356 Lectures on Dynamics of Stochastic Systems
plays here the role of time), i.e., its solution satisfies the relationship
δu(x, R)
δε(x
0
, R
0
)
= 0 for x
0
< 0, x
0
> x. (13.3)
The variational derivative at x
0
→ x − 0 can be obtained according to the standard
procedure,
δu(x, R)
δε(x − 0, R
0
)
=
ik
2
δ
R − R
0
u(x, R). (13.4)
Consider now the statistical description of the wavefield. We will assume that ran-
dom field ε(x, R) is the homogeneous and isotropic Gaussian field with the parameters
h
ε(x, R)
i
= 0, B
ε
(x −x
0
, R − R
0
) =
ε(x, R)ε(x
0
, R
0
)
.
As was noted, field u(x, R) depends functionally only on preceding values of field
ε(x, R). Nevertheless, statistically, field u(x, R) can depend on subsequent values
ε(x
1
, R) for x
1
> x due to nonzero correlation between values ε(x
0
, R
0
) for x
0
< x and
values ε(ξ, R) for ξ > x. It is clear that correlation of field u(x, R) with subsequent val-
ues ε(x
0
, R
0
) is appreciable only if x
0
− x ∼ l
k
, where l
k
is the longitudinal correlation
radius of field ε(x, R). At the same time, the characteristic correlation radius of field
u(x, R) in the longitudinal direction is estimated approximately as x (see, e.g., [33,34]).
Therefore, the problem under consideration has small parameter l
k
/x, and we can use
it to construct an approximate solution.
In the first approximation, we can set l
k
/x → 0. In this case, field values u(ξ
i
, R)
for ξ
i
< x will be independent of field values ε(η
j
, R) for η
j
> x not only functionally,
but also statistically. This is equivalent to approximating the correlation function of
field ε(x, R) by the delta function of longitudinal coordinate, i.e., to the replacement
of the correlation function B
ε
(x, R) whose three-dimensional spectral function is
8
ε
(q
1
, q) =
1
(
2π
)
3
∞
Z
−∞
dx
Z
dR B
ε
(x, R)e
−iq
1
x−iqR
(13.5)
with the effective function B
eff
ε
(x, R),
B
ε
(x, R) = B
eff
ε
(x, R) = δ(x)A(R), A(R) =
∞
Z
−∞
dxB
ε
(x, R) (13.6)
Using this approximation, we derive the equations for moment functions
M
mn
(x;R
1
, . . . , R
m
;R
0
1
, . . . , R
0
n
) =
*
m
Y
p=1
n
Y
q=1
u
x;R
p
u
∗
x;R
0
q
+
. (13.7)
In the case of m =n, these functions are usually called the coherence functions of
order 2n.