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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 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 α αλ µ= + + + + ,
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( ) ( )[ ] N A B C 4 1 2 2 2 5 14 4( )
/α
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
t
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
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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:
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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
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
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
+
−
+ ++
+ω
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=
+
+ + +[ ] ( )
l
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) ( )( )
( )
( ) ( )
l
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.
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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
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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.
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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,
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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
k
. (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.
REFERENCES
1. V. J. Ablowitz and H. Segur, Solitons and the Inverse Scattering Problem, SIAM, Philadelphia (1981).
2. A. A. Andronov, A. A. Vitt, and S. E. Khaikin, Theory of Oscillations [in Russian], Nauka, Moscow (1981).
3. L. Ascione and A. Grimaldi, Elementi di Meccanica del Continue, Massimo, Napoli (1993).
4. C. Banfi, Introduzione alla Meccanica dei Continui, CEDAM, Padova (1990).
5. C. Cattani and L. Toscano, “Hyperbolic equations in wavelet bases,” Acoustic Bulletin, 3, No. 2, 3–9 (2000).
6. C. Cattani and M. Pecoraro, “Nonlinear differential equations in wavelet basis,” Acoustic Bulletin, 3, No. 4, 4–10 (2000).
7. C. Cattani, “Wavelet solutions of evolution problems,” Atti Accademia Peloritana dei Pericolanti, Classe I, Scienze Fis.
Mat. e Nat., LXXX, 46–50 (2002).
8. C. Cattani and A. Ciancio, “Wavelet analysis of linear transverse acoustic waves,” Atti Accademia Peloritana dei
Pericolanti, Classe I, Scienze Fis. Mat. e Nat., LXXX, 1–20 (2002).
9. C. Cattani and A. Ciancio, “Energy wavelet analysis of time series,” Atti Accademia Peloritana dei Pericolanti, Classe I,
Scienze Fis. Mat. e Nat., LXXX, 67–77 (2002).
10. C. Cattani, “Wavelet analysis of dynamical systems,” Electronics and Communications, No. 16, 166–182 (2002).
11. C. Cattani and Ya. Ya. Rushchitskii, “Plane waves in cubically nonlinear elastic media,” Int. Appl. Mech., 38, No. 11,
1361–1365 (2002).
12. C. Cattani, “The wavelet-based technique in dispersive wave propagation,” Int. Appl. Mech., 38, No. 4, 493–501 (2003).
13. C. Cattani, Ya. Ya. Rushchitskii, and S. V. Sinchilo, “Propagation of the energy of nonlinearly elastic plane waves,” Int.
Appl. Mech., 39, No. 5, 583–586 (2003).
14. C. Cattani and Ya. Ya. Rushchitskii, “Cubically nonlinear elastic waves: wave equations and methods of analysis,” Int.
Appl. Mech., 39, No. 10, 1115–1145 (2003).
15. S. Earnshow, “On the mathematical theory of sound,” Trans. Royal Society of London, 150, 133–156 (1860).
16. J. K. Engelbrecht and U. K. Nigul, Nonlinear Strain Waves [in Russian], Nauka, Moscow (1981).
17. V. I. Erofeyev, Wave Processes in Solids with Microstructure [in Russian], Mosk. Gos. Univ., Moscow (1999).
18. Z. A. Goldberg, “On interaction of plane longitudinal and transverse waves,” Akust. Zh., 6, No. 2, 307–310 (1960).
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27. M. I. Rabinovich and D. I. Trubetskov, Introduction to Theory of Oscillations and Waves [in Russian], Nauka, Moscow
(1984).
28. Ya. Ya. Rushchitskii, “A nonlinear wave in a two-phase material,” Dop. Akad. Nauk Ukr. RSR, Ser. A, No. 1, 49–52
(1990).
29. Ya. Ya. Rushchitskii, “A plane nonlinear wave in a two-phase material,” Dop. Akad. Nauk Ukr. RSR, Ser. A, No. 2,
45–47 (1990).
30. Ya. Ya. Rushchitskii and I. A. Ostrakov, “Generation of new harmonics of nonlinear elastic waves in a composite
material,” Dop. Akad. Nauk Ukr. RSR, Ser. A, No. 10, 63–66 (1991).
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31. Ya. Ya. Rushchitskii and I. A. Ostrakov, “Distortion of a plane harmonic wave propagating in a composite material,”
Dop. Akad. Nauk Ukr. RSR, Ser. A, No. 11, 51–54 (1991).
32. Ya. Ya. Rushchitskii, “Interaction of elastic waves in a two-phase material,” Prikl. Mekh., 28, No. 5, 13–21 (1992).
33. Ya. Ya. Rushchitskii and E. V. Savel’eva, “Evolution of harmonic wave propagating in a two-phase material,” Prikl.
Mekh., 28, No. 9, 42–46 (1992).
34. Ya. Ya. Rushchitskii and V. O. Bilyi, “On longitudinal and transverse affinor Green’s functions and existence of wave
triplets in multiphase media,” in: Abstracts of Papers Read at Int. Math. Conf. dedicated to Academic P. Kravchuk ,
Kiev–Lutsk, Ukraine (1992), p. 184.35. Ya. Ya. Rushchitskii, “Interaction of compression and shear waves in a composite material with nonlinearly elastic
components in the microstructure,” Prikl. Mekh., 29, No. 4, 18–26 (1993).
36. Ya. Ya. Rushchitskii, “Nonlinear plane waves in an orthotropic body,” Dop. Akad. Nauk Ukrainy, No. 12, 60–62 (1993).
37. J. J. Rushchitsky, “Analytical investigation of wave triplets in a multi-phase medium,” in: Abstracts of Papers Read at
the 1st European and 13th Int. Conf. on Nonlinear Vibrations, Hamburg–Harburg, Germany (1993), p. 138.
38. Ya. Ya. Rushchitskii, “Resonance interaction of nonlinear waves in two-phase mixtures,” Prikl. Mekh., 30, No. 5, 32–41
(1994).
39. J. J. Rushchitsky, “The combinational scattering of sound on sound in multi-phase solids,” in: Abstracts of Lectures Read
at the 26th Symp. on Vibrations in Physical Systems, Poznan, Poland (1994), pp. 124–125.
40. Ya. Ya. Rushchitskii and V. O. Bilyi, “Toward the existence of certain type of combinational scattering of sound on
sound in a two-phase solid,” Dop. Akad. Nauk Ukrainy, No. 10, 58–63 (1994).41. Ya. Ya. Rushchitskii and I. N. Khotenko, “Linear elastic waves in two-phase piezoelectrics,” Dop. Akad. Nauk Ukrainy,
No. 3, 41–43 (1995).
42. J. J. Rushchitsky, “Interaction of elastic waves in an isotropic multi-phase materials,” J. Theor. Appl. Mech., Bulgarian
Acad. Sci., No. 5, 82–93 (1994–1995).
43. J. J. Rushchitsky, “Wave triplets in two-phase composites,” Mech. Comp. Mater ., 31, No. 5, 660–670 (1995).
44. Ya. Ya. Rushchitskii, “Analysis of wave interaction in two-phase materials within the framework of the micro-structural
theory of mixtures,” in: Abstracts of Papers Read at the Int. Sci. Colloq. on Nonlinear Dynamics of Solids with
Microstructure [in Russian], Nizhnii Novgorod, Russia (1995), pp. 21–22.
45. Ya. Ya. Rushchitskii, “Waves and the direct piezoelectric effect in two-phase piezoelectrics,” Prikl. Mekh., 31, No. 10,
42–48 (1995).
46. J. J. Rushchitsky, “Lax–Nelson problem on the direct piezoelectric effect in two-phase materials,” ZAMM (Special issuefor lectures of ICIAM-95), 52, No. 1, 411–414 (1996).
47. Ya. Ya. Rushchitskii, E. V. Savel’eva, and A. P. Kovalenko, “Self-generation of transverse waves in hyperelastic
media,” Prikl. Mekh., 32, No. 6, 30–38 (1996).
48. J. J. Rushchitsky, “New properties of transverse waves in quadratically nonlinear elastic materials (non-classic results in
classic theory),” in: Abstracts of Lectures Read at the 26th Symp. on Vibrations in Physical Systems , Poznan, Poland
(1996), pp. 244–245.
49. Ya. Ya. Rushchitskii, “Three-wave interaction and generation of the second harmonic in single-phase and two-phase
hyperelastic media,” Prikl. Mekh., 32, No. 7, 38–45 (1996).
50. J. J. Rushchitsky, “Phenomena of break down instability and parametric amplification of waves in two-phase materials,”
in: Abstracts of Papers Read at the 31st Solid Mechanics Conf. SolMech’96 , Olsztyn–Mierki, Poland (1996),
pp. 211–212.51. Ya. Ya. Rushchitskii and V. O. Bilyi, “On the break-down instability of triplets in a hyperelastic two-phase medium,”
Dop. NAN Ukrainy, No. 11, 63–69 (1996).
52. Ya. Ya. Rushchitskii, “Nonlinear waves in solid mixtures,” Prikl. Mekh., 33, No. 1, 3–38 (1997).
53. J. J. Rushchitsky and I. M. Khotenko, “Nonlinear plane waves in piezoelectric powders,” in: Abstracts of Lectures Read
at the 18th Symp. on Vibrations in Physical Systems, Poznan, Poland (1998), pp. 304–305.
54. Ya. Ya. Rushchitskii and I. M. Khotenko, “On nonlinear waves in two-phase piezopowders,” Int. Appl. Mech., 34,No.8,
746–754 (1998).
55. Ya. Ya. Rushchitskii and I. M. Khotenko, “Constructing the quadratically nonlinear theory of waves in two-phase
piezoelectric powders,” Dop. Akad. Nauk Ukrainy, No. 9, 61–67 (1998).
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56. Ya. Ya. Rushchitskii and I. M. Khotenko, “Nonlinear plane harmonic waves in two-phase piezoelectric powders,” Dop.
Acad. Nauk Ukrainy, No. 10, 60–66 (1998).
57. Ya. Ya. Rushchitski and S. I. Tsurpal, Waves in Materials with Microstructure [in Russian], Inst. Mekh., Kiev (1998).
58. J. J. Rushchitsky, “Interaction of waves in solid mixtures,” Appl. Mech. Rev., 52, No. 2, 35–74 (1999).
59. Ya. Ya. Rushchitskii, “On the classification of elastic waves,” Int. Appl. Mech., 35, No. 11, 1104–1110 (1999).
60. J. J. Rushchitsky, “Theoretical and computer modeling of non-linearly deformed piezoelectric powders,” Int. J. Nonlin.
Sci. Phys. Simul ., No. 2, 202–213 (2000).
61. Ya. Ya. Rushchitskii, “Extension of the microstructural theory of two-phase mixtures to composite materials,” Int. Appl. Mech., 36, No. 5, 586–614 (2000).
62. J. J. Rushchitsky, “Phenomenon of self-switching waves: statement, shortened and evolution equations,” in: Abstracts of
Lectures Read at the 19th Symp. on Vibrations in Physical Systems, Poznan, Poland (2000), pp. 202–203.
63. J. J. Rushchitsky, “Novel solitary waves in elastic materials: existence and nonlinear interaction,” in: Abstract Book of
the ICTAM 2000, Chicago, USA (2000), p. 165.
64. Ya. Ya. Rushchitskii, “Novel solitary waves in elastic materials: existence and nonlinear interaction,” Int. Appl. Mech.,
37, No. 7, 921–928 (2001).
65. Ya. Ya. Rushchitskii, “Self-switching of plane waves in hyperelastic materials,” in: Abstracts of Lectures Read at the 8th
All-Russian Congr. on Applied and Theoretical Mechanics [in Russian], Perm, Russia (2001), p. 56.
66. Ya. Ya. Rushchitskii, “Self-switching of waves in materials,” Int. Appl. Mech., 37, No. 11, 1492–1498 (2001).
67. J. J. Rushchitsky and S. V. Sinchilo, “Energy of plane harmonic waves in composite materials,” in: Abstracts of Papers Read at the 1st SIAM-EMS Conf. on Applied Mathematics in Our Changing World , Berlin, Germany (2001), p. 46.
68. J. J. Rushchitsky, “Computer-aided analysis of the new type of waves in elastic materials,” in: Book of Abstracts of the
5th World Congr. on Computational Mechanics, Vol. 1, Vienna, Austria, (2002), p. 286.
69. Ya. Ya. Rushchitskii, I. N. Khotenko, and E. V. Savelieva, “Plane shear waves in piezopowders: unexpected new
phenomenon—the generation of the third harmonics,” in: Book of Abstracts of the 30th Int. Summer School “ Advanced
Problems in Mechanics”, St. Petersburg, Russia (2002), p. 84.
70. J. J. Rushchitsky, “Self-switching of displacement waves in elastic nonlinearly deformed materials,” Comptes Rendus de
l’Academie des Sciences, Serie IIb Mecanique, 330, No. 2, 175–180 (2002).
71. J. J. Rushchitsky, “Some new aspects of the plane wave second harmonics generation in elastic bodies,” in: Abstracts of
Papers Read at the 20th Symp. on Vibrations in Physical Systems , Poznan, Poland (2002), 252–253.
72. J. J. Rushchitsky and E. V. Terletska, “Computer modelling of the plane solitary wave evolution (the micro-structurecharacteristic size and the wave bottom interaction),” in: Abstracts of Papers Read at the 20th Symp. on Vibrations in
Physical Systems, Poznan, Poland (2002), pp. 254–255.
73. J. J. Rushchitsky, I. N. Khotenko, and E. V. Savelieva, “Some new aspects of the plane wave second harmonics
generation in elastic bodies,” in: Abstracts of Papers Read at the 20th Symp. on Vibrations in Physical Systems , Poznan,
Poland (2002), pp. 256–257.
74. J. J. Rushchitsky and C. Cattani, “Nonlinear acoustic waves in materials: retrospect and some new lines of
development,” in: Abstracts of Workshop on Potential Flows and Complex Analysis, Kiev, Ukraine (2002), p. 16.
75. Ya. Ya. Rushchitskii and C. Cattani, “Generation of the third harmonics by plane waves in Murnaghan materials,” Int.
Appl. Mech., 38, No. 12, 1482–1487 (2002).
76. Ya. Ya. Rushchitskii and C. Cattani, “The subharmonic resonance and second harmonic of a plane wave in nonlinearly
elastic bodies,” Int. Appl. Mech., 39, No. 1, 93–98 (2003).77. Ya. Ya. Rushchitskii, C. Cattani, and E. V. Terletska, “The effect of the characteristic dimension of a microstructural
material and the trough length of a solitary wave on its evolution,” Int. Appl. Mech., 39, No. 2, 197–202 (2003).
78. J. J. Rushchitsky and C. Cattani, “The third harmonics generation and wave quadruples,” in: Abstracts of GAMM Annual
Conf ., Padua, Italy (2003), p. 234.
79. Ya. Ya. Rushchitskii, “Cubic nonlinearity in the theory of waves in elastic materials,” in: Abstracts of Papers Read at the
6th Int. Conf. on Mathematical Problems in the Mechanics of Inhomogeneous Structures [in Russian], Lviv, Ukraine
(2003), pp. 50–52.
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80. Ya. Ya. Rushchitskii, E. V. Savel’eva, and I. N. Khotenko, “Cubic nonlinear waves in piezoelastic materials,” in:
Abstracts of Papers Read at the 6th Int. Conf. on Mathematical Problems in the Mechanics of Inhomogeneous Structures
[in Russian], Lviv, Ukraine (2003), pp. 52–53.
81. Ya. Ya. Rushchitskii and C. Cattani, “Solitary elastic waves and elastic wavelets,” Int. Appl. Mech., 39, No. 6, 741–752
(2003).
82. J. J. Rushchitsky and C. Cattani, “Cubic nonlinear elastic waves: interaction, wave quadruples,” in: Abstracts Book of the
5th EUROMECH Solid Mech. Conf ., Thessaloniki, Greece (2003), pp. 68–69.
83. J. J. Rushchitsky, C. Cattani, and S. V. Sinchilo, “Cubic nonlinearity in elastic materials: theoretical prediction andcomputer modelling of new wave effects,” Mathematical and Computer Modelling of Dynamical Systems, 10, No. 11,
84–100 (2003).
84. J. J. Rushchitsky and C. Cattani, “Shortened and evolution equations of interaction of plane cubically nonlinear elastic
waves,” Int. Appl. Mech., 40 (2004) (in print).
85. J. J. Rushchitsky, C. Cattani, and S. V. Sinchilo, “Comparative analysis of evolution of the elastic harmonic wave profile
induced by the second and third harmonics,” Int. Appl. Mech., 40 (2004) (in print).
86. J. J. Rushchitsky and I. N. Khotenko, “Cubically nonlinear waves in piezoelastic materials,” Int. Appl. Mech., 40 (2004)
(in print).
87. J. J. Rushchitsky, C. Cattani, and E. V. Terletska, “Evolution of a solitary wave in a microstructural
material—experience of applying the wavelet analysis,” Int. Appl. Mech., 40 (2004) (in print).
88. J. J. Rushchitsky, I. N. Khotenko, E. V. Savel’eva, and S. V. Sinchilo, “Cubically nonlinear waves in piezocomposites—computer simulation of new interaction effects,” Int. Appl. Mech., 40 (2004) (in print).
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