1. Of course, the amplitude would never increase infinitely in real-world situations. The mechanical model

adopted is valid only for finite and not very high amplitudes.

 Remark 2.2. Resonance is traditionally interpreted by analyzing the forces acting in the system. The elastic forces are

 balanced by inertia forces—after a short initial pulse, the system oscillates at an eigenfrequency in autonomous mode, without

energy supply. The forced oscillations occur at the frequency of the constraining force, which supplies energy to sustain the

oscillations. At resonance, the system does not need the constraining force to sustain free oscillations, and the energy goes to

increase the amplitude of oscillations.

When p → 2ω and the period of the external force is equal to half the natural period of the system, the general solution is

 x t  F t 

mt ( ) sin= 0

42

ωω . (2.5)

The amplitude in (1.44) increases without limit, which is indicative of a resonance in the system. This resonance is

called the first or principal subharmonic resonance [2, 27].

Let us now turn back to the first wave problem.

 Remark 2.3. Both natural oscillations in (2.3) are characterized by an eigenfrequency defined by the mechanical

 properties of the system. Free plane waves in an elastic body (2.2) are characterized by a phase velocity (sound velocity in this

 body) defined by the mechanical properties of the body.

The second approximation is found as the solution of the equation

( )ρ λ µu u N u utt xx xx x,**

,**

,*

,*− + =2 1

or 

( ) ( ) ( ) ( )ρ λ µ ωu u N u k kx t  tt xx,**

,** / sin− + = −2 1 2 21

0 2 3 . (2.6)

 Remark 2.4. The right-hand side of (2.6) takes its form, the second harmonic of a free plane wave, from the hypothesis

that deformation is described by the Murnaghan potential. If nonlinear deformation is not described by the Murnaghan potential,

then the second harmonic does not appear and the corresponding phenomenon fails to be detected.

Thus, (2.6) is an inhomogeneous wave equation whose right-hand side has the form of the second harmonic of wave

(2.2). The situation is similar for the principal subharmonic resonance problem. This means in particular that the amplitude

appearing in the solution of (2.6) increases as the wave propagates.

This solution really has the form of a pure second harmonic with amplitudes continuously increasing with the distance

the wave travels:

( ) ( ) ( )u x t x N 

u k k x t  11

10 2

12

1

1

8 22** * *, cos ( )=

+  

    −

λ µω . (2.7)

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Combining (2.2) and (2.7), we obtain

u x t u x t u x t  1 1 1( , ) ( , ) ( , )* **= + ( ) ( ) ( )= − −+

  

    −u kx t x

 N u k k x t  0 1

10 2

12

1

1

8 22cos cos ( )* *ω

λ µω . (2.8)

This long-standing result displays many features of quadratically nonlinear waves in materials, including two important

effects: self-interaction of waves and generation of the second harmonic.

Both effects are well manifested in the evolution of the initially harmonic profile. This evolution was the subject of computer simulation in [81, 83].

The main goal of the computer simulation was to estimate the ranges of frequencies and amplitudes where the evolution

of the wave profile is most intensive and, hence, can be detected well. The simulation has revealed new elements in the evolution

 pattern. Let the profile evolve in four stages:

Stage 1. The initial cosine profile tilts downward at a constant angle, i.e., the maximum positive values decrease and

maximum negative values increase.

Stage 2. The peaks of the profile get lower, gradually forming a plateau. Then the middle part of the plateau begins to

sag, producing two humps. The frequency of reoccurrence of the same profile is equal to the initial frequency of oscillation.

Stage 3. Preserving the prior period, the profile takes an increasingly pronounced two-humped shape until its trough

touches the abscissa axis.

Stage 4. As the trough goes farther down, the profile becomes nearly harmonic, having the frequency of the secondharmonic and unequal rises and falls (the first rise is high, the first fall is roughly half the first rise, the second rise is slightly

higher than the first one, and the second fall is roughly twice as high as the first fall). Thus, gradually changing, the profile of the

first harmonic turns into that of the second harmonic, i.e., we observe a transition of one harmonic into another.

 Remark 2.5. The computer analysis involves six physical constants (density, two Lamé constants, and three Murnaghan

constants) for eighteen granular composite materials. These materials are denoted by KM , where K  = 1 corresponds to steel

granules and polystyrene matrix; K  = 2, to copper granules and polystyrene matrix; K  = 3, to copper granules and tungsten

matrix; K  = 4, to copper granules and molybdenum matrix; K  = 5, to tungsten granules and aluminum matrix; and K  = 6, to

tungsten granules and molybdenum matrix. There are three modifications for each of the K  materials. These modifications,

labeled by M , differ by the volume fractions of granules, c1, and matrix, c2: M = 1 corresponds to c1 = 0.2 and c2 = 0.8; M = 2, to

c1 = 0.4 and c2 = 0.6; and M = 3, to c1 = 0.6 and c2 = 0.4. The physical constants are given in [55, Table 5.2].

The results of the computer simulations (numerous plots) were used to analyze three most typical materials: 11, 41, and62. The frequency was varied within the ultrasonic range from relatively small values (at which visible distortions of the profile

appeared only after a large number of oscillations) to relatively large values (at which the profile evolution started to be observed

after the second or third oscillation). The amplitude was varied from 0.05 mm (small displacements) to 0.5 mm (not very large

displacements). In all the experiments, the maximum amplitude of the distorted wave was exactly half as much again the initial

amplitude. This phenomenon stems from the convention adopted in nonlinear wave theory [27, 91] that the initial hypotheses of 

the method of successive approximations are invalid for large amplitudes.

All the plots were grouped so as to represent different stages of the profile evolution. On all the plots, the abscissa is the

distance x in meters and the ordinate is the displacement amplitude u1 in millimeters. Time is fixed. In what follows, we will

discuss only the plots for the material 11.

The first group of plots is where the initial amplitude is the same, u10 = 0.1 mm, and the frequencies vary. Figure 1

demonstrates the first stage of profile evolution (the profile tilts downward). This effect is more or less clear for differentmaterials and can be observed well for the material 11, whose wave phase velocity is relatively low, v11 =1.848⋅103 m/sec. This

 plot corresponds to the smallest studied frequency of 10 kHz.

Figure 2 demonstrates the first three stages (developed evolution). This plot corresponds to a frequency of 50 kHz.

Given a small initial amplitude, we conclude that all the three stages can be seen at a distance of 2 m.

Figure 3 represents a frequency of 100 kHz, which is extremely high for the material 11 (here a significant distortion is

observed to the right of the beginning of wave propagation).

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The second group includes plots for a fixed frequency of 40 kHz and varying initial amplitude. Figure 4 shows that

when the initial amplitude is small, u10 =0.05 mm, the wave profile evolves slowly—at a distances of 1.5 m, the evolution is still

at the first stage.

Figure 5 shows that for a larger amplitude (u10 = 0.1 mm) the evolution is still slow.

In Fig. 6, the amplitude is three times larger than the initial amplitude (u10 = 0.15 mm). Here the evolution reaches the

second stage at best.

Finally, for an amplitude of 0.5 mm (u10 =0.5 mm), we observe two different situations for materials with a small wave

velocity and nonsmall wave velocity. For the former materials, including the material 11, a ten-fold increase in the initial

amplitude leads to a critical stage in the evolution process—significant distortions start to appear immediately. This case is

shown in Fig. 7.

All the four stages of profile evolution may be demonstrated under large finite deformations. Thus, the effect of the

initial amplitude on the evolution is much weaker than that of the frequency of the initial harmonic wave.

Finally, Fig. 8 shows how the initially given first harmonicω transforms into the second harmonic 2ω. In the figure, two

different (initial and advanced) parts of the same plot for the material 11 with ω = 100 kHz and u10 = 0.1 mm are superimposed

(see two rows of distance values along the horizontal axis).

We have discussed some features of the first problem of nonlinear acoustics. Let us turn back to the second and third

 problems.

1372

Fig. 1

0.1

0 2 4 6 8 10

Fig. 2

0 0.5 1 1.5 2

0.1

Fig. 3

0.1

0 0.2 0.4 0.6 0.8 1

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The second problem is described by the equations

( )ρ λ µu u N u utt xx xx x1 1 2 3 32,**

,**

,*

,*− + = , (2.9)

ρ µu utt xx3 3 0,**

,**− = (2.10)

and the boundary conditions

u t u t u t u t  3 3 0 1 20 0 0( , ) cos , ( , ) ( , )= = =ω 0. (2.11)

As is seen from system (2.9), (2.10), the second equation is autonomous, whereas the first equation includes both the

longitudinal displacement u1 and the transverse displacement u3, this latter appearing nonlinearly. This dissymmetry reflects the

fact that longitudinal and transverse waves propagate differently.

Equation (2.10) is linear and homogeneous and the corresponding wave will be linear:

( )u x t u k x t  3 3 0 3( , ) cos= −ω . (2.12)

Thus, new waves are not generated during the propagation of transverse waves, the second approximation coincides

with the first one, and a transverse wave reproduces itself in its classical representation.

The first equation (2.9) can be rewritten as

1373

Fig. 4

0.04

0 0.2 0.4 0.6 0.8 1 1.2 1.4

Fig. 5

0 17 18 19 20 21 22 23

0.1

Fig. 6

0 0.2 0.4 0.6 0.8 1

0.15

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( ) ( )ρ λ µ ωu u N u k k x t  tt xx1 1 2 3 02

33

32 1 2 2,**

,**

/ ( ) sin ( )− + = − . (2.13)

However, it is well to bear in mind that the first approximation for longitudinal waves is zero because no longitudinal

wave is initially excited. That is why the equation of the second approximation has the form (2.9) or (2.13).

Then the solution of Eq. (2.13) is

( )[ ]

( )[ ]u x t   N u k  

v vk k x k  1

2 3 02

3

12

32

3 1 14

** ,( )

( ) ( )sin cos=

−− +

ρ ph ph

( )[ ]k x t 3 2− ω . (2.14)

Thus, a transverse wave generates a composite longitudinal wave, modulated in space and propagating with double

frequency.

Let us consider the third approximation. The basic system has the form

( ) ( ) ( )ρ λ µu u N u u u u N utt xx   xx x1 1 1 1 1 1 1 22,** *

,*** * **

,* **

,− + = + + + ( ) ( )3 3 3 3

* **,

* **,

+ +u u u  xx x

, (2.15)

( ) ( )ρ µu u N u u u u u utt xx   xx x3 3 2 1 1 3 3 3 3,** *

,*** * **

,* **

,*− = + + + +( ) ( )**

,* **

,  xx xu u1 1+

. (2.16)

The solutions of Eqs. (2.15) and (2.16) can be represented as the superposition of many waves:

1374

Fig. 7

0.5

0 0.2 0.4 0.6 0.8 1

Fig. 8

0 0.025 0.050 0.075 0.100 0.125 0.150

3.058 3.083 3.108 3.133 3.158 3.183

0.4

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u x t  N u

v vw x t 1

2 3 02

1 32 15

2** * ( , )

( )

( )( , )=

ω

ρ ph ph [ ]+−

  N N u

v v v vw

1 22

3 04 2

31

23

21

23

416

( ) ( )

( ) ( ) ( ) ( )

ω

ρ ph ph ph ph

11

4

nn

 x t ( , )=∑ , (2.17)

[ ]u x t  N u

v v vw1

22

3 03 2

21

23

23

48

** * ( , )( ) ( )

( ) ( ) ( )=

ω

ρ ph ph ph

31

4

nn

 x t ( , )=∑ , (2.18)

where w m1 and w m3 are newly generated waves.  Remark 2.6. These waves can be or cannot be synchronized with the basic wave. Two waves are synchronized (in

 phase) if they have the same characteristics in the phase plane. The phenomenon of generation of new waves can be considered to

consist of the phenomenon of generation of a new harmonic and the phenomenon of generation of new composite waves. The

new harmonic is understood as follows: an initially sinusoidal wave,

u x t u k x t  1 1 0 1( , ) cos ( )= −ω , (2.19)

 propagating through a nonlinear medium generates new longitudinal waves with phases multiple of that from (2.19):

u m k x t m N  m1 0 1cos ( ) ( )− ∈ω . (2.20)

These waves are phase synchronized with the basic wave (2.19). When wave (2.19) generates its transverse harmonics,they combine with the basic transverse wave producing waves modulated in space, which are synchronized neither with the

initial longitudinal wave nor with the initial transverse wave. They are said to be composite waves.

The third problem assumes that both longitudinal and transverse waves are initially excited. The following two

equations have to be solved:

( )ρ λ µu u N u u N u utt xx xx x xx x1 1 1 1 1 2 3 32,**

,**

,*

,*

,*

,*− + = + , (2.21)

( )ρ µu u N u u u utt xx xx x xx x3 3 2 3 1 1 3,**

,**

,*

,*

,*

,*− = + . (2.22)

The solution for the longitudinal wave consists of two parts: (2.8) and (2.17). The transverse wave is the sum of a

classical linear transverse wave (2.12) and a composite wave with a small period of modulation

( )u x t   N u u

vk k x3

2 1 0 3 0

33 3 1

1

2** ( , )

( )sin= −

ω

ρ ph

×+

− ++

( ) ( )

( ) ( ) ( )cos

v v

v v vk 

12

32

14

12

32 3

3 2

1

23

  ph ph

  ph ph ph

( ) ( )k x t v

v vk k x1

32

12

32 3 12

1

2−

−−

ω( )

( ) ( )cos

 ph

  ph ph

. (2.23)

Thus, the above three problems of nonlinear acoustics (solved by the method of successive approximations) allow us to

describe a series of nonlinear wave phenomena, which can be united as those associated with the basic nonlinear phenomenon of 

wave interaction.

Let us look at what is going on when the medium through which waves propagate is orthotropic [36, 55]. If the elastic potential has the form

( )W c c A Biimm mm ikik ik   ik  i im ik mk i ik = + − + +1

21

1

32 2 2ε δ ε ε ε ε ε ε mm i mmC +

1

33ε , (2.24)

then plane waves propagating along the axes of symmetry are described by equations similar to (3.16)–(3.18) from [14]. For 

example, the basic system of equations for quadratically nonlinear plane polarized waves propagating along the Ox1-axis is

ρ u c u N u u N u u N  tt 1 1111 1 11 11

1 1 1 1 1 21

2 11 2 1 3, ,( )

, ,( )

, ,− = + + ( ), ,

13 11 3 1u u , (2.25)

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( )ρu c u N u u u utt 2 2323 2 11 21

2 11 1 1 1 11 2 1, ,( )

, , , ,− = + , (2.26)

( )ρu c u N u u u utt 3 1313 3 11 31

3 11 1 1 1 11 3 1, ,( )

, , , ,− = + , (2.27)

( )  N c A B C N c A B N  11

1111 1 1 1 21

1122 1 1 31

3 2 31

2

( ) ( ) ( ), ,= + + + = + + = c A B1133 1 1

1

2+ + .

Let us turn back to the main nonlinear wave effect—interaction of waves. This effect can be divided into two ones:interaction of waves with equal frequencies and interaction of waves with different frequencies.

All the previous problems studied the interaction of waves with equal frequencies. It was also additionally assumed that

waves propagate in the same direction. Lifting these two restrictions complicates the problem. An example is the

synchronization of waves in a quadratically nonlinear medium. No more than three waves can be synchronized in this medium;

three synchronized waves are called a wave triplet. What is most important is that two noncollinear waves with all parameters

(amplitude, frequency, and polarization) different are initially excited [20, 21, 55, 94]:

( ) ( ) ( )r r r r r r ru x x x t A t k r A t k r  1 2 3 1 0 1 1 2 0 2 2, , , cos cos= − + −ω ω , (2.28)

where the wave vectorsrk α may form an arbitrary angle; the amplitude vectors

r Aα0 may be polarized differently—they may be

 both parallel and perpendicular to the propagation direction; andrr OX = → , X x x x= ( , , )1 2 3 , is the radius-vector of the point X .

The second approximation follows from the solution of some inhomogeneous vector Lamé equation. According to this

solution, there is some special, resonance-like case where the energies of the given two waves are fully pumped into a new, third

wave. This wave has the frequency

ω ω ω3 1 2= ± (2.29)

and the wave number 

r r rk k k 3 1 2= ± . (2.30)

Physics calls (2.29) and (2.30) resonance conditions; and three waves related by these conditions are called a wave

triplet or just a triplet.

There are six different combinations of wave constituents in triplets

  L L L L L T  ( ) ( ) ( ), ( ) ( ) ( ) ,ω ω ω ω ω ω1 2 3 1 2 3+ = + =

  L T L L T T  ( ) ( ) ( ), ( ) ( ) ( ) ,ω ω ω ω ω ω1 2 3 1 2 3+ = + =

T T T T T L( ) ( ) ( ), ( ) ( ) ( ) ,ω ω ω ω ω ω1 2 3 1 2 3+ = + = (2.31)

where L corresponds to the longitudinal wave and T , to the transverse wave.

The third wave (similarly to the first and second ones) can have two different polarizations.

Also we can obtain special restrictions on the angle between the two primary waves—the triplet does not exist for all

values of the angle. The frequency ranges of two primary waves cannot be arbitrary. Some problems arise in calculating theamplitude of the third wave. That is why the method of slowly varying amplitudes is additionally used.

 Next few pages will be devoted to problems for quadratically nonlinear waves solved by the method of slowly varying

amplitudes.

Let us again turn to the article [14] where the methods of successive approximations and slowly varying amplitudes

were described and compared, with the remark that they supplement each other.

We start with the evolution equations [14] (they are written for longitudinal waves, denoted by the subscript “1”)

( ),( )  A A A ei k k k x

11 1 1 12 1313 12 11= − −σ , ( ),

( )  A A A ei k k k x12 1 2 11 13

13 12 11= − −σ ,

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( ),( )  A A A ei k k k x

13 1 3 11 1213 12 11= − −σ ,

σλ µ

σλ µα

δ δ

α= −

+

+=−

+

 N k k k k  

 N k k  1 1 13 1 13

13

1 11 12

2 2 2 2

( )

( ),

( )( ).α δ+ = 3 (2.32)

As a rule, the quantity

∆k k k k  = − −13 11 12 (2.33)

is considered a measure of phase matching. The condition ∆k =0 is called the phase index matching condition. When ∆k =0, the

 behavior of waves can be explained by an example. Let the third wave be not initially excited, A13 0( ) =0. By the hypothesis that

amplitudes vary slowly, the amplitudes A11 and A12 may be assumed constant over a not very long distance. Then only the third

equation in (2.32) can easily be solved:

[ ]{ }  A x N k k A A x13 1 1 2 11 122 2( ) / ( )= +λ µ . (2.34)

Thus, under full (frequency and space) synchronism, the amplitude of the third wave is directly proportional to the

distance traveled. This situation is similar to a resonance. From the assumed balance of energy of the triplet, it follows that the

energies of the two primary waves are pumped into the third wave. This example shows that both the method of successive

approximations and the method of slowly varying amplitudes include the full synchronism conditions as a necessary conditionfor the existence of a triplet.

Energy analysis is very useful in the theory of triplets. For elastic triplets, the Manley–Rowe relations introduced in

nonlinear optics [27, 55, 91] can be written as

σ σ σ σ σ2 11 1 12 1 3 12 2 13 2 3~

( )~

( ) ,~

( )~

( ) ,~

  N x N x C N x N x C N  − = + = 11 1 13 3( )~

( )  x N x C  + =σ , (2.35)

where~

( ) | |  N x A A Am m m m1 1 1 12= = are the intensities of waves. Formulas (2.35) turned out to be a unique tool for solving

 problems of parametric amplification of waves and related problems.

 Remark 2.7. Relations (2.35) help to look at triplets from an unexpected point of view. It is easy to obtain from (2.35) the

energy balance law in the form ω σm m mm

 A12

1

3

=

∑ =const. This formula may be regarded as an equation for a general ellipsoid with

semiaxes ω ω2 3 , ω ω1 3 , and 1 1 2/ ω ω in the three-dimensional space of variables A11, A12, and A13. The surfaces of 

constant energy will be general ellipsoids; and the phase trajectories are the intersections of the ellipsoid with the cylindrical

surfaces defined by the Manley–Rowe relations

σ σ3 112

1 132 A A+ = const, σ σ3 12

22 13

2 A A+ = const, σ σ2 112

1 122 A A− = const .

In the neighborhood of the A11- and A12-axes, the trajectories have the form of ellipses, i.e., under small variations the

amplitudes of the two primary waves oscillate weakly, and the process is stable.

However, trajectories that reach the third axis have a different property—two waves receive energy from the third wave.

In other words, the third wave breaks down.

Thus, the three waves interact by two scenarios: (i) two initially given waves put out their energy to the third wave andthen practically cease to exist and (ii) one initially given wave breaks down into two new waves and then practically cease to

exist.

The last issue to consider in this subsection is the problem of interaction of two waves in a special formulation. Consider 

two coupled waves entering a medium or light guide. Initially one wave is more powerful (a pumping wave with a high

amplitude) and the other wave is weak (a control signal with a very small amplitude). The parameters of the two waves are fixed

at some finite distance from the entry (at the exit). Under certain conditions, a very small change in the control signal causes an

abrupt change in the intensities of the waves on leaving the medium; in particular, the strong wave can switch from its frequency

to the frequency of the control signal and back (that is why this problem is called the self-switching problem).

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Consider a longitudinal wave. The method of slowly varying amplitudes first represents both the control signal and

 pumping wave in the form of harmonic waves with spatially varying amplitudes A x pum ( )and A xsign ( ), fixed frequencies ω pum

and ω sign , and fixed wave numbers k  pum and k sign :

u x t A x e u x t Ai k x t  

  pum pum sign sign  pum pum( , ) ( ) , ( , ) (

( )= =−ω x e

i k x t  )

( )sign sign− ω. (2.36)

It is convenient to replace this complex representation of waves with a real one:

{ }u x t A x e a x k xi k x t  

  pum pum pum pum  pum pum( , ) Re ( ) ( )cos

( )= =−ω [ ]− +ω ϕ  pum pumt x( ) ,

{ }u x t A x e a xi k x t  

sign sign signsign sign( , ) Re ( ) ( )cos

( )= =− ω [ ]k x t xsign sign sign− +ω ϕ ( ) .

 Next we will formulate the first group of assumptions: the frequency of the weak wave is half that of the strong wave,

2ω ωsign pum= . Our interest here is with the effect of self-generation of the weak wave on the strong wave, since it is just a wave

with the frequency of the strong wave. We will not consider the self-generation of the strong wave, since it is a different wave

effect that is not related to the self-switching effect. The ordinary nonlinear interaction of two waves should be taken into account

too. Now, we can obtain a shortened equation and then write the evolution equations.

Let us formulate the second group of assumptions: the direct effect of the weak wave on the strong wave can be

neglected because of the predicted ineffectiveness of this influence; the direct effect of the strong wave on the weak wave seemsto be significant.

The evolution equations include either two decoupled equations, of which the first one describes the evolution of the

signal wave and the second equation, the evolution of the strong wave,

dA

dxS A e

dA

dxS A Ai kx

 pum

  pum sign

sign

sign pum sign= =−( ) ,2 ∆ e i kx∆ ,

S  N  k 

k S 

 N k k k  pum

sign

 pumsign pum pum sig=

+=

++1

21

2 2λ µ λ µ

( ), ( n sign pum), ∆k k k = −2 , (2.37)

or three equations, of which two equations are for the real amplitudes ρ pum

( ) x and ρsign

( ) x and the remaining equations are for 

the phase difference ϕ ϕ ϕ( ) x k = − +2 sign pum ∆ ,

( )( ( )) ( ) cos ( )ρ ρ ϕ  pum pum sign  x S x x′ =2

, (2.38)

( ( )) ( ) ( )cos ( )ρ ρ ρ ϕsign sign sign pum  x S x x x′ =− , (2.39)

( ( )) ( )( ( ))

( )ϕ ρ

ρ

ρ  x k S x S  

 x

 x′ = − −

 

 ∆ 2

2

sign pum pum

sign

 pum

 

   sin ( )ϕ x . (2.40)

Let us now introduce characteristic intensities of wave quantities:

  I x A x x  pum pum pum( ) | ( )| ( ( ))= =2 2ρ , I x A x xsign sign sign( ) | ( )| ( ( )) .= =2 2ρ (2.41)

There are two well-studied cases: the mismatch ∆k of wave numbers is small and is zero. For the second case and new

variable ξ = S F xsign , the solution is

 ) I sign ( ) tanh ( ),ξ ξ ξ= + 0

 ) ) I I   pum sign( ) cosh ( ) ( tanh ( ) )ξ ξ ξ ξ= + =− −1

0 01 0 . (2.42)

 Remark 2.8. If the initial intensity of the signal wave is equal to zero (the initial amplitude of the signal wave is equal to

zero), then the arbitrary constant ξ 0 is equal to zero too. The initial intensity of the pumping wave decreases with time and the

intensity of the signal wave increases until all of the energy of the strong wave has gone to the signal wave.

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Thus, we have found the analytical solution to the problem on the interaction of two waves. It remains to discuss the

wave self-switching phenomena—our interest is with the intensities and phase difference at the exit of the medium—at a

distance l from the entry.

The most useful information can be derived from the cubic equation ) )  I I Gsign sign( )1 2 2− − = 0, following from (2.42),

and its roots

( ) ) ) I I sign sign( ) ( ) sin ( ),1

20 0≈ ϕ)

m )

 I I sign sign( , ) ( ) sin ( ) .2 3 1 0 0≈ ϕ (2.43)

Here two cases are very interesting:

A. The initial intensity of the signal wave is zero, ) I sign ( )0 = 0. Then

 ) ) I I l sign pum( ) ( )ξ = =1 0 . Thus, all of the energy of 

the pumping wave goes to the signal wave. Here we observe that the first harmonic enters the medium and turns into the second

harmonic on leaving the medium. The wave switches from the first to the second harmonic.

B. The initial intensity of the signal wave is very small, yet not zero. Let us calculate the normalized intensity of the

signal wave that leaves the medium, supposing that the strong wave hardly supplies energy to the signal wave:

 ) I 

U l sign ( )ξ ≈−+

    

   <<

1

12 1,

U I e l ≈ ≈4 0 0 12 2 )sign ( )sin ( )ϕ ξ ( )→ ≈ << ≈− )

 )

 I  I 

el l 

sign

sign( )

( )

sin ( )sin ( )ξ

ϕϕξ64 0

01 0 1

22 . (2.44)

Here the situation is different. If the signal wave is of very low intensity, then the strong wave travels through the medium almost

changeless. At the exit of the medium, we observe a strong pumping wave with frequency ω and a weak signal wave. If the

intensity of the signal wave is zero, then the signal wave will have the frequency 2ω at the exit. This phenomenon is called

self-switching of waves.

Similar results were obtained in [64] for a more complicated medium, a two-phase elastic mixture.

2.2. Harmonic (Periodic) Waves in the Microstructural Theory of the Second Order. We start with the basic system of 

wave equations (1.31)–(1.33). First, let us compare systems (1.15)–(1.17) and (1.31)–(1.33) and formulate the main distinction.

Formally speaking, each of the three equations (1.15)–(1.17) corresponds to the coupled system of two equations (1.31)–(1.33).

From the wave point of view, this fact implies wave doubling. The wave pattern in a mixture is richer; therefore, introducingnonlinearity complicates the mechanism of wave interaction.

Most of the results obtained in the microstructural theory of the first order can be extended to the microstructural theory

of the second order.

Let us analyze these results according to the scheme proposed in Section 2.1.

First, consider problems solved by the method of successive approximations, beginning with the three standard

 problems of nonlinear acoustics. The formulations of all the problems are classical, except that the medium of propagation is a

mixture and that this medium is dispersive.

The first problem assumes solving the coupled system [14, 55]

( ) ( )ρ λ µ λ µ βααα

α αα δ α

u u u u utt xx xx1 1 3 3 1 12 2,( )

,( )

,( ) ( )− + − + − −( )1 1 1 1

( ) ( ),

( ),

( )δ α α α= N u u  xx x (2.45)

with the boundary conditions u t u t  o1 10( ) ( )

( , ) cosα α ω= .

In the second approximation, the solution is

u x t C e l k C  i k x t  1 1 1 1 1

1 1( )** ( ) ( ) ( )* ( )

( , ) ( )( )*α α ω δ δα

= +− − e i k x t  − −( )( )*

1 1δ

ω

+ +  

    − x

 M S l k ik c C u e i1

11 1 2 1 0 1

2ωαδ

δ δδ

δ δ( )

( )* ( )* ( ) ( ) ( ) ( ) ( )( )* ( )*

k x t i k x t   x

 M S C e1 1 1

1

11

2δ αω

ααα ωω− − −+

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+ + +  x

 M S C u

 x

 M S l k ik c

1

11 0 1

1

11 1

ω ωδα

α δαδ

δ δαδ

( ) ( ) ( )* ( )*( ) [ ]

 

   

− + −

C u ei k k x t  

1 0 121 1 1( ) ( ) ( )

( )* ( )*δ α ωα δ

. (2.46)

The first and second terms in (2.46) constitute the solution in the linear approximation, i.e., they are two harmonic

waves (two modes) with different wave numbers and other properties known from the linear theory of mixtures. The third and

fourth terms describe the second harmonics of the first and second modes, respectively. These harmonics are generated by the

modes independently. Attention should be focused on the dependence of the amplitudes of the second harmonics on the

amplitudes of the initial impulses and frequencies, which is more complicated than in a liquid or an elastic body, and also on the

fact that they are no longer real, but complex numbers. Finally, the fifth terms describe a new complex longitudinal wave, which

is due to the nonlinear interaction of two different modes. The wave numbers k 11( )*

and k 12( )*

are always different, the difference

increasing as the cut-off frequency is approached from the right. The new wave describes spatial beating with the beating

frequency depending only on the parameters of the linear problem. The spatial modulation period also depends on the parameters

of the linear problem.

  Remark 2.9. This last wave should be discussed individually. It describes a new microstructural

  phenomenon—interaction of two different modes of the same longitudinal wave. Such an interaction is characteristic of 

two-phase mixtures. It would also be manifested with transverse waves and has to be taken into account in studying the full wave

 pattern. The fact should be considered that the second mode is stopped at low frequencies. Therefore, the new wave arises at high

frequencies (they are supersonic frequencies for many real composites).The second standard problem for mixtures is more interesting than the corresponding classical problem. This problem

implies solving the following systems in the second approximation:

ρ λ µ λ µααα

α αα δ

u u utt xx xx1 1 3 3 12 2,* * ( )

,* * ( )

,** (

( ) ( )− + − + ( )) **( ) **( ) ( ),

*( ),

*( )− − =β α δ α α αu u N u u  xx x1 1 2 3 3 , (2.47)

ρ µ µ βααα

αα δ α

u u u u utt xx xx3 3 3 3 3,* * ( )

,* * ( )

,**( ) **( )− − − −( )3 0

**( )δ = . (2.48)

The solution of (2.48) for the boundary conditions u t u t  3 30( ) ( )

( , ) cosα α

ω= init and u t u t  2 10 0 0( ) ( )

( , ) ( , )α α

= = and zero initial

conditions is well known [55]:

[ ] ( )u u e l k u ei k x t i k x

3 30

3 3 30

3 1 3**( ) ( ) ( ) ( )

( ) ( )α α ω δ δα δ

= +− + − [ ]130 3 3 3 3

3 31

+ =−

ω α α δ δ

δt 

uu l k u

l k ,

( )

(

( )( ) ( ) ( )

( )

init init

) ( )( )

l k 3 3δ . (2.49)

 Remark 2.10. The second harmonic is not generated here—the wave does not interact with itself. Also, amplitudes are

not equal to the initial amplitude. This property is characteristic of mixtures.

Let us dwell on system (2.47). First, it is necessary to calculate the nonlinear right-hand side from the known linear 

solution (2.49). System (2.47) may be solved by selecting similar functions and is represented as a superposition of five waves:

[ ] ( )u x t u e l k u ei k x t i k  

1 1 10

1 10

1 1 1( ) ( ) ( ) ( )

( , )( ) (α α ω δ δα

= +− + − [ ] [ ]δ αωα

ω) ( )  x t i k x t  

iS e1 3 11

2+ − ++

[ ] [ ]+ +− + − + +iS e iS ei k x t i k k x t  2

23

3 1 31

32

1α ω α ω

δ( ) ( ) ( )

( ) . (2.50)

The first two waves in (2.50) are two modes of linear longitudinal waves. The third and fourth waves are in fact the

second harmonics for the previous two waves. The fifth wave is of greatest interest.

 Remark 2.11. The fifth wave represents a new effect not described in classical nonlinear theory—interaction of two

different modes of the same wave. This effect is due to the microstructural nature of mixture theory.

 Remark 2.12. In composites, the new synchronism 2 1 31

32

k k k ( ) ( ) ( )α ≈ + should result in small amplitudes, i.e., the wave

numbers in the frequency range where the two modes exist are of orders from 1 to 10 –2 m –1. As a rule, there is no synchronism

and no nonlinear effects are superimposed.

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Let us examine solution (2.50) in the frequency range where the second mode does not exist. The solution is one

composite (superimposed) wave:

( )u x t u x t S k k xk 

1 1 1 1 1 11

32

1

1

22

( ) ( ) ( ) ( )( , ) ( , ) sin sin

α αα= = − 1

13

2

1

2

22

( ) ( )+−

k  x t ω . (2.51)

Thus, a superimposed longitudinal wave, which is spatially modulated with the period of amplitude modulation,

∆  x k k v v1 11

32 1 1 3 1

2 2 2 2= − = −π π ω/ [ ] / [ ]( ) ( ) ( ) ( )

  ph ph , arises in both phases.

 Remark 2.13. The equality k k 11

32

2( ) ( )= is quite likely to apply to composites. On the whole, the period of modulation

may exceed the length of the carrier wave by an order of magnitude or more.

 Remark 2.14. In composites with small k k 11

32

2( ) ( )= , the superimposed wave (3.7) acquires an amplitude proportional to

 x1. In contrast to classical nonlinear media, a microstructural nonlinear medium may accumulate nonlinear distortions even in

the absence of ordinary synchronism.

The third standard problem is distinguished by the asymmetric relations between the basic equations. On the whole, the

interaction between longitudinal and transverse waves is asymmetric. Wave motion is described by the coupled system [55]

 L u L u L u L u

n n

1 1 13 1 1 1 3 3α

α δ

α

α

α

α( ) ( ) ( ) ( ) ( ) ( )

+ = + , (2.52)

( )  L u L u L u uk k n

2 23 4 1 3αα δ

αα α( ) ( ) ( ) ( ) ( )+ = . (2.53)

 Remark 2.15. In a two-phase mixture, longitudinal and transverse waves have two modes each, i.e., two compression

waves and two shear waves propagate simultaneously, and their phase velocities are all different. In the general case, all these

waves interact. The interaction of modes is of major interest because it does not occur in classical media.

Assume that longitudinal and transverse vertical waves are simultaneously excited in a material, which means imposing

zero initial conditions and boundary conditions in the form u x t u t  m m( ) ( )

( , ) cosα α ω1

0= . There are no displacements u2( )α

,

um0( )α = const, m= 1, 3. Then the solution of system (2.52), (2.53) can be written in the form

[ ] ( )u x t C e l k C ei k x t i

1 1 1 1 1 11 1**( ) ( ) *( ) ( )

( , )*( )α α ω δ δα

= +− + − [ ]k x t 1 1*( )δ ω+

+ +  

    − x

 M S l k ik c C u e

i1

1

1 12 1 0 1

2ωαδ δ δ δ

δ δ( )

*( ) *( ) ( ) ( ) ( ) ( )k x t i k x t   x

 M S C eα

δαω

ααα ωω*( ) *( )

( )− − −+ 1

11

21

+

+ + x

 M S C u

 x

 M S l k ik c

1

11 0 1

1

1

1 1ω ωδα

α δαδ δ δ

( ) ( ) *( ) *( )( )

[ ]αδ

δ α ωα δ  

   

− + −

C u ei k k x t  

1 0 12

1 1( ) ( ) ( )

*( ) *( )

+ +−

++

+

Q e Q e

ik k 

  x t ik k 

1

2

22

2

211

31

11

23

2

α

ω

α

( ) ( ) ( ) ( ) ( ) ( ) ( )

22

3

221

11

31

32

1  x t ik k k 

 x t 

Q e

+

+ ++

α

ω

,

( )Q S k k xγα γαγ γ = −sin

( ) ( )1

221 3 1, ( )Q S k k k x3 3 1 3

13

21

1

2α αα= − −sin

( ) ( ) ( ). (2.54)

The first five waves in (2.54) represent the solution of the first problem (2.46) discussed above. Of interest are the sixth,

seventh, and eighth waves whose modes interact. These waves represent a new element in the solution that combines nonlinear 

and microstructural effects.

The terms with the amplitudes Qiα are longitudinal waves with complex wave numbers and double frequencies, i.e.,

they are second harmonics. These waves are spatially modulated. Here, synchronization is possible within a narrow frequency

range such that the conditions k k 1 32( ) ( )γ γ ≈ and k k k 1 3

13

2( ) ( ) ( )α ≈ + are satisfied.

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The solution for transverse waves of system (2.52), (2.53) has the form

[ ] ( )u x t A e l k A ei k x t i

3 1 3 3 3 33 1**( ) ( ) *( ) ( )

( , )*( )α α ω δ δα

= +− + − [ ]k x t 3 1*( )δ

ω+

+  

    − x

 M S l k k c A u e

i1

11 3 3 3 1 3 0 3

ωα

α αα

α α~( ) ~*( ) *( ) ( ) ( ) [ ]( )

*( ) *( )k k x t  1 3 2

α α ω+ − [ ]+ − + − x

 M S A u e

i k k x t  1

11 3 0 3

21 3ω

αα α ωα α~ ( ) ( ) ( )

*( ) *( )

+ +    

  

 x

 M S l k ik c A u e

1

12 3 3 3 2 3 0 3

ωδ

δ δδ

δ δ~( ) ~*( ) *( ) ( ) ( ) [ ]− + −i k k x t  ( )

*( ) *( )1 3 2δ δ ω [ ]+ − + − x

 M S A u e

i k k x t  1

12 3 0 3

21 3ωδ

δ δ ωδ δ~ ( ) ( ) ( )*( ) *( )

. (2.55)

It consists of six waves. The first two waves are a normal linear two-modal representation of a transverse wave in a

two-phase mixture. The other waves are second harmonics with wave numbers that are linear combinations of wave numbers of 

various modes.

  Remark 2.16. What composite waves have in common is that their amplitudes depend proportionally on the wave

numbers. Note that the amplitudes of the self-generated second harmonics contain squared wave numbers in the numerators.

Transition to high frequencies increases the effect of self-generation.

Let us now consider features of the interaction of waves with different frequencies. The main problem here is the triplet

 problem. It should be pointed out that 21 types of triplets may hypothetically exist in a two-phase mixture:

T T L L L T  ( ) ( ) ( ) ( ) ( ) ( )( ) ( ) ( ), ( ) ( ) (11

22

13

11

22

1ω ω ω ω ω+ = + = ω 3 ) ,

  L T L( ) ( ) ( )( ) ( ) ( ) ,21

12

13ω ω ω+ = and so on. (2.56)

The superscript indicates the mode number.

Using the classical procedure is not trivial for a mixture, since, in contrast to the classical nonlinear procedure where

wave vectors are constant, these vectors are functions of frequency. The distribution coefficients of the amplitude matrix depend

on the frequency too. A major difficulty also arises in calculating the inverse Fourier transform.

The resonance conditions have the form [55]

ω ω ω1 2 3 0± + = , (2.57)

k r k k  l t ( )[( )]( )

( )

( )

( )

(( ) ( )

ακ 

δδκ 

δω ω ω− ± − −1 2

01 1 21

1

2

r r r δω2

2 0)

( ) = . (2.58)

Thus [55], various triplets are possible in solid mixtures (composite materials).

Let us now analyze some results obtained by the method of slowly varying amplitudes.

The basic assumption of the method deals with nonlinearity: it is weak during wave motion and the wave amplitude

varies slightly for a time equal to one period (or over a distance equal to the wavelength). Also, we will extend the spectrum of 

nonlinear properties. For this purpose, we will use the first variant of the Murnaghan potential, i.e., we additionally take into

account the nonlinear interaction between phases by incorporating three new constants A3, B3, and C 3 into the Murnaghan

 potential.

Let us consider a longitudinal wave in a two-phase mixture to demonstrate features of the wave pattern.

First, the mode exists in both phases of the mixture simultaneously. If the first longitudinal mode is selected as a participant of interaction, then a harmonic wave propagate in the first phase of the mixture and a similar wave, in the second

 phase. In the case of the second mode, a different pair of waves with different amplitudes propagates through the mixture. Thus,

an individual mode participates in interaction. Let us narrow the analysis to longitudinal waves alone. They do not generate

transverse waves during the interaction, which simplifies the description.

If the first mode is chosen as a participant of interaction, then a wave with an arbitrary amplitude and a

frequency-dependent wave number (the mixture is a dispersive medium) [ ]u x t A e

i k x t  1

11

11

1( ) ( ) ( )

( , )( )

= −ω ω propagates in the first

 phase. The second phase conveys the same wave but with a different amplitude, [ ]u x t l A e

i k x t  1

21

21

11

1( ) ( ) ( ) ( )

( , ) ( )( )

= −ω ω ω. This

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amplitude depends on the frequency. When the second mode is chosen as a participant of interaction, then the situation will be

similar.

Consider the basic system for longitudinal waves [55]

ρ λ µ λ µ βααα

α αα δ

u u u utt xx xx1 1 3 3 1 12 2,( )

,( )

,( ) (

( ) ( )− + − + − ( )α δ) ( )− u1 = +  N u u N u u  xx x xx x1 1 1 13

1 1( )

,( )

,( ) ( )

,( )

,( )

.α α α δ δ

(2.59)

We will restrict ourselves to the interaction of three waves. First, let us assume that the synchronism conditions are

satisfied in terms of frequencies. Next we select one of the six possible triplets: “1st harmonic 1st mode + 1st harmonic 1st mode =2nd harmonic 2nd mode.” Under frequency synchronism, the shortened equations (one equation for each phase) break down into

three evolution equations (three for each phase). The spatialsynchronism condition has the form k k k 111

1 122

2 131

3( ) ( ) ( )

( ) ( ) ( )ω ω ω+ = .

  Remark 2.17. Because of the dispersivity of solid mixtures, the wave numbers are no longer constants. If the wave

synchronism conditions are satisfied, then the evolution equations assume the classical form (we write one of them),

( )( )( ) ( ) ( ) ( )* ( )*

  A A A A A132

13 111

122

111

122′ = −σ , (2.60)

where the coefficients for the first phase σ1k  and for the second phase σ2k  are different. Compare, for example σ13 ,

σ

ω ω

λ µ λ µ13

11

2 12

3 11

13

3 3 2 22 2=

+

+ + +

l l N N  ( ) ( ) ( ) ( )

( ) ( )

( ) ( ) l 

k k 

k  k k 1

23

12

2 12

3

11

31

2

2 1

2

( )

( ) ( )

( )

( ) (

( )

( ) ( )

( ) ( )ω

ω ω

ω ω +[ ])

( )ω 3 ,

and σ23 ,

σω ω

λ µ λ µ23

11

2 12

3 12

13

2 2 3 32 2=

+

+ + +

l l N N  ( ) ( ) ( ) ( )

( ) ( )

( ) ( ) l 

k k 

k k k 

12

3

12

2 12

3

11

3

12

2 12

( )

( ) ( )

( )

( ) (

( )

( ) ( )

( )( )

ω

ω ω

ωω +[ ])

( )ω 3 .

They are also different from the classical one. The classical coefficients are constant, whereas the others are functions of 

the frequencies of all the waves.

The spatial synchronism condition has the form

k k k 11

1 12

2 13

3 0( ) ( ) ( )( ) ( ) ( )ω ω ω+ + = .

Let us now examine the evolution equations. Formally, they have a classical form. However, different phases will have

three different evolution equations with frequency-dependent coefficients. The situation is similar with the Manley–Rowe

relations. Three integrals (two independent and the third one derives from the first two) can easily be written for the evolution

equations. Different phases are described by three relations with different coefficients. Also, each triple of waves obeys the law

of conservation of energy

( )ω σ ω ω ωk k  k k 

 A( , , )( )

1 2 3 11 2

1

3

=∑ = const. (2.61)

 Remark 2.18. The energy of the mixture is distributed in two ways: (i) from wave to wave within each triplet (in each phase) and (ii) from mode to mode in case of change in the excitation frequency.

The Manley–Rowe equations make it possible to investigate some interesting physical effects associated with triplet

evolution in space. Let us consider some nonclassical cases such as the interaction of the first mode with itself, resulting in

generation of the second mode. Here the classical procedure is used. It is supposed that the initial amplitude of the third wave

 A132

0( )

( ) is zero and that the amplitudes A111( )

and A121( )

of the primary waves are constant. In establishing the synchronism

condition, it is assumed that ω ω ω1 2= = and ω ω3 2= . The solutions of the evolution equations are

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( )  A x x

l N N 

13 22 1

21

11

3

3 3 2 2

2

2 2( )

( )( ) ( ) ( )

( )( ) ( )

ω

ω

λ µ λ µ=

+

+ + +[ ] ( )

k A

12 1

1 2

111 2

2( )

( ) ( )

( )( )

ωω , (2.62)

  A x xl N N 

23 22 1

21

21

3

2 2 3

2

2 2( )

( )( ) ( ) ( )

( )( )

( ) (ω

ω

λ µ λ µ=

+

+ + +[ ] ( )

3 12 1

1 2

111 2

2) ( )( )

( )

( ) ( )

k A

ωω . (2.63)

It is then possible to calculate the evolution of the amplitude of the second harmonic in both phases.Thus, the first mode generates the second harmonic of the second mode. In different phases, the amplitudes of the new

wave increase differently. This is a new, theoretically revealed effect.

  Remark 2.19. This situation is common for mixtures. Considering a specific triplet in a two-phase mixture actually

implies considering two triplets with similar synchronism conditions and different amplitudes (i.e., the relative energies carried

 by the wave constituents are different). Such triplets exist separately in the phases of the mixture.

 Remark 2.20. Two similar harmonics of the first mode generate the second harmonic not only in the second mode but

also in the first one.

Let us consider the case where two waves enter the medium and one (first) of them carries a major portion of energy.

Then

~

( )

~

( ),

~

( )( ) ( ) ( )

  N N N  11

1

12

1

13

1

0 0 0 0>> = . (2.64)

The third Manley–Rowe relation has the form

σ σ σ3 111

1 1 131

1 3 111

30~

( )~

( )~

( )( ) ( ) ( )

  N x N x N C  − = = ; (2.65)

therefore,~

( )( )

 N x131

1 can increase only at the cost of ~

( )( )

 N x111

1 . However, according to the first Manley–Rowe relation

σ σ2 111

1 1 121

1 1~

( )~

( )( ) ( )

  N x N x C  − = , (2.66)

such an increase can occur only when~

( )( )

 N x121

1 decreases. On the other hand, the second Manley–Rowe relation must hold too:

σ σ σ3 121

1 2 131

1 3 121

20~

( )~

( )~

( )( ) ( ) ( )

  N x N x N C  − = = , (2.67)

and C 2 is small compared with C 3. Thus,~

( )( )

 N x131

can increase by no more than C N 2 3 121

0= σ~

( )( )

. But it is small.

If the first and second waves in the triplet are of low frequency and the third one is of high frequency, then we obtain an

interesting result well known in nonlinear physics: the energy of low-frequency waves cannot be transferred to high-frequency

waves. This looks like an increase in the signal frequency, i.e., the low-frequency signal wave (first wave) interacts with the

strong idler wave (second wave), forming a new high-frequency pumping wave (third wave). The energy of the new wave is low,

and the effect is weak.

 Remark 2.21. The distinction between the classical triplet and the triplet in a two-phase mixture is in the facts that the

energy is redistributed between the allied triplets in the phases of the mixture and that these two triplets exist simultaneously.

Let us now examine the case where a high-frequency wave as a constituent of a triplet entering a medium carries a major 

 portion of the triplet energy,~

( )~

( )( ) ( )

 N N 131

111

0 0>> ,~

( )( )

 N 121

0 . It then follows from the first and third Manley–Rowe formulas

( )~( )

~( )

~( ) ,

~( )

( ) ( ) ( ) ( )  N x N N x N x12

11

2

313

113

11 11

110= −

σ

σ( )= −

σ

σ1

313

113

110

~( )

~( )

( ) ( )  N N x (2.68)

that both~

( )( )

 N x111

1 and~

( )( )

 N x121

1 can increase considerably and simultaneously. Consequently, the energy of the high-frequency

wave may be pumped over to two different low-frequency waves. This phenomenon of parametric oscillations, known in

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nonlinear physics [27, 91, 92, 95], is called the break-down instability of a triplet, since it reflects the ability of a high-frequency

wave to break down into two low-frequency waves.

The next two sections are devoted to solitary (aperiodic) waves. We will briefly discuss a few principal results for 

quadratically nonlinear waves. For cubically nonlinear waves, such results are absent yet.

2.3. Solitary (Aperiodic) Waves by the Microstructural Theory of the First Order. We start with the basic system of 

wave equations (1.15)–(1.17). Let us define a solitary wave first. A solitary plane wave is meant an aperiodic wave whose profile

concentrates within a finite domain outside which the amplitude of the wave is either zero or almost zero. The finite domain is

called the bottom of the profile and its length is called the bottom length.Our goal is to show that classic quadratically nonlinear theory permits analyzing the interaction of not only harmonic

(periodic) waves with sinusoidal profiles but also aperiodic (simple) waves with arbitrary smooth initial profiles.

 Remark 2.22. A simple wave describes the distortion of the initial profile, and this distortion is due to the nonlinear 

dependence of the phase velocity on the phase. A similar dependence for the phase velocity is incorporated into the definition of 

dispersive periodic waves: the frequency and wave number appearing in the dispersion equation are in nonlinear relationship.

Therefore, the phase velocity depends nonlinearly on the frequency. This nonlinear dependence is the cause of the distortion of a

 pulse formed from waves with close frequencies. It is obvious that these mechanisms are similar.

We will further consider plane waves and two standard cases of their excitation. Let us begin with the first standard

case. This is about one longitudinal wave entering a medium. In this case, the wave phenomena are described by one equation

(2.1). It is convenient to rearrange it as follows:

u c u utt  L x xx12

1 11 0, , ,( )− + =α , (2.69)

where [ ]c L = +( ) /λ µ ρ2 is the phase velocity of a longitudinal wave in a linear elastic body and α λ µ= +[ / ( )] N 1 2 is a

nondimensional quantity.

The subsequent analysis is devoted to a wave of longitudinal displacement. We will deviate from the classic harmonic

solution and will search for the solution in the form of a simple wave—an initial disturbance propagating in space and varying in

time. This disturbance is a finite longitudinal displacement whose initial profile,

u x F x( , ) ( )0 1= , (2.70)

is a twice differentiable continuous function.

 Remark 2.23. The above-posed problem on the motion of a pulse may be considered as a model problem for a

semiinfinite rod: a longitudinal displacement, disturbance, initially generated at the end of the rod within a small bounded area

moves as a longitudinal wave along the rod.

The solution of Eq. (2.69) is sought in the form of the D’Alembert wave with an unknown variable phase velocity v ph

u x t F x v t  ( , ) ( )= −1 ph . (2.71)

 Remark 2.24. The phase velocity v ph may be treated as a local velocity at a point x and at time t . In this case, the analysis

of solution (2.71) agrees with the well-known procedure for simple waves. The procedure used below agrees also with

Lighthill’s description of Riemann’s waves [55].

In the case being considered, the formula v c u  x ph = +1 11 α , is valid, whence it follows that the phase velocity depends

nonlinearly on the solution, which means that the wave has all the attributes of a simple wave.

Instead of the exact solution (2.71), we may use an approximate formula accurate to within the squares of the small

nonlinear terms αu  x1, :

( )u x t F x c u t   x1 1 1 1

1 21( , ) ,

/= − +

α ( )( ) ( ) ( ) ( )[ ]≈ − − ≈ − − ′ − F x c t c tu F x c t c t F x c t   x1 1 1 1 1 1 1 1 1

21 2 1 2/ /,α α

( ) [ ] ( )= − = −u x t c t u x t u u x t   x1 1 1

2

10

11 2 1 2lin lin lin( , ) / ( , ) ( , ) /,α ( ) [ ]c t u u x t   x1 10 2

1

2α , ( , )lin , (2.72)

where u10 is the maximum amplitude in the initial profile and u x t 1

lin ( , ) is the linear solution normalized to u10 .

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There is a certain analogy between the simple wave solution (2.72) and the classical solution (2.8) of the first standard

 problem.

Let us look at this analogy in the case where the initial wave profile is aperiodic and has the form of a bell, i.e., the form

of the Chebyshov–Hermite function of zero index [55]:

u x a e x1 0

202

( , ) ( / )= − . (2.73)

We will search for the solution in the form of a more specific simple wave

u x t a e x v t  1 022

( , ) ,( / )= = −− σ σ ph . (2.74)

We obtain

[ ] ( ) [ ]( )u x t a e c t a e  x c t x c t  1 0

21 0

212

12

1 2( , ) /( ) / ( ) /≈ −′

− − − −α

2

[ ] ( ) ( ) ( )= − −− − − −a e c ta x c t a e  x c t   x c t 0

21 0 1

20

12

12

1 2( ) / ( )/ α . (2.75)

This formula is quite instructive. It better demonstrates the mentioned similarity between the solutions of the first

standard problem of nonlinear acoustics for a harmonic wave and for a simple bell-shaped wave. The similarity is primarily due

to the presence of exponent in the functional representations of two waves.

Let us now dwell on that similarity. First, recall the following representation of the solution for harmonic waves (2.8):

( )u x t a e k a xek x c t k x c t  1 0 1

20

2 21 1 1 11 8( , ) / ( ) ( )( ) ( )≈ −− − − −α . (2.76)

 Remark 2.25. The first term in Eq. (2.76) describes a linear harmonic wave, which is also called the first harmonic. The

second term also describes a linear harmonic wave, which is the second harmonic. This is the way the generation of the second

harmonic is described and this is the main feature of solution (2.76). However, there is one more important feature associated

with the form of the amplitude of the second harmonic. This amplitude is proportional to the squared wave number  k 12 , the

squared initial amplitude a0

2 , and the spatial coordinate x1

. The presence of the spatial coordinate is responsible for the distortion

of the initial profile. Such a distortion is the main nonlinear effect in this case and in the whole theory of nonlinear waves.

Let us now address solution (2.75). Its structure is the same as that of the classical solution (2.76). The first term on the

right-hand side describes a wave that is the initial bell-shaped profile moving without distortions with a constant phase velocity

equal to the velocity of longitudinal waves in a linear elastic body.

Thus, the first and second harmonics for the bell-shaped wave are e x c t − −( ) /12 2 and e x c t − −( )1

2, respectively. They both

are simple waves in the sense of D’Alembert since their velocity is constant. Thus, the effect of generation of the new simple

wave—second harmonic—is described using the above approach. Computer simulation of wave profile evolution was discussed

in [55].

The above-described interaction of longitudinal simple plane waves is not an exception. It must be manifested with all

types of waves. We will demonstrate this for simple transverse plane waves. Consider the second standard problem. Recall that it

is about transverse oscillation motion only. In this problem, wave motion is described by system (2.9), (2.10). This system issolved by the method of successive approximations, assuming smallness of the nonlinear terms in the second approximation. In

the first approximation, the transverse motion is linear and the solution assumes the form of a simple D’Alembert wave

u x t F F x c t  3 3 3 3 3( , ) ( ) ( )= ≡ −τ . (2.77)

The wave is simple in the sense of D’Alembert and its initial profile u x F x3 30( , ) ( )= propagates without distortions with

a constant velocity equal to that of classical transverse waves in an elastic medium, c3.

In the first approximation, the longitudinal wave does not interact with the transverse wave and it is not excited. The

second approximation for the transverse wave agrees with the first approximation, i.e., the simple wave has the basic property of 

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the harmonic wave—it does not generate new transverse waves. However, it generates a new longitudinal wave, as follows from

Eqs. (2.9) and (2.10).

Let us take representation (2.77) into account and write Eq. (2.9) in the form

( ) [ ]{ }u c u N F  tt xx1 12

1 1 3 32

3, , / ( ) /− = ∂ ∂ρ τ τ . (2.78)

It is easy to show that the partial solution of this equation with a known right-hand side has the form of a simple wave

[ ]u x t n1 2 3 3 3 1( , ) ( ) ( )= −Φ Φτ τ ,

( ) [ ]τ ρ τ θ θτ

1 1 2 2 32

12

3 3 32

0

2

3

= − = − = ∫   x c t n N c c F d  , / ( ) , ( ) ( )Φ .

Thus, the new simple D’Alembert longitudinal wave is the difference between two simple D’Alembert longitudinal

waves propagating with different phase velocities c1 and c3.

2.4. Solitary (Aperiodic) Waves by the Microstructural Theory of the Second Order. We start with the basic system of 

wave equations (1.31)–(1.33). A problem of simple waves in a microstructural medium such as a mixture arises quite naturally

once this problem is successfully solved in the classical formulation. However, there are some restrictions in this problem. The

first restriction is that the basic equations of mixture theory do not admit D’Alembert wave solutions.Let us discuss this problem. First recall that the equations of plane linear waves in a mixture are the direct generalization

of the classical Klein–Gordon equation. Both equations describe similar effects. The first of them is the microstructural

dispersion of harmonic waves.

From the mathematical standpoint, the first restriction is due to the presence of the term − −βα δ

( )( ) ( )

u uk k  .

In all cases, harmonic solutions follow from the property of the exponential function whereby all its derivatives are

expressed in terms of the function itself. Then the question logically arises: Will a pulse whose initial profile is not arbitrary, in

contrast to the D’Alembert solution, but is described by some function with predefined properties preserve its shape while

 propagating? Or, to put it differently, is there a solution in the form of a simple wave whose profile is defined by the initial

function?

Let us first outline this problem as a whole. Assume that, according to the above-mentioned property, the second

derivative of the function is expressed in terms of the function itself. This condition is not exotic. Some classes of special

functions, such as

the Chebyshov–Hermite function ′′ + + − =ψ ψ n n  z n z z  ( ) ( ) ( )1 2 02 ,

the Whittaker function ( ) ( )[ ]{ }′′ + − + + − =w z z w1 4 1 4 02 2/ / /λ / µ , and

the Mathieu function ′′+ − =w p q x w( cos )2 2 0,

 possess such a property. All the three equations have a similar form:

′′ = F z f z F z  ( ) ( ) ( ), (2.79)

 f  is a known function.

If we select the initial pulse in the form of the function F(x) from Eq. (2.79) and search for the solution in the form of a

simple wave with the same profile F z ( ) ( z x v z t  = − ph ( ) ), then the nonclassical terms − −β α δ( )( ) ( )u uk k  do not hamper the

transformation of the basic equations into the dispersion equations. In this case, however, the variability of the phase velocities

will be restricted tv z o′ =( ) ( )1 , which is the price we pay for using this approach.

Let the initial pulse be given by u x A x( ) ( )( , ) ( )α α ψ 0 0= . We will search for the solution in the form

u x t A z A e z 1 0

22( ) ( ) ( ) /( , ) ( )α α αψ = ≡ − , (2.80)

where z x v z t  = − ( ) is the phase and v z ( ) is the phase velocity. The final solution has the following form [55]:

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u x t A z p z A z A e1 0 0( ) ( ) ( ) ( ) ( ) ( ) ( )( , ) ( ) ( ) ( )α α α δ δ δ αψ ψ = + = − [ ] [ ]( ) / ( ) ( ) ( ) /( ) ( )

( ) z z   p z A eα δδ δ2 22 2+ − . (2.81)

Here, the phase is a number since two different phase velocities v( )α exist in the mixture. Thus, the simplicity of solution (2.81) is

due to two essential complications: nonlinear dependence of the phase velocity on the phase (the wave becomes simpler) and the

approximate form of the basic system.

The simple wave solution (2.80) can easily be generalized to the arbitrary Chebyshov–Hermite function

u x t A z  n1

( ) ( )( , ) ( )α α ψ = . The evolution of several initial profiles was numerically simulated and demonstrated by a great many

 plots in [14, 55].

The interaction of three simple waves with profile (2.80) was studied in [55] using the method of slowly varying

amplitudes. Two questions arose here: What is the slowness of a solitary wave and how do we formulate the resonance

conditions?

3. Cubically Nonlinear Elastic Waves. This type of waves has been studied much less than that discussed above. That

is why we cannot compare many results obtained for quadratically nonlinear waves with the corresponding results for cubically

nonlinear waves, the latter are just absent.

3.1. Harmonic (Periodic) Waves by the Microstructural Theory of the First Order. We start with the basic system of 

wave equations (1.22)–(1.24). Recall its representation

( ) ( )ρ λ µu u N u u N u u u u

tt 1 1 11 1 1 11 1 1 2 2 11 2 1 3 11 3 12

, , , , , , , ,− + = + +

( )+ + + N u u N u u u u u u3 1 11 1 12

4 2 11 2 1 1 1 3 11 3 1 1 1, , , , , , , ,( ) , (3.1)

( )ρ µu u N u u u utt 2 2 11 2 2 11 1 1 1 11 2 1, , , , , ,− = + + + + N u u N u u N u u4 2 11 2 12

5 2 11 1 12

6 2 11 3 12

, , , , , ,( ) ( ) ( ) , (3.2)

( )ρ µu u N u u u utt 3 3 11 2 3 11 1 1 1 11 3 1, , , , , ,− = + + + +  N u u N u u N u u4 3 11 3 12

5 3 11 1 12

6 3 11 2 12

, , , , , ,( ) ( ) ( ) , (3.3)

( )( ) ( ) ( ) ( )[ ]  N A B C N A B C  3 43 2 2 6 3 1 2 2 2 5 14 4= + + + + = + + + +/ , /λ µ λ µ ,

( )( )  N A B N A B C  5 63 2 2 2 3 10 4= + + + = + +/ ,λ µ .

Let the solution of the basic system (3.1)–(3.3) with all the nonlinear terms on the right-hand sides neglected be the zero

approximation. To obtain the first approximation, consider the system

( )ρ λ µu u N u u N u u utt 1 1 11 1 1 11 1 1 2 2 11 2 12,**

,**

,*

,*

,*

,*− + = + +( )3 11 3 1,

*,

*u

+ + + N u u N u u u u u u3 1 11 1 12

4 2 11 2 1 1 1 3 11 3 1 1,*

,*

,*

,*

,*

,*

,*( ) ( ),

*1 , (3.4)

( )ρ µu u N u u u utt 2 2 11 2 2 11 1 1 1 11 2 1,**

,**

,*

,*

,*

,*− = + + + +  N u u N u u N u u4 2 11 2 1

25 2 11 1 1

26 2 11 3 1,

*,

*,

*,

*,

*,

*( ) ( ) ( )2 , (3.5)

( )ρ µu u N u u u utt 3 3 11 2 3 11 1 1 1 11 3 1,**

,**

,*

,*

,*

,*− = + + + + N u u N u u N u u4 3 11 3 1

25 3 11 1 1

26 3 11 2 1,

*,

*,

*,

*,

*,

*( ) ( ) ( )2 , (3.6)

where u x t k * ( , )1 and u x t k 

** ( , )1 are the first and the second approximations of the solutions, respectively.

The uncoupled system of inhomogeneous wave equations (3.4)–(3.6) allows us to indicate some new possibilities in the

wave interaction analysis.

 Possibility 1. The first standard problem in quadratically nonlinear wave-interaction analysis deals with the generation

of second harmonics of one initially excited longitudinal plane wave. This problem is described by Eq. (3.4) that includes no

cubically nonlinear terms and no transverse waves:

( )ρ λ µu u N u utt 1 1 11 1 1 11 1 12, , , ,− + = . (3.7)

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In this case, the quadratically nonlinear term ( ), ,  N u u1 1 1 1 1 1 on the right-hand side is responsible for the

above-mentioned basic effect in the theory of nonlinear waves. The additional cubically nonlinear term N u u3 1 11 1 12

, ,( ) in

Eq. (3.4) is responsible for the generation of third harmonics. Thus, we have a new possibility to analyze the generation of third

harmonics.

 Possibility 2. Possibility 2 is the most natural special case of Possibility 1. We can analyze how the progress (either in

time or in space) of the second and third harmonics taken separately affects the evolution of the initial harmonic profile of the

longitudinal wave. Results of this analysis can be compared at this stage, but later they should be considered together.

  Possibility 3. In the second standard problem of the quadratically nonlinear wave-interaction analysis, a transverse

vertical wave is initially excited and new longitudinal waves are generated (transverse waves cannot be generated). Introducing

cubic nonlinearity endows this problem with new features. The term  N u u4 2 11 2 12

,*

,*( ) in Eq. (3.5) describing the propagation of a

transverse wave guarantees that in the approach of elastic potential a transverse horizontal wave will generate its own third

harmonics. It is also important that in the classical quadratic approach where the term N u u4 2 11 2 12

,*

,*( ) is absent, the initially

excited transverse wave in the form of the first harmonic does not generate other harmonics beside itself, and, therefore, the

second standard problem is not interesting in the context of transverse waves.

 Possibility 4. A new problem can be formulated within the framework of approach (3.4)–(3.6). We will call it the fourth

standard problem. Here a certain (say, vertical) transverse wave is initially excited, and then it generates another (horizontal)

transverse wave. Thus, it becomes possible to describe the new effect of energy pumping from one transverse wave to another.

The next two possibilities are associated with the method of slowly varying amplitudes. Let us return to Eqs. (3.1)–(3.3)and apply this method (which involves long calculations). Here we face many possibilities, of which we will mention two. Note

that using Eqs. (3.1)–(3.3), one can obtain and analyze the shortened and evolution equations only for the specific case of cubic

nonlinearity.

 Possibility 5. Using the evolution equations, we can study the interaction of four waves or the so-called wave quadruple

 problem. There are various possibilities for the choice of four elastic waves, including the case of two pumping waves, one signal

wave, and one idler wave, which is similar to the parametric amplification problem.

 Possibility 6. Using the evolution equations with cubic nonlinearity, we can analyze the self-switching problem (it has

 been considered above for quadratically nonlinear elastic waves). Here it is also possible to describe the frequency switching

mechanism for elastic waves whereby the frequency changes by a factor of three.

Each of the six possibilities can be treated as a particular development of the nonlinear model constructed here, on the

one hand, and as a theoretical prediction of new wave effects, on the other hand.Thus, there are many new possibilities for the analysis of nonlinear waves.

Let us start with the first possibility and consider the first standard problem. We neglect some nonlinear terms on the

right-hand side of the initial wave equation Eq. (3.4):

( )ρ λ µu u N u utt 1 1 11 3 1 11 1 122,

**,

**,

*,

*( )− + = . (3.7)

The first approximation is still linear and can be described by formula (2.2). The second approximation can be obtained

 by the procedure for quadratic nonlinearity:

( ) ( ) ( )u x t x N 

u k k x t  13

10 3

13

1

1

8 2** * *( , ) sin=

+  

    −

λ µω ( ) ( ) ( )−

+  

    −

1

24 23

310 3

13

1 x N 

u k k x t  λ µ

ω* *sin , (3.8)

and the full solution is expressed as u x t u x t u x t  1 1 1( , ) ( , ) ( , )* **= + .

The plots below show how the progress of the third harmonic affects the evolution of the longitudinal wave profile.

There is some similarity between the influence analyses in this and the quadratically nonlinear cases. First, the same three

materials were found out to be the most characteristic. We divide all the plots into two sets (with one parameter fixed and another 

varied), each set consisting of three groups. The essential distinction from the quadratically nonlinear case is that appreciable

influence at reasonable distances cannot be observed for small strains (small initial amplitudes) and low frequencies.

The transition from small to finite strains is possible with the Murnaghan potential, since it was originally introduced for 

finite strains.

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Figure 9 demonstrates three detected stages of evolution resulting from the progress of the third harmonic. In the figure,

four different parts of the same plot (see four rows of distance values under the horizontal axis) are superimposed. The stages of 

 profile evolution can be described in the following way:

Stage 1. The left part of the top of the cosine curve goes down (or moves toward the initial axis of vertical symmetry)

and the right part remains unchanged. This occurs at the upper area of the top, and this area occupies about half the maximum

amplitude.

Stage 2. The left part goes back to the level of the fixed right part and deviates slightly to the left from the initial cosine

shape. At the same time, a plateau with two small humps is gradually formed. These humps stay at the level of the initial peak.

Stage 3. The top of the right hump slowly approaches the plateau level and then remains unchanged at the level of initial

 peak. The left hump grows rapidly, its right part being slightly steeper. This increase can be traced on the plots where the

amplitude values lie between the initial maximum amplitude and half the maximum (i.e., within the limits of validity of the

approach being used).

The first group of plots corresponds to a fixed initial amplitude of 0.1 mm and varying frequencies. Figure 10 represents

the material 62. Here only the first stage can be observed (the profile’s left part tends toward the ordinate axis). The effect is quite

evident for the material chosen. The plot corresponds to a frequency of 100 kHz.

The plot in Fig. 11 corresponds to an initial frequency of 400 kHz. Here we see the first two stages and the beginning of 

the third one (an intermediate stage of evolution resulting from progress of the third harmonic for a fixed initial amplitude) for the

material 62.

The plot in Fig. 12 corresponds to an initial frequency of 700 kHz. This frequency is extremely high for the material 62;

that is why the evolution is well developed even at very small distances (the limiting stage of evolution resulting from the

 progress of the third harmonic for a fixed initial amplitude).

The second group of plots corresponds to a fixed frequency of 400 kHz and a varying initial amplitude. There are three

sets of plots within this group similar to the previous ones. The first set of plots demonstrates poorly developed evolution for a

small initial amplitude of 0.05 mm. The materials studied display different rates of evolution. The evolution rate is maximum for 

the material 62 (Fig. 13)—the first two stages are clearly manifested at small distances (a poorly developed stage of evolution

due to the progress of the third harmonic for a fixed initial frequency).

The next plot corresponds to an amplitude twice as large as the initial amplitude (0.1 mm). This group of plots is

represented in much the same way as the previous one. The progress in the evolution is almost the same. But it occurs at smaller 

distances here—different materials show different progress (an intermediate stage of evolution due to the progress of the third

harmonic for a fixed initial frequency). The main observation is that a moderate increase in the initial amplitude causes a

moderate acceleration in the evolution. The previously mentioned distinctions between materials remain.

1390

Fig. 9

0 0.02 0.04 0.06 0.08 0.10.12 0.14 0.16 0.18 0.20.22 0.24 0.26 0.28 0.30.32 0.34 0.36 0.38 0.4

0.15

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The last plot corresponds to an initial amplitude five times greater than 0.1 mm (Fig. 14). Similarly to Figs. 3, 7, and 13,

the materials 11 and 62 represent a limiting case of evolution, which means that the wave profile becomes strongly distorted after 

several initial oscillations (developed evolution due to the progress of the third harmonic for a fixed initial frequency).

Thus, a ten-fold increase in the amplitude (from 0.05 to 0.5 mm) results in the manifestation of all the stages of 

evolution at rather small distances for the material 62.

In contrast to the second harmonic, the progress of the thirdharmonic has a different effect on the evolution (the patterns

of wave profile evolution are essentially dissimilar) and the resulting influence is more sensitive to changes in the initial

amplitude than to changes in the initial frequency. The third harmonic of a longitudinal wave can be detected at higher 

frequencies and higher amplitudes than the second harmonics.

 Remark 3.1. Cubic and quadratic nonlinearities are both present. Therefore, the observed second and third harmonics of a longitudinal wave cannot be separated (or can be separated conditionally). The third harmonic can be experimentally detected

only in combination with the second one. The computer simulation revealed that it is possible to detect second harmonics whose

initial frequencies and amplitudes much lower than those needed to detect the third harmonic. In some materials (e.g., the

materials 11 and 62), when the second harmonic is fully mature, the third harmonic has not even begun to develop yet. However,

the material 41 is an example of materials in which both harmonics affect the evolution simultaneously. This is, however,

observed within a range where the second harmonic already dominates and the third harmonic still develops.

  Remark 3.2. The above-mentioned difficulties with separation of the effects of the second and third harmonics for 

longitudinal waves are absent for transverse waves. In this case, the second harmonic is not excited, and we observe only the

third harmonic. This enables us to combine theoretical and experimental studies.

1391

Fig. 10

0.1

0 20.2 20.4 20.6 20.8 21

Fig. 11

0 0.6 0.7 0.8 0.9

0.1

Fig. 12

0.15

0 0.05 0.1 0.15 0.2 0.25

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Let us now analyze a typical problem for cubically nonlinear waves using the method of slowly varying amplitudes. Let

only a longitudinal wave be initially excited and let it do not generate transverse waves.

We will exclude from the analysis the effect of quadratic nonlinearity on the interaction of longitudinal waves,

assuming that this problem has been studied well. Thus, we will analyze the self-interaction and interaction of longitudinal

waves with one another. These effects are described by only one equation (2.9)

( )ρ λ µu u N u utt 1 1 11 3 1 11 1 122, , , ,( )− + = . (3.9)

 Remark 3.3. It is useful to note that so-called four-wave interactions are most interesting from the physics standpoint in

the wave interaction analysis for cubically nonlinear media. Just as three-wave interactions in quadratically nonlinear media

imply that wave triplets occur, four-wave interactions in cubically nonlinear media imply that wave quadruplets can form under certain conditions. Therefore, an analysis of four-wave interactions in an elastic medium (according to Eq. (3.9)) seems

 promising.

General conditions for effective interactionof waves-participants are matching of frequencies and wave vectors [82, 88]:

ω ω ω ω4 1 2 3=± ± ± , (3.10)

r r r rk k k k  4 1 2 3= ± ± ± . (3.11)

The scheme of interaction according to the general conditions (3.10) and (3.11) is usually interpreted in optics [88] as

the generation of a new wave by three different pumping waves. This scheme can be implemented in an infinite number of ways,

1392

Fig. 13

0.04

0 3.1 3.2 3.3 3.4 3.5

Fig. 14

0 50.2 50.4 50.6 50.8 51

0.1

Fig. 15

1.5

0 0.025 0.05 0.075 0.1 0.125 0.15 0.175

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 by choosing different directions of pumping waves. One of the best-studied schemes additionally assumes that the outgoing

(fourth) wave is characterized by the same parameters (frequency and wave vector) as one of the pumping waves. Another 

widely used scheme considers the following waves: two pumping waves, one signal wave, and one idler wave. We studied this

scheme for Eq. (3.9) in [82].

We started the analysis with two-wave interaction using conditions for the existence of stable quadruplets in the form

ω ω ω ω1 2 3 4+ = + , (3.12)

r r r rk k k k  1 2 3 4+ = + . (3.13)

This case may be regarded as the first step in the analysis of four-wave interaction, which represents the real, so-called

wave-front inversion (WFI) scheme for optic waves. According to this scheme, two identical pumping waves with a nonsmall

amplitude A z A z A z  1 2( ) ( ) ( )= = enter a medium from two opposite sides (along the abscissa axis). While propagating through

the medium, the waves interact, the interaction being considered as two-wave interaction. Simultaneously, a weak signal with a

small amplitude A3 propagates perpendicularly to those two waves (i.e., along the applicate axis). According to condition (3.12),

this signal generates a fourth wave, which is also weak, has a small amplitude A4, and propagates in the opposite direction to the

wave A3.

The interaction of the weak waves is analyzed as four-wave interaction. The combined interaction is manifested as an

infinite increase in the amplitudes of the weak waves with time.

 Remark 3.4. The necessity to consider two-wave interactions in cubically nonlinear media follows from two hypotheses

formulated especially for this scheme. Hypothesis 1: Two weak waves (signals) do not influence the two pumping waves;

therefore, the pumping waves can be considered independently. Hypothesis 2: The pumping waves influence the weak signals;

therefore, in analyzing the interaction of the signals, all the four waves should be considered together, assuming that the pumping

waves are known.

Taking the aforementioned into account, we first consider the two-wave interaction of longitudinal elastic waves and

represent the solution of Eq. (3.9) according to the method of slowly varying amplitudes:

u x t A x e B x ei k x t i k x t    A A B B( , ) ( ) ( )( ) ( )1 1 1

1 1= +− +ω ω . (3.14)

Implementing this method, we obtain one shortened equation

( )( )k A e k B e N k A A xi k x t  

 B xi k x t  

 A  A A B B

,( )

,( ) /

11

11

342 2− ++ = +ω ω λ µ { 3 3 4 3 3e k B ei k x t  

 Bi k x t    A A B B( ) ( )− ++ω ω

+ + +− + +k k k k A Be k k k   A B A Bi k x t k x t  

 A B A  A A B B2 2 2 22( ) ([ ( ) ( )]ω ω }+ − + +2 2 2k AB e B

i k x t k x t    A A B B) [( ) ( )]ω ω . (3.15)

Shorten equations are usually split. To split Eq. (3.15), we will neglect the self-influence of waves and analyze the

mutual influence of two waves. Consideration should be given to the fact that the frequencies of both waves are equal,ω ω A B= ,

i.e., the frequency synchronism condition is valid for these two waves. Then Eq. (3.15) is split into the following two equations:

( ) ( )  A k k k k A Be B k k k k AB e  x A B A Bi k k x

  x A B A Bi A B

,( )

,,1

11

2 22 2= + = ++ ( )k k x A B+ 1 . (3.16)

Under the conditionr rk k  A B+ = 0, the evolution equations below follow from (3.16):

  A k A B B k AB x A x A, ,,1 1

3 2 3 2= = . (3.17)

Let us return to the WFI scheme and take into account the equality of the initial amplitudes of both waves,

  A x B x A x( ) ( ) ( )1 1 30 0= = = = (that the amplitudes depend on the coordinate x3 means that the scheme considers a wave beam

and the amplitude in the beam cross-section is not uniform). Then the solution of the nonlinear system (3.17) can be written

explicitly:

  A x A x e B x A x ek A x x k A x A A( ) ( ) , ( ) ( )( ( )) ( (1

03 1

03

3 03

21

3 0= =− 3

21)) x . (3.18)

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  Remark 3.5. From (3.18) it follows that the traditional nonlinear interaction of two identical opposite waves is very

specifically described by the method of slowly varying amplitudes: waves (wave beam) meet in the cross-section x1 = 0 and

 begin to interact, with the frequenciesω ω A B= and velocities v k k   A A B B= =( / ) ( / )ω ω remaining constant and the amplitudes

varying sinusoidally with a maximum amplitude A 0 and a period T N k A A

= +( ( / [ ( ) ]π λ µ2 33 0 2 ). A feature of the pumping

waves revealed here is that their amplitude is constant and the constancy is due to energy pumping. Thus, the hypothesis of 

negligible exhaustion of pumping wave energy can be accepted.

Let us point out another feature of the pumping waves. Energy is constantly pumped into these waves, but they

  propagate through an elastic medium that does not permit energy outflow. Thus, energy goes to other waves, and the full

four-wave interaction scheme has to be used. In this case, two weak waves that receive energy from the pumping waves have to

 be additionally considered. It should be noted that the medium is elastic and all wave phenomena that occur in it range from

kilohertzs to megahertzs.

In analyzing the interaction of weak waves, Hypothesis 2 formulated above should be born in mind; i.e., the general

four-wave interaction scheme should be used and then the shortened and evolution equation should be written for this (more

general) case.

Let us write the solution in the form of four longitudinal waves with different characteristics (amplitudes, wave vectors,

and frequencies):

u x t A x e k x t  mm

i

m m mm

( , ) ( ) , .= = −=∑1

4

ϕ

ϕ ω (3.19)

Hereafter the subscript “1” in x1 is omitted.

Applying the method of slowly varying amplitudes, we obtain the shortened equation

k dA

dxe

iN k k A A em

m i

m

n k  n k i

n

m n k ϕ ϕ ϕ

λ µ=

+∑ =−

+1

43 2 2 2 2

2 2( )( )

==∑∑

1

4

1

4

. (3.20)

Here we have to use the frequency synchronism condition; it has the form (3.12) and corresponds to the WFI scheme.

As a result, shortened equations can be written as

( )[ ] ( )  A iN k k k k k k k A A A e x

i k k 

1 3 2 3 4 11

2 3 4 2 3 421 2

,

(

/ ( )= − + + +− − − +

λ µ [ ]k k x

k A A A3 4

1

3

1 1 1

+

+)

, (3.21)

( )[ ] ( )  A iN k k k k k k k A A A e xi k k 

2 3 1 3 4 21

1 3 4 1 3 42 1 2,

(/ ( )= − + + +− − − +λ µ [ ]k k xk A A A3 4

23

2 2 2+ +) , (3.22)

( )[ ] ( )  A iN k k k k k k k A A A e xi k k 

3 3 1 2 4 31

1 2 4 2 3 42 1 2,

(/ ( )= − + + +− − − +λ µ [ ]k k xk A A A3 4

33

3 3 3+ +) , (3.23)

( )[ ] ( )  A iN k k k k k k k A A A e xi k k 

4 3 1 2 3 41

1 2 3 1 2 32 1 2,

(/ ( )= − + + +− − − +λ µ [ ]k k xk A A A3 4

43

4 4 4+ +) . (3.24)

Further we apply the condition for matching of the wave vectors and obtain the following evolution equations from the

nonlinear system (3.21)–(3.24):

 A A A A A A A A A A A A A A x x1 1 2 3 4 1 1 1 1 2 2 1 3 4 2 2 2 2, ,, ,= + = +κ σ κ σ

 A A A A A A A A A A A A A A x x3 3 1 2 4 3 3 3 3 4 4 1 2 3 4 4 4 4, ,,= + = +κ σ κ σ , (3.25)

where ( )[ ] ( )κ λ µ1 3 2 3 4 11

2 3 42= − + + +−iN k k k k k k k  / ( ) and ( )σ λ µ1 3 13 2= − +iN k  / .

In analyzing the evolution equations, it is frequently appropriate to assume that the self-generation effect of each wave

is weaker than the interaction of waves with one another. This implies that the second summands on the right-hand sides in (3.25)

can be neglected. Adopting this hypothesis, we obtain the evolution equations in the form

′ =  A A A A1 1 2 3 4κ  , ′ =  A A A A2 2 1 3 4κ  , ′ =  A A A A3 3 1 2 4κ  , ′ =  A A A A4 4 1 2 3κ  . (3.26)

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 Remark 3.6. It should be noted that the evolution equation (3.26) corresponds to a quite general four-wave interaction

scheme. The WFI scheme is narrower and a constituent of the general scheme.

The WFI scheme employs the last two evolution equations. They are simpler because the pumping waves are

known—expressed by formulas (3.18). We can now determine A A1 2 as A A A1 2 10 2= | | and obtain the evolution equations in the

form

( )′ =  A A A3 3 10 2

4κ  , ( )′ =  A A A4 4 10 2

3κ  . (3.27)

It is evident that we can find the analytical solution of system (3.27) and then conduct the subsequent analysis

numerically, carrying out computer simulations for various materials and various ranges of ultrasonic waves.

In the last part of the present study, we would like to focus on the capabilities of the energy analysis and, more

specifically, on the first integrals of the nonlinear evolution equations (3.27)—the Manley–Rowe relations and the general

energy balance law following from them.

The procedure is well known for nonlinear waves of any nature. The evolution equations are the starting point; we start

with Eqs. (3.27).

Let us multiply the first equation by A1:

 A A A A A A1 1 1 1 2 3 4′ =κ  . (3.28)

Performing the operation of complex conjugation in the first equation and multiplying the resultant equation by A1, we

finally obtain

 A A A A A A1 1 1 1 2 3 4′ =−κ  . (3.29)

After that, we sum (3.28) and (3.29) and use the notation A A A A A S  1 1 1 1 12

1′ + ′ = ′ = ′(| | ) for the intensity of a wave:

( )′ = −S A A A A A A A A1 1 1 2 3 4 1 2 3 4κ  . (3.30)

The other three relations can be derived similarly:

( )′ = −S A A A A A A A A2 2 1 2 3 4 1 2 3 4κ  , (3.31)

( )′ = − +S A A A A A A A A3 3 1 2 3 4 1 2 3 4κ  , (3.32)

( )′ = − +S A A A A A A A A4 4 1 2 3 4 1 2 3 4κ  . (3.33)

It can be easily seen that the first integrals of the system of evolution equations (known as the Manley–Rowe relations)

follow from (3.30)–(3.33)

( ) ( ) ( ) ( )S S S S  1 1 2 2 3 3 4 4/ / , / /κ κ κ κ  − = − =const const,

( ) ( ) ( ) ( )S S S S  1 1 3 3 2 2 4 4/ / , / /κ κ κ κ  + = + =const const.

The general energy balance law can be derived from the last equations by multiplying the mth equation by ω m and

summing all the terms:

( )ω κ m m mm

S /=

∑ =1

4

const. (3.34)

The combination of the evolution equations and the Manley–Rowe relations is the basis for analysis of many four-wave

interaction problems.

4. Concluding Remarks. Quadratically nonlinear waves in elastic materials have been investigated much better than

cubically nonlinear waves. At least three different approaches—the method of successive approximations, the method of slowly

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varying amplitudes, and the wavelet-based method—apply well to quadratically nonlinear waves. Most likely, all these

approaches can also be applied (and we have already started applying them) to cubically nonlinear waves.

The main wave effects well studied for quadratically nonlinear waves and methods for their analysis should be used as

guiding lines for the cubically nonlinear wave analysis, because many first publications on the interaction of cubically nonlinear 

waves demonstrated a certain correspondence between quadratic and cubic wave effects.

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