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PHY 808 Dissertation
PART 1
Integral Equations
PART 2
Geophysical Problem
By Group N;
GIWA KUNLE WASIU (BIOPHYSICS)
AGBOEBA THANKGOD (GEOPHYSICS)
PALMER THEOPHILUS EZE (GEOPHYSICS)
UBOGWU FELIX (THEORETICAL PHYSICS)
Course Lecturer: Professor John, Idiodi
July, 2013
PART 1:
STATEMENT OF THE PROBLEM: This problem is to discuss integral equations and their
application to physical problems, outlining the various techniques for solving them as
treated in [1] and [2].
INTEGRAL EQUATIONS
INTRODUCTION
Integral equations are equations in which an unknown function appears under an
integral sign. An integral equation is called fredholm equation if the range of integration is
fixed. This arises from boundary value problems of elliptic partial differential equation.
b
adyyfyxkxgxF , (1a)
where yxk , is called the kernel, f(y) is unknown function. Integral equation with
unbounded range of integration, which arises from the initial value problem for hyperbolic
partial differential equation is called the voltera integral equation.
x
adyyfyxkxgxF , (1b)
There are several methods, available for solving integral equations. The series
solution method was applied to non-homogenous voltera quantum, and also, the Adomian
decomposition method was applied to integral equation with cauchy kernel [1].
SERIES SOLUTION OF INTEGRAL EQUATION
For a non-homogenous voltera integral equation of the second kind of the form
x
adttUtxkxfxU ., (2)
The function (U(x) is expressed as a power series
k
k
u
xaxU
0
(3)
Also the Taylor expansion of f(x) and k(x,t) is obtained to get a solution for equation
(2). On substituting the power series for U(x), U(t) and the Taylor series expansion of f(x) and
k(x,t) coefficient 0, kak are determined. Having determined the co-efficient, the solution to
(2) is obtained in a power series form.
Series solution of singular integral equations
1.1 Solve the integral equation
dttuutxtUx
0 (4)
Solution
Put 5
5
4
4
3
3
2
2
1
1
0
0
0
xaxaxaxaxaxaxaxUk
k
k
3
3
2
2
1
1
0
0
0
xaxaxaxaxatUk
k
k
equation (4) becomes
0
00 k
k
k
x
k
k
k dtxaxExxa
0
00
1
00 k
k
k
x
k
k
k
x
k
k
k dttaxdttaxxa
xx
k
k
k dttatataaxdttatatataxxa0
3
3
2
2100
4
3
3
2
2
10
0
xx
tatatatax
tatatatax
0
4
3
3
2
2
10
0
5
3
4
2
3
1
2
0
4325432
4325432
4
3
3
2
2
10
5
3
4
2
3
1
2
0 tatatatax
tatatatax
5334223112
0
0
4534232x
aax
aax
aaxa
ax
201262
5
3
4
2
3
1
2
05
5
4
4
3
3
2
2
1
1
0
0
xaxaxaxaxxaxaxaxaxaxa
Equating co-efficient of similar power of x.
!3
1
6
1
6,0
2,1,0 1
3
0
210 a
aa
aaa
!5
1
120
1
6
1
20
1
20,,0
12
3
52
4
a
aa
a
5
5
4
4
3
3
2
210 xaxaxaxaxaaxU
!5
5
!3
3 xxxxU
In closed form [2],
xxU sin
0
12
!12
1
m
mm
m
xxU .
1.2 Solve the integral equation.
dttUetxexxU txx
x
0
sincos (5)
4
4
3
3
2
210
0
tatatataataxUputk
k
k
also in series form;
!6!4!2
1642 xxx
xCos
!7!5!3
753 xxxxxSin
!3!2
132 xx
xe x
!3!21
32 ttte t
equating (5) becomes
!7!5!3!3!21
!6!4!21
75332642
0
xxxxx
xxx
xxxxa
k
k
k
dttatataatt
txxx
xx
3
3
3
210
32
0
632
!3!21
!6!3!21
!7!5!3!3!21
!6!4!21
75332642 xxxxx
xxx
xxxxU
dttatatatatatata
tatatatatatataaxx
x
i
x
!3!3!3!3!2!2!2
!3!21
6
3
5
2
43
0
4
2
3
1
2
0
4
3
3
2
2
10
3
3
3
2100
32
!7!5!3!3!21
!6!4!21
75332642 xxxxx
xxx
xxxxU
dttaa
aa
ta
aataaaxx
xx
30133
20
120100
32
!3!2
!2!3!21
!7!5!3!3!21
!6!4!21
75332642 xxxxx
xxx
xxxxU
x
taaaa
ta
aataa
taxx
x
0
4
0123
30
12
201
0
32
4!3!2
!22!3!21
!7!5!3!3!21
!6!4!21
75332642 xxxxx
xxx
xxxxU
4!3!2
3!22!3!21
4
0123
3
0
12
2
010
32
taaaa
taaa
xaaxa
xxx
!3!3!3!2!2!5!3!5!3!4!21
653642
5342 xxxxxx
xxx
xxxU
4!3!23!22
4
0123
3
0
12
2
010
taaaa
taaa
xaaxa
643!222
6
0
4
01
4
0
12
3
0
3
01
2
0
uataa
taaa
xaxaaxa
4012300
2
201
0
342
224261246
2
23!4!21
aaaaaaa
xaa
xax
xxxx
xU
40123
3011201
0
24
1
2426124
3
1
6
21
2
1
211
xaaaa
xaaa
xaa
xaxU
40133
311201
0
24
126
6
tan22
2
311
xaaaa
xaa
xaa
xaxU
Comparing co-efficient
0111,1 00 aaa
12
2
2
310
2
301
2
aa
a
2
1
6
3
6
122
6
32 012
3
aaaa
8
1
24
11023
24
126 0123
4
aaaa
a
821
432
4
4
3
3
2
210
xxxxU
tatataxaaxU
In closed form,
1 xexU
2.0 Adoption of the method for singular integral equation
Considering,
1
1dt
xt
tUxxU
Put
0i
ii tTaxU
where tTi is the Chebyshev polynomial of the first kind.
1
10
xdtxt
tTaxU
k
ii
for 3,2,1,0i
xdtxt
tTatTatTatTaxU
3322111001
1
N.B: The Chebyshev equation 01 22 yuyxyx has solutions, the
Chebyshev polynomial, xTn given by a Rodrigues’s formular [3],
2
12
1
22
1!2
1!2
n
n
nn
n xdx
d
n
xnxT
For
2
12
1
02
0
020
0 1!0
1!02:0
x
dx
dxxTn
111 2
1
2
122
0 xxxT
For 2
12
1
1221
1 1!2
1!12:1
x
dx
dxxTn
xxxxx
2
12
1
2
1
222
122
1
2
1!112
For 23
2
2
222
2 1!4
1!22:2
2
1
xdx
dxxTn
2
1
2
122 12
2
31
3
1xx
dx
dx
2
1
2
122
12 122
1131
3
1xxxxx
1.21 222
2 xxxxT
For n = 3
25
2
3
323
3 1!6
1!3.2 2
1
xdx
dxxT
2
32
2
22 12
2
51
15
12
1
xxdx
dx
2
1
2
122
322 12
2
3.11
3
1xxxx
dx
dx
2
1
2
1
2
1222
1222 12
2
1..123212.
2
31
3
1xxxxxxx
2
1
2
1
2
12322
122 11211 xxxxxxx
322
3 121 xxxxxT
333 22 xxxxx
xxxT 34 3
3
tttTttTttTtT 34,12,,1 3
3
2
210
Hence,
xdtxt
dttta
xt
dtta
xt
dtta
xt
dtaxU
IIII
4321
1
1
3
31
1
2
21
1
11
1
0 3412
for
11
1
10
0 ln
xtadtxt
a
x
xaxxaI n
1
11ln1ln01
for
1
1
11
1
1
11
12
xt
dtxadtadt
xt
taI by partial fraction
111
1
112 ln xtxattaI
xxxaa 1ln1ln11 11
x
xxaaI
1
1ln,2 12
for
dtxt
axt
dtta
xt
dttaa
1
12
1
1
2
21
1
2
22
12122
dtxt
axt
dtxdtxta
1
12
1
1
21
12
1.2
x
xaxtxxt
ta n
1
1lnln
22
1
1
2
1
1
2
2
x
xa
x
xxxxa n
1
1ln
1
1ln
2
1
2
12 2
2
x
xa
x
xxaxaI n
1
1ln
1
1ln24 2
223
for
dtxt
sttaI
31
134
4
dtxt
ta
xt
dtxdtxtxta
1
13
1
1
31
1
22
3 34
x
xxha
x
xxtx
tta
1
123
1
1ln
334 3
3
1
1
223
3
x
xxaa
x
xaxx
xx
xa
1
1ln36
1
1ln4
23
1
23
14 333
322
3
x
xxaa
x
xaxxaI
1
1ln36
1
1ln42
3
24 333
32
34
x
xxaa
x
xaxxa
aI
1
1ln36
1
1ln48
3
8333
32
33
4
x
xxaxa
x
xxaa
x
xaxU
1
1ln24
1
1ln2
1
1ln 2
22110
xx
xxaa
x
xaxxa
a
x
xa
1
1ln36
1
1ln48
3
8
1
1ln 233
32
33
2
N.B:
1 1
12
22
1
1ln
n n
nx
x
x
from
5432
5
1
4
1
3
1
2
11ln xxxxxx
5432
5
1
4
1
3
1
2
11ln xxxxxx
532
5
2
3
22
1
1ln
5323 xx
xxxxx
x
xTaxTaxTaxTaxU 33221100
xaxaaxaxaaxU 3
3
32
2
210 342
532342
53
03
3
32
2
210
xxxaxaxaaxaxaa
5344
8322
532
22
53
11
xxxxaxa
xxxxaa
5388
5
8
532
533
3
2
33
53
2
xxxxaxaxa
xxxa
xxx
xxaa
5366
53
33
Equating the co-efficient of x
for 03
862: 33120
0 aaaaax (i)
for 12423: 22031
1 aaaaax
1362 3210 aaaa (ii)
for 06822: 3312
2 aaaax
01422 311 aaa (iii)
for 03
24
3
24: 2
2
0
3
3 a
aa
ax
043
10
3
23
20 aaa
(iv)
for 0683
2: 33
14 aaa
x
023
23
1 aa
(v)
133
1aa
178
1,
178
10,
178
56,
178
33201
aaaa
xxxx
xTaxU nn
n
34178
112
178
10
178
3
178
56 32
0
178
3
178
4
178
10
178
20
178
3
178
56 32 xxxxxU
3232
4.20666178
1
178
4
178
20
178
6
178
66xxx
xxxxU
APPLICATION OF THE DECOMPOSITION METHOD TO THE SOLUTION OF INTEGRAL
EQUATION WITH CAUCHY KERNEL
The application of Adomain decomposition method to integral equations
gives solutions in form of rapidly convergent power series with elegantly
computable terms. The power series so developed yields either exact solution
in a closed form or accurate approximate solutions by considering a truncated
number of terms for real life problems [4].
The main approach of the method is demonstrated as follows
considering the voltera integral equation of the form.
1,0,,0
tdssutsktgtUt
(6)
where tg the non homogenous part is sufficiently smooth to guarantee the
existence of unique solution 1,0tfortu . In the operator from equation (6)
tuLtgtU (7)
with the operator L defined as dssutsktuLt
,0 (8)
Representing tuL in (7) by the decomposition series
0n
n tUtU (9)
Putting this into (7)
00 n
n
n
n tULtgtU (10)
The components tUofUUUU n210 ,, in (9) are defined in a recurrent
manner using the algorithm.
01
0
ktuLtU
tgtU
K
(11)
with the recurrent equation, then.
t
t
dssutsktuLtU
dssutsktuLtU
tgtU
0112
0001
0
)(,
)(, (12)
The components nUUU 10 , are thus readily computed and hence tU of
(6) follows immediately in the series form using (9). In real life, (9) is usually
evaluated as truncated series and few term of the series yield results with
high accuracy [1].
APPLICATION OF ADOMIAN DECOMPOSITION METHOD TO INTEGRAL
EQUATION WITH CAUCHY KERNEL
dssusti
tgtUt
11
0 (13)
where ttg 21
Applying the decomposition method.
ttgtUo 21
dsst
s
idssu
sttU
t
21110
01
Using the transformation
dtdstts cossin2sin 2
0,0 s
2, ts
dtt
t
iU cossin2.
sin1
sin21220
1
2
dti
tU sin.sin21
2 2
01
dtdi
U22
001
2
2cos12sin
2
2
2
001
2
2sincos
2
t
i
tU
i
t
i
tct
i
tU
2
21
21
Also dssUst
U 12
1
dsst
i
s
i
s
iU
t
0
2
2
1
Using the above transformation
22
0
2
022cos
sincossin21sincos2.
cos
sin2
t
dtdt
t
tU
22
0
3
0
2
2sinsin
46
d
td
22
0
3
0
2
2 3
coscos
2
sin2
t
3
42
ttU
tUtUtUtUtU n
k
n
210
0
3
4221
tt
i
t
i
tt
NON LINEAR INTEGRAL EQUATION WITH CAUCHY KERNEL
dssust
tgtU nt
0
(14)
where T is a constant and n is an integer 2 . In operator from equation (14)
tuLtgtU n (15)
where the operator L is defined by
dssust
tuL nt
n
0
(16)
The non-linear term in equation (14) is equated to the polynomial series as
tAtU n
n
n
0
where the An’s are the so called Adomian polynomial. The frame work for
generating the polynomial [5] is defined as;
03
0
33
102
0
2
210
0
33
02
0
22
10
0
22
0
0
11
00
!3
!2
ufdu
duuf
du
duuuf
du
duA
ufdu
duuf
du
duA
ufdu
duA
ufA
(17)
where nuuf
substituting tUtU n
n
n
0
into equation
tALtgtUtU n
n
n
n 00
The component of tU are defined in recurrent manner by
01 nALU nn
Hence, dssAst
ALtUt
00
01
dssAst
ALtUt
10
12
Therefore the solution of equation (14) follows immediately by summing
the sUn` .
Application to non-linear integral equation
Considering,
dssUsti
tttUt
2
0
23
21 11
34
Defining An polynomial, 2uuf
2
12002
0
22
10
0
22
100
0
11
2
000
2!2
2
uuuufdu
duuf
du
duA
uuufdu
duA
uufA
3223
21
2
09
16
3
86
34 tttttU
322
09
16
3
8ssssU
st
dssss
itU
t
32
01
916
38
1
Using the transformation, 2sints
dttds sincos2
for 2
,0,0 tsands
2
3422
01
sin
sincos2.sin9
16sin
3
8sin
1 2
tt
dtttt
itU
cos
sincos2.sin9
16sin
3
8sin
1
3422
0
2
t
dtttt
i
dttti
t
73523
0sin
9
16sin
3
8sin
2 2
2 22
0 0
735
0
23 sin9
16sin
3
8sin
2
dttttti
ttU
N.B: Using the reduction formula
dIdI n
n
n
n
2
2 sin,sin
2
1 1sincos
n
n
n InnI
1
0
2
03 2sincos
3
1sin
22
IdI n
3
2cos
3
2sin2
3
122
003
dI n
15
8
3
2
5
44
5
135
II
35
16
15
8
7
66
7
157
II
Hence,
35
16
9
16
15
8
3
8
3
22 32 ttti
ttU
27
25
23
315
512
45
128
3
411 ttt
itU
tUtU n
k
n
n
0
where k is smaller for very accurate results.
tUtUtU 10
termnoise
ttti
tt 27
25
23
23
21
315512
45128
341
34
tU is approximately [6] is equal to
21
ttU
Conclusively, it can be observed that solution to any integral equation can be obtained if an
informed choice is made of the appropriate method to apply. The Fredholm-type integral
equations, the power series methods guarantee elegant and exact solution while in the case
of Voltera- integral equations, the best method which will give a speedy computable solution
can be by using the Chebyshev polynomial or the Adomian decomposition method; if the
kernel is of the Cauchy type. This work would provide great insight and serves as eye opener
to anyone working on integral equations.
REFERENCES
[1] Aihie V.U (2009), Application of the decomposition method to the solution of integral
equation with cauchy Kernel, Journal of the Nigerian Association of Mathematical
Physics, Vol. 14, pp 41-44.
[2] Aihie V.U (2009), Series solution of singular integral equations, Journal of the
Nigerian Association of Mathematical Physics, Vol. 14, pp 45-48.
[3] Fox L. and Parker I.B. (1968), Chebyshev Polynomials in Numerical
Analysis, Oxford University press, London, pp 46. [4] Adomian G (1988), A review of the decomposition method in applied Mathematics(
Journal of Mathematical analysis and application,Vol 2 pp 115,501,544)
[5] Adomina G (1994), Solving frontier problems of physics, the decomposition method,
Kluwer academic, Boston.
[6] Adomian G. and Reach .R (1992), Noise terms in decomposition solution series
computer Mathematics pp 11,24,61.
PART2: GEOPHYSICAL PROBLEM
STATEMENT OF PROBLEM:
To deduce the application and correlation of Bessel functions to the potential
and resistivity obtained by vertical electrical sounding of n-layered earth. To
show that the derived potentials and resistivity using mathematical analysis
correlates with the experimental results obtained by the Egbai (2002), Asokia
et al (2001) as well as Asokia et al (2002).
1.0 INTRODUCTION
This is a dissertation to derive the potential, resistivity transform and
apparent resistivity of a stratified earth as used in the published papers of
Egbai (2002), Asokia et al (2001) and Asokhia et al (2002). To start with, it is
necessary to explain resistivity.
Electrical resistivity also called specific electrical resistance is the repulsion of
a current within a circuit. It explains the relationship between voltage
(amount of electrical pressure) and ampere (amount of electrical current). The
resistance R of a wire with a constant width can be calculated from resistivity
formular given as
(1.1)
where is the length of the conductor, measured in meters [m], A is the cross-
sectional area of the conductor measured in square meters [m²], and ρ (rho) is
the electrical resistivity (also called specific electrical resistance) of the
material, measured in ohm-meters (Ω m).
From Ohm’s law,
(1.2)
Where
= Potential difference across sample (V )
= Electric current through the sample (A)
Equating equations (1.1) and (1.2), we obtain
· (1.3)
From (1.3) above, we obtain
(1.4)
Where;
E = Electric field (V/m)
j = Current density (A/m2)
σ = conductivity (S)
2.0 THE POINT SOURCE ON A STRATIFIED EARTH.
Fig. 2.1 Layering strata and notations
In order to derive the potential due to a point source over a horizontally
layered strata, Koefoed et al (1979), made the following assumptions.
1. The subsurface consists of a finite number of layers with finite thickness
and the deepest layer extended to infinity; the layers are separated from each
other by horizontal boundary planes.
2. Each of the layers is electrically homogenous as well as electrically
isotropic.
3. The field is generated by a current source that is located at the surface of
the earth.
4. The current emitted by the source is direct current.
From the potential field theory, the electric field E, is the negative gradient of
the potential V and is given as
(2.1)
Taking the divergence of (1.4), we obtain
(2.2)
The substitution of (2.1) into (2.2) yields
(2.3)
From the third assumption, the divergence of the current density j is zero
except at the surface or the uppermost layer. Hence, equation (2.3) has the
form
(2.4)
Where δ(x) is called dirac delta function. Its value is zero for all x except at the
point of the current source.
In (2.4), we have used
Equation (2.4) is an in-homogenous differential equation of the second order.
For source free media, the Dirac delta function δ(x) = 0 and (2.4) becomes
(2.5)
Equation (2.5) is a well known Laplace equation. Equation (2.5) in cylindrical
co-ordinates become
(2.6)
In equation (2.6), we assumed that the potential distribution is uniform and
symmetrical about the z-axis through the source and is independent of the
angle θ (Keller et all, 1966).
The solution to equation (2.6) is obtained by the method of separation of
variables resulting in two second ordinary differential equation. Stefanesco et
al (1930), derived the potential due to a point source of current I at a point (r,
z) on the surface of a stratified earth as
(2.7)
Where An(λ) and Bn(λ) are functions of λ and J0(λr) is the Bessel function of
order - zero of the first kind.
To prove (2.7), we substitute
V (r, z) = R(r)Z(z) into (2.6) to get
(2.8)
Divide through by RZ to obtain
(2.9)
we have
(2.10)
Therefore from (2.9), we have
(2.11)
Where λ2 is separation constant.
Re-arranging (2.10), we obtain
(2.12)
and
(2.13)
We obtain the solution for for (2.12) as
(2.14)
To solve (2.13), we let
so that
(a)
(b)
(c)
By substituting (a) and (c) into (2.13), we get
(2.15)
By comparing (2.15) with the standard Bessel equation of order ν
(2.16)
We observe that (2.15) is the well-known Bessel equation of order zero with λ
= μ. Thus, if we set λ = μ in (2.15) and ν = 0 in (2.16), the result is the same.
Equation (2.15) becomes
(2.17)
We note that when Bessel’s equation is encountered in physical situations, x
is usually some multiple of a radial distance (x = μr) and so take values in the
range 0 ≤ x ≤ ∞.
We often require that the solution to (2.17) be solved by Frobenius series
method since at x = 0, it gives a singularity. Let
(2.18)
Substituting (2.18) into (2.17), we obtain
Divide through by xc−2 to get
(2.19)
If we set x = 0, and demand that the terms in the summation varnish with n ≥
0, we obtain the indicial equation.
c2 = 0 ∴ c = 0 (double value)
From (2.19), we have
To obtain the recurrence relation, we shift the index of the second summation
so that
(2.20)
Since indicial roots c are equal, we shall obtain only one solution in the form a
Frobenius series.
Substitute c = 0 into (2.19) to get
By setting a0 = 1, a1 = 0, we may then calculate a2, a4, a6, . ..
∴ Solution to (2.17) becomes
with a0 = 1 we obtain
(2.21)
The solution given in (2.21) agree well with the solution of (2.14) with ν = 0. i.e
So we write equation (2.21) in close form
(2.22)
By combining (2.16) and (2.22), we obtain the solution to equation (2.6). In
differential form, we have that
As △ λ approaches the limit △ λ → 0 we get
Since Vn(r, z) is measured at the surface where external current source exists,
we have
Hence,
Note that this is equation (2.7) earlier noted.
Also, in (2.22) we replaced μ = λ since it is an arbitrary constant.
Using an integral from the theory of Bessel’s functions known as the Lipschitz
integral defined as
=
we obtain
(2.23)
Substitute (2.23) into (2.7) to obtain
(2.24)
At the base, there is no external source current and therefore, the potential
integral is not required. We must also reject terms like eλz as the potential
must remain finite when z → ∞.
Potential at base (Substratum)
(2.25)
The following boundary conditions are used to determine the functions
An(λ),Bn(λ)
and Cn(λ).
1.
2. At each of the boundary planes in the subsurface, the electrical potential
must be continuous i.e.
3. At each boundary planes in the subsurface
Applying boundary condition (1) to (2.7), we get
(2.26)
Using boundary condition (2) and equating (2.24) to (2.25), we obtain
(2.27)
Using the boundary condition (3), we get
(i)
(ii)
Equating (i) and (ii), we obtain
(2.28)
From equating (2.26) we have
By substituting into (2.27), we get
(2.29)
Also we make the substitution of (2.26) into (2.28) to obtain
(2.30)
From equations (2.29) and (2.30), we obtain
(2.31)
We set
, so
Thus,
(2.32)
From (2.26), we have
Where Kn is called the reflection coefficient.
We substitute An (λ) and Bn(λ) into (2.7) at z = 0 to obtain
(2.33)
Where θn (λ) is called the kernel function.
θn (λ) is a function of the thickness and reflection coefficients for an assumed
earth model and is given by
by using the property of Bessel’s function
(2.34)
We obtained the formula for the apparent resistivity. Differentiating (2.33)
with respect to r gives:
Using (2.34) and factoring out , we get
(2.35)
The LHS of (2.35) is called the Schlumberger apparent resistivity (ρa)
(2.36)
J1(λ) is the Bessel function of order-one where
BESSEL'S FUNCTIONS UNDER THE STUDY
The method of separation of variable was applied to the Laplace’s equation of
(2.6) in cylindrical coordinate. The resulting Bessel equation of order zero was
obtained in (2.15). This zero-order Bessel function of the first kind arises from
the application of Frobenius series method to equation (2.15) (Stroud, 2003).
The first-order Bessel function of the first kind J1(λr) also arises from the
derivative of the apparent resistivity.
The graph of the Bessel’s function under the study is shown in the Fig. 2
Fig. 2: The graph of Bessel functions J0(x) and J1(x)
The zero-order Bessel function of the first kind J0(x) arises from the
application of separation of variable to Laplace’s equation in cylindrical
coordinates which gives the solution for the potential at the surface of n-layer
earth.
The first-order Bessel function of the first kind J1 (x) arises from the
computation of the apparent resistivity. The table of the Bessel function under
the study has been obtained from mathematical tables as shown below;
Table 1: Table of values for the Bessel function
[Source; Stroud (2003), p.311 ]
z J0(X) J1(X)
0 1 0
0.1 0.9975 0.0499
0.2 0.99 0.0995
0.3 0.9776 0.1483
0.4 0.9604 0.196
0.5 0.9385 0.2423
0.6 0.912 0.2867
0.7 0.8812 0.329
0.8 0.8463 0.3688
0.9 0.8075 0.4059
1 0.7652 0.4401
1.1 0.7196 0.4709
1.2 0.6711 0.4983
1.3 0.6201 0.522
1.4 0.5669 0.5419
1.5 0.5118 0.5579
1.6 0.4554 0.5699
1.7 0.398 0.5778
1.8 0.34 0.5815
1.9 0.2818 0.5812
2 0.2239 0.5767
2.1 0.1666 0.5683
2.2 0.1104 0.556
2.3 0.0555 0.5399
2.4 0.0025 0.5202
2.5 -0.0484 0.4971
2.6 -0.0968 0.4708
2.7 -0.1424 0.4416
2.8 -0.185 0.4097
2.9 -0.2243 0.3754
3 -0.2601 0.3391
3.1 -0.2921 0.3009
3.2 -0.3202 0.2613
3.3 -0.3443 0.2207
3.4 -0.3643 0.1792
3.5 -0.3801 0.1374
3.6 -0.3918 0.0955
3.7 -0.3992 0.0538
3.8 -0.4026 0.0128
3.9 -0.4018 -0.0272
4 -0.3971 -0.066
4.1 -0.3887 -0.1033
4.2 -0.3766 -0.1386
4.3 -0.361 -0.1719
4.4 -0.3423 -0.2028
4.5 -0.3205 -0.2311
4.6 -0.2961 -0.2566
4.7 -0.2693 -0.2791
4.8 -0.2404 -0.2985
4.9 -0.2097 -0.3147
5 -0.1776 -0.3276
AN INVERSE PROBLEM IN DIFFERENTIAL EQUATIONS
BY R. E. LANGER
1. Introduction.
The differential equation as a tool requires no introduction to either the
mathematician or the applied scientist. Problems in endless variety are
continually solved through this medium, the process almost invariably
beginning with an epitome of the problem's essential characteristics in the
form of a differential equation, which is thus determined explicitly both as to
its structure and its coefficients, and proceeding
thence to a deduction of the form or properties of a suitable solving function.The
present note is devoted to a problem in which this customary order of events is in
large measure reversed. The formulation
of the problem yields in this case the structural form of a differential equation, and
beyond this the existence of a solution which satisfies certain specified conditions.
From these data the determination of the equation itself, that is, of its coefficient
function, is required and constitutes the solution of the problem.
2. The Physical Problem.
In the investigation of shallow geological structures, and in the study of the
electrical resistivity of the earth's crust at depths below the surface, an
appropriate experimental procedure centers around the supply of a direct electric
current through a small electrode to the surface of the earth. The electrical
potentials which result at the surface of the earth are measurable at all distances
from the electrode, and
constitute entirely the immediately obtainable data. From them it is desired to
compute, if possible, the conductivity of the earth below as a function of the depth.
With the idealizations involved in regarding the conductivity as a differentiable point
function depending upon the depth alone, and in taking the ground as a horizontally
uniform in-finite half-space, the problem may be formulated in the following way. Let
x, the depth, and ρ, the horizontal distance from the electrode, be taken as
cylindrical coordinates with origin at the electrode. The electrical potential ø(ρ, x)
may be shown then to satisfy the differential equation
in which (x) denotes the earth's conductivity. The substitution
separates the variables and resolves the equation into the components
The first of these is a Bessel equation, and, since the potential is to remain finite and
vanish at infinity like the reciprocal of the distance, it must be concluded that
The second component equation is of the Sturm-Liouville type, and since (x)
is positive, its solutions are of exponential form. Let 1{x, λ) denote a solution which
is positive, and, as a function of x, monotonically decreasing. The condition that
vanish everywhere at the surface except at the electrode leads by familiar
reasoning to the formula
the surface potentials are accordingly given by
a relation which by the Fourier-Bessel integral theorem may be inverted into the
form
The formulas thus derived reveal the significant fact that the functions Ω(λ) and ø(ρ,
0) are each uniquely determined by the other, and hence that the information
embodied in the surface potential data is completely embraced in the function Ω(λ)
when the latter is given for . It is to be shown how from these data the
conductivity function may (x) be computed.
3. The Mathematical Problem.
The considerations sketched in brief above may be looked upon as having
crystallized the physical problem into the following somewhat idealized
mathematical one.
On some interval a certain function (x) is known to be analytic and
positive. Beyond this it is known that the differential equation.
possesses a solution 1{x, λ) which has the properties:
(i) that for λ on the range (0, ∞ ) and x on the interval (0, h) the relations
are satisfied; while
(ii) at x = 0, the boundary condition
is fulfilled, Ω(λ) being a function which is compatible with the preceding hypothesis,
and which is known and given for . The function (x) is to be computed.
A process for the desired computation may be deduced as follows.
Let the equation (1) be written in the form
It is then readily seen to possess a fundamental set of solutions which are
represented asymptotically (as to λ ) by a pair of expressions
In which
Hence the solution which satisfies the condition (3), and includes a suitable factor
independent of x, is representable by a formula
Now unless the first term on the right of this expression is dominant for all values of
x on (0, h), the one or the other of the conditions (2) will inevitably be violated when λ
is sufficiently
large. It follows, therefore, that
a form which on substitution into the condition (3) is found to impose upon the
function Ω(λ) a condition of compatibility to the effect that it admit of a
representation
Since by hypothesis the function Ω(λ) is given, the infinite set of constants , (n =
l, 2, 3, • • • ), is to be considered as known.
Let the function be defined by the formula
It is then found on the one hand in virtue of (la) to satisfy the
Riccati equation
and on the other hand, in virtue of (3), (4) and (5), to be asymptotically representable
in a form
the coefficients vn (x) being analytic on (0, h), and satisfying the boundary relations
A relation
then follows, the coefficients being related to those of the series (8) by the recurrence
formulas*
If the equation (7) is now written in the form
and the series (8) and (8a) are formally substituted in it, it is found as a result that
The function (x), however, does not depend upon . λ Hence it
must be concluded that
And
Of the equations (12) the first p in number when taken together constitutes a linear
algebraic system for the unknowns . The system has a
determinant of value unity
and on solution yields the formulas.
These formulas may be materially simplified as follows. The iteration of the formula
(10) yields the relations.
from which it may be seen that if to the last column in the determinant (13) there is
added the combination.
the effect is formally to replace the elements by zeros and in the
case of the last row to replace by In precisely the same way it will
be seen upon reference to the formulas (10), that if to the first column in (13)
there is added the combination
the formal effect is to replace the elements by zeros, and in the case
of the last row to replace . Similar reductions of the remaining
columns may likewise be made, the formula (13) being reduced in consequence to
the form
If in this, finally, there is added to the last row the combination
the determinant disintegrates into the formulas
In which
Let the functions f1, f2, f3...., be defined successively by the recurrence formula
Then it is readily seen that the repeated differentiation of the first of formulas (14),
and substitution from the remaining formulas, gives the expression
For the derivatives of the functions v1(x)
For general values of x the functions involved in the right member of (17) are
not known. They are given, however for x=0 by (9), whence
With these values available the MacLaurin expansion of the function v1{x) is
computable, and since the first of the formulas (10) gives to (11) the form
the desired computation of the function (x) has been accomplished.
CONCLUSION
By series of mathematical methods and analysis we have been able to
achieve the potential at the surface of the two layered earth at the distanced r
from the current source (I).
Also the kernel function which is a function of the thickness and
reflection coefficient was obtained for the assumed earth model.
The Bessel zero- order function of the first kind and first order of
the first kind arose from the calculation for an n- layered earth with
apparent resistivity and arbitrary thickness considered.
In conclusion we obtained the tables for the Bessel function under focus
and then plotted an elegant figure to show the proper behavior of the function
for the n-layer earth surface. The derived potential and resistivity correlates
with studies carried out by Asokhia et al (2001). Finally, the resistivity
transformation function T(x) obtained, properly agrees with the works of
Langer et al (1993) as also stated by Gosh D.P (1971).
REFERENCES
Asokhia M.B and Ujuanbi O. (2001), J. Nig. Ass. Math. Phys. Vol. 5, 79-88.
Asokhia M. B, S.O. Azi and O. Ujuanbi O. (2002), J. Nig. Ass. Math. Phys.
Vol. 4, 269-280.
Egbai J.C. (2002), J. Nig. Ass. Math. Phys. Vol 6, 207-222
Ghosh. D. P. (1971), The application of Linear Filter Theory to the Direct
Interpolation of Geo-electrical Resistivity Sounding measurement, Geophysical
Prospecting (Netherlands) V. 19, no 2, 192-217
Stroud K.A (2003), Advanced Engineering Maths, 4th Ed., palgrave
macmillian, New York, 305-311
Keller G. V. and Friscknecht F. C. (1966), Electrical Methods in
Geophysical Prospecting, Pergamon Press, 90-196 and 299-353
Koefoed O. and Dirks F.J. (1979), Determination of resistivity sounding
filters by the Wiener-Hopf least squares method, Geophysical Prospecting
Vol.27, 245-250.
Stefanesco S., Schlumberger C. and Schlumberger M. (1930), Sur la
distribution electrique potentielle autour d’une prise de terre ponctuelle dans
un terrain a couches horizontals, homogenes et isotopes. J. de physique et le
padium, series 7, Vol. 1, 132-140.