International Journal
on Marine Navigation
and Safety of Sea Transportation
Volume 4
Number 4
December 2010
415
1 INTRODUCTION
The intensification of shipping gave rise to compli-
cation of navigating conditions at sea roots and in
recent years over 75% of navigation accidents oc-
curred in restricted waters and bounded waterways.
The growth of merchant ship dimensions during the
last decades led to the situation in which vast regions
of oceans and seas become comparatively shallow.
The wrecks of modern large vessels getting
stranded or collided are accompanied by serious
economical losses and negative ecological conse-
quences.
The estimation of ship motion characteristics in
restricted waterways is necessary not only for elimi-
nating the possibilities or minimizing the number of
accidents, but for substantiation of sea routes dimen-
sions in the proximity of ports as well.
Modern theoretical and experimental hydrody-
namics provides us with a great amount of infor-
mation for predicting seakeeping qualities of ships in
open deep sea. On the contrary such an information
for a vessel sailing in shallow water is comparatively
poor and the proper methods are not widely devel-
oped. Such a situation may be explained by virtue of
the additional difficulties arising in the theoretical
investigation of the potential boundary value prob-
lems for a ship propagating in shallow water condi-
tions. First of all the complicacy of the singularities
method is ten times higher for shallow water poten-
tial problems in comparison with the unbounded sea
ones. Then the strip method widely used in practical
calculations is inconsistent with the physical reality
and often causes insoluble problems when using in
shallow water cases with clearly expressed three di-
mensional water flow phenomena.
Thus a new approach for investigating ship hy-
drodynamic problems free from difficulties of clas-
sical method of singularities and shortcomings of
strip method is vital. Such approach is demonstrated
in this paper.
2 BOUNDARY VALUE PROBLEM FOR
VELOCITY POTENTIAL
If the water around a ship is considered as inviscid
incompressible fluid the important hydrodynamic in-
formation is derived from the solutions of boundary
value problems for the velocity potential. Founded
on basic physical principles the nonlinear problems
with apriori unknown boundaries are simplified by
linearization and the solutions of corresponding lin-
ear problems are practically used. Consider a vessel
floating with a zero forward speed in shallow water
with the depth
H
under the action of regular waves
ti
вв
er
σ
ζ
=
,
в
r
and
σ
being wave amplitude and cir-
cular frequency accordingly.
The longitudinal
x
and transverse
y
axes of the
Cartesian coordinate system are taken on the free
surface of water and the vertical axe
z
is pointed
downward.
The potential function
can be divided
into cosine
ñ
Φ
and sine
s
Φ
parts
( ) ( ) ( )
[ ]
tisc
ezyxizyxtzyx
σ
,,,,Re,,, ΦΦ=Φ
(1)
Asymptotic Theory of Ship Motions in Regular
Waves Under Shallow Water Conditions
Y.L. Vorobyov
Marine Engineering Bureau, Ukraine
M.S. Stasenko
Odessa National Maritime University, Odessa, Ukraine
ABSTRACT: The hydrodynamic theory of ship motions in shallow water under the action of regular waves is
discussed. The boundary value problem for velocity potential is solved using the matched asymptotic expan-
sion method (MAEM). The solution is based on Fourier Michell integral transformation technique and char-
acteristics of Helmholtz and Klein Gordon equations. Using the obtained results formulae for hydrodynamic
characteristics are derived. The application of these formulae demonstrated good coincidence of the results of
calculations and model experiments carried out in towing tank of Odessa National Maritime University.
416
It is systematically demonstrated in investigations
of Y.L. Vorobyov (Vorobyov, 2002), that estimation
of added inertia, damping, coupling coefficients and
exciting forces can be done using asymptotic values
of radiation potential. So we can avoid the necessity
of treating the wave scattering problem and difficul-
ties of integration in the hull proximity.
Consider the ship performing longitudinal har-
monic oscillations with circular frequency
σ
. The
potential functions
( )
zyx
sñ
j
,,
,
Φ
,
5,3,1=j
must satis-
fy the following differential systems
( ) ( )
;,,,0,,
0
,
2
2
2
2
2
2
Ezyxzyx
zyx
sc
j
=Φ
+
+
(2)
( ) ( )
0
,
2
,,00,, Σ=Φ
+
yxyx
gz
sc
j
σ
; (3)
( ) ( ) ( )
;,,,,,,
,
Szyxzxuzyx
n
j
sc
j
=±Φ
(4)
( ) ( )
<<=Φ
yxHyx
z
sc
j
,,0,,
,
. (5)
If the ship is performing transverse harmonic os-
cillation with circular frequency
σ
, the potential
functions
( )
zyx
sc
j
,,
,
Φ
,
6,2=j
must satisfy the dif-
ferential systems (2), (3), (5) and hull conditions
( ) ( )
( )
( )
.,,
,0,,,,,,
Szyx
zyx
n
zxvzyx
n
s
jj
c
j
=±Φ
±=±Φ
(6)
Both systems must satisfy radiation conditions in
the infinity.
If the velocity of oscillations is taken to be unity,
( )
zxu
j
,
and
( )
zxv
j
,
are for longitudinal oscillations
5,3,1=j
( ) ( ) ( ) ( )
( ) ( ) ( )
,,cos,cos,
,,cos,,,cos,
5
31
zNxxNzzxu
zNzxuxNzxu
=
==
(7)
and for transverse oscillations
6,2=j
( ) ( ) ( )
( ) ( )
yNxxNy
zxvyNzxv
,cos,cos
,,,cos,
62
=
==
(8)
Now let us consider ship as slender body, suppos-
ing that
( )
ε
OLB =
,
( )
ε
OLT =
,
TBL ,,
being her
length, beam and draft,
1<<
ε
and the hull varies
slowly along the longitudinal axe. Under this as-
sumption matched asymptotic expansion method
(MAEM) is used for solving the potential problems.
According to MAEM the flow field is divided in-
to two zones: far field zone where
( )
1OLy =
and
near field zone in which
( )
ε
OLy =
. The condition
along the boundary between the zones are not for-
mulated and satisfied in the process of matching the
solutions in far and near fields along the their
boundary.
3 FAR FIELD SOLUTIONS
If the observation point is located in the far field as
0
ε
the hull degenerates into a cut
22 LxL =
δ
of free surface plane
0=z
. The
potential functions
sc
j
,
Φ
are harmonic (2) in the
layer
Hz
0
with ship centerplane
0=y
ex-
cluded, satisfy free surface (3) and radiation condi-
tions. The boundary conditions on the centerplane
0±=y
, that is on the inner boundary of the outer
zone are not formulated as soon as the hull (with its
centerplane) belongs to inner zone. The only identi-
ties come from the physical considerations
( ) ( )
( )
( )
;5,3,1,0,,,
,,;,,,,
,
,,,
=>+Φ
=
=Φ
+Φ=Φ
jyzyx
y
zyx
y
zyxzyx
sc
j
sc
j
sc
j
sc
j
(9)
( ) ( )
( )
( )
.6,2,0,,,
,,;,,,,
,
,,,
=>+Φ
=
=Φ
+Φ=Φ
jyzyx
y
zyx
y
zyxzyx
sc
j
sc
j
sc
j
sc
j
(10)
In accordance with (9), (10) the boundary condi-
tions on the centerplane
0±=y
are taken in the
form
( ) ( ) ( )
;5,3,1,0,0,;,,0, ==±Φ
±=±Φ
jzx
y
zxfzx
y
s
jj
c
j
(11)
( ) ( ) ( )
6,2,0,0,;,,0, ==±Φ±=±Φ jzxzxgzx
s
jj
c
j
, (12)
where unknown functions
( )
zxf
j
,
and
( )
zxg
j
,
are
taken as known ones for a moment.
Let us find the solution of the outer problem (2),
(3), (11), (12), (5) for cosine amplitude
( )
zyx
c
j
,,Φ
of velocity potential
( )
tzyx
j
,,,Φ
. Using the Fourier
method for the outer differential problem we find the
expansions for
( )
zyx
c
j
,,Φ
( ) ( ) ( ) ( ) ( )
=
+=
Φ
1
0
0
,,,,
m
m
m
jj
c
j
zZyxFzZyxFzyx
; (13)
417
( ) ( ) ( )
( )
( ) ( )
.,,
1
,
;,,
1
,
0
0
0
0
zzZzyx
H
yxF
zzZzyx
H
yxF
m
H
c
j
m
j
H
c
jj
d
d
Φ=
Φ=
(14)
The eigen functions
( )
zZ
0
,
( )
zZ
m
form a com-
plete orthogonal set in
[ ]
H,0
with mean square val-
ue of 1:
( ) ( )
( ) ( ) ( )
( ) ( )
( )
,
2
2sin
1
2
1
;
2
2
1
2
1
;
,
0
0
0
2
1
0
2
1
00
+=Ν
+=Ν×
×Ν=Ν=
H
H
z
H
Hsh
zHzch
zZHzchzZ
m
m
m
m
mm
α
α
α
α
α
α
(15)
where
0
α
= real positive root of the equation
Hth
g
00
2
αα
σ
=
(16)
and
<<<
321
ααα
= subsequence of real positive
roots of the equation
0
2
=+
g
Htg
mm
σ
αα
. (17)
As soon as
( )
zyx
c
j
,,Φ
is harmonic and the eign
function system is orthogonal,
( )
yxF
j
,
0
and
( )
yxF
m
j
,
satisfy the Helmholtz and Klein-Gordon
equations
( )
( )
.0,
,0,
2
2
2
2
2
0
2
0
2
2
2
2
=
+
=
+
+
yxF
yx
yxF
yx
m
jm
j
α
α
(18)
Taking in mind, that for
5,3,1=j
( ) ( )
zxfzx
y
j
c
j
,,0, ±=±Φ
, the boundary conditions
for equations (18) according to (14) are to be taken
in the form
( ) ( )
( ) ( )
,22,
2
1
0,
,
2
1
0,
00
LxLxxF
y
xxF
y
m
j
m
j
jj
±=±
±=±
γ
γ
(19)
where
( ) ( ) ( )
( )
( ) ( )
.,
2
;,
2
0
0
0
0
zzZzxf
H
x
zzZzxf
H
x
m
H
j
m
j
H
jj
d
d
=
=
γ
γ
(20)
According to Green theorem and conditions (19),
(20), after using radiation conditions we find for
5,3,1=j
( )
( ) ( )
( ) ( )
( ) ( )
( ) ( )
,,
1
,
2
1
,,
0
2
2
0
1
0
0
2
2
000
=
Κ
Ν=Φ
H
mj
L
L
m
m
m
H
j
L
L
c
j
ddZfRzZ
H
ddZfRzZ
H
zyx
ζξξζξα
π
ζξζζξα
(21)
( ) ( ) ( ) ( ) ( )
,,
2
1
,,
0
0
2
2
000
=Φ
H
j
L
L
s
j
ddZfRJzZ
H
zyx
ζξζζξα
(22)
where
( )
RJ
00
α
,
( )
R
00
α
Ν
,
( )
R
m
α
0
Κ
=Bessel func-
tions,
( )
2
2
yxR +=
ξ
.
The last formula is based on Green theorem,
equations (18), boundary condition
( )
0,0, ±Φ
zx
y
s
j
and radiation conditions.
Now returning to (18) we find that for
6,2=j
( ) ( )
zxgzx
y
j
c
j
,,0, ±=±Φ
, the boundary condition
for equation (18) must be taken in the form
( ) ( ) ( ) ( )
xxFxxF
m
j
m
jjj
γγ
2
1
0,,
2
1
0,
00
±=±±=±
. (23)
where
( ) ( ) ( )
( )
( ) ( )
.6,2,,
2
;,
2
0
0
0
0
==
=
jzzZzxg
H
x
zzZzxg
H
x
m
H
j
m
j
H
jj
d
d
γ
γ
(24)
Now taking solutions of (18) that satisfy bounda-
ry conditions (23), (24) along the cut
2Lx
after
using radiation conditions we have
( ) ( ) ( )
( ) ( )
( ) ( )
( ) ( )
,,
1
,
2
1
,,
0
2
2
0
1
0
0
2
2
000
=
Κ
Ν
=Φ
H
mj
L
L
m
m
m
H
j
L
L
c
j
ddZgR
y
zZ
H
ddZgR
y
zZ
H
zyx
ζξξζξα
π
ζξζζξα
(25)
418
( ) ( )
( ) ( ) ( )
.6,2,,
2
1
,,
0
0
2
2
00
0
=
×
×=Φ
jddZgRJ
y
zZ
H
zyx
H
j
L
L
s
j
ζξζζξα
(26)
4 NEAR FIELD SOLUTIONS. MATCHING
To study flow phenomena in the near field the trans-
verse coordinates are stretched
εη
y=
,
εζ
z=
and as
0
ε
omitting terms of
( )
2
ε
O
we obtain the
totality of two dimensional boundary value problems
in
constx =
planes for
( )
ζη
,
c
j
Φ
( ) ( ) ( )
( ) ( )
( ) ( ) ( ) ( )
( ) ( ) ( ) ( )
( )
.6,5,3,2,1,;0,
;,;,cos,
;,;,cos,
;
2
1
,;00,
;,,0,
3
2
2
11
2
2
2
2
=<=Φ
=Φ
=Φ
>==Φ
+
=Φ
+
+
+
jh
xLN
N
xLN
N
xb
g
xe
c
j
c
c
c
j
c
j
ηη
ζ
ζηζζη
ζηηζη
η
σ
εκηκ
ζ
ζηζη
ζη
(27)
Here
( )
xe
= a fluid domain in a form of strip
{ }
h<<
ζη
0,
with frame contour
( )
xL
+
excluded,
( )
xb
= the width of this contour.
The problem for
( )
ζη
,
s
j
Φ
is uniform and has a
trivial zero solution. The boundary value problem
(27) has to be discussed keeping in mind that for
matching procedure the asymptotics of solutions
when
η
tends to infinity are needed. These asymp-
totics are found using specially worked out proce-
dure. In addition to harmonic potential
( )
ζη
,
c
j
Φ
let
us introduce the conjugate harmonic stream function
( )
ζη
,
c
j
Ψ
and multi-valued analytical function
( ) ( )
+Φ=+=
ζηηχ
,,
c
jj
iyU
( )
ζη
,
c
j
iΨ+
being de-
termined outside the close contour
( ) ( )
xLxL
+
U
.
Various branches of
( )
χ
j
U
differ one from another
by function
[ ]
( )
( )
=
=
+
=
,5,3,1,
;6,2,
2
000
00
jB
jA
hchshh
hhchch
U
j
λλλ
ζλλ
(28)
where
A
=
( )
ηλλ
00
cos,xP
j
,
B
=
( )
ηλλ
00
sin,xQ
j
,
0
λ
= real positive root of the equation
hth
g
00
2
λλ
σ
ε
=
. (29)
We notice that outer boundaries of inner zone
±∞
η
are at the same time the inner boundaries
of the outer zone
0±=y
. We have from (28) and
(29)
( )
( )
( )
,5,3,1,,
2
1
,0,
000
000
0
=
+
±=± j
HHchshH
HzHchch
xQzxf
jj
ααα
ααα
α
(30)
( )
( )
( )
.6,2,,
2
1
,0,
000
00
0
=
+
=± j
HHchshH
HzHchch
xPzxg
jj
ααα
αα
α
(31)
Functional coefficients
( )
0
,
α
xQ
j
and
( )
0
,
α
xP
j
are determined in the form
( ) ( )
( )
( ) ( ) ( )
[ ]
( )
( )
,sincos
exp4,
0
0
000
2
1
0
0
2
03
dtt
dt
tdZ
tAttstBtA
tZ
g
xQ
xb
+
×
=
+++
αααα
σ
α
(32)
( )
( )
( )
( ) ( ) ( )
[ ]
( )
( )
,cossin
exp4,
0
0
000
2
1
0
0
2
03
dtt
dt
tdZ
tAttstBtA
tZ
g
xP
xb
+
×
=
+++
αααα
σ
α
(33)
where
( )
tA
+
= values of potential function under de-
termination on the contour with the equation
( )
tZz
0
=
and
( )
( )
2
0
1
+=
dt
tdZ
tS
.
As soon as
( )
tA
+
is unknown, it is proposed to
take its approximate value when the frequency of
oscillations tends to infinity. Values of
( )
tB
+
are
values of normal derivative of potential function ac-
cording to the hull boundary conditions. The value
of
( )
tA
+
can be easily found using the standard inte-
gral equation procedure.
For
( )
05
,
α
xf
and
( )
06
,
α
xf
we find
( ) ( ) ( ) ( )
02060305
,,;,,
αααα
xxfxfxxfxf ==
(34)
Inserting (30)-(34) into (21), (22) and (25), (26)
we actually performed matching of solutions in far
and near field zones upon their boundary and get an
approximate solutions for five radiation potentials
uniformally valid in the whole water domain.
5 HYDRODYNAMIC COEFFICIENTS OF SHIP
MOTIONS
It is convenient to find damping and exciting forces
according to Haskind-Newman approaches where
419
asymptotic expansions of radiation potentials are
used. Thus we avoid the necessity of solving the dif-
fraction problem and simplify calculations because
of the simplicity that asymptotics of potential func-
tions have far from ship hull. According to
(Haskind, 1973, Newman, 1961) wave exciting forc-
es and moments acting on a vessel may be calculated
using such expressions
( ) ( ) ( )
[ ]
5,3,1,2
0
==Χ jiFFer
sc
ti
j
ββγβ
σ
. (35)
( )
( )
( )(
)
( )
( )
ξζ
βξα
βξα
ζαα
ζαζξ
β
β
ddHshth
chf
F
F
L
L
H
j
s
c
=
cossin
coscos
,
0
0
00
2
2 0
0
(36)
( ) ( ) ( )
[ ]
6,2,sin
2
1
0
=+=Χ jiFFer
cs
ti
j
βββγβ
σ
. (37)
Functions
( )
β
sc
F
,
are determined by (36), but for
6,2=j
instead of
( )
zxf
j
,
( )
zxg
j
,
is taken. Func-
tions
( )
zx
f
j
,
5,3,1=j
and
( )
zxg
j
,
6,2=j
are giv-
en by (30) - (34).
In expressions (35) - (37)
0
r
- incoming wave
amplitude,
β
- angle between longitudinal axe of
ship hull and vector of wave crests propagation.
The real parts of (35) and (37) must to be taken
into account.
Damping forces and moments are calculated ana-
lyzing the energy flow carried of to infinity from
ship hull by outgoing waves. According to (Haskind,
1973, Newman, 1959) damping coefficients
ij
µ
are
given by formulae
( )
( )
( )( )
( )
( )
.5,3,5,3,,
,
16
000
2
2
2
2
2
3
0
2
3
00
==×
××
×
Ψ
=
jidxdxJQ
xQx
q
j
L
L
L
L
j
i
i
ij
ξξααξ
ξα
αρσα
µ
(38)
2
3
,
2
3 ji
are taken equal to zero for
1== ji
.
( )
( ) ( )( )
( )
( ) ( )
[ ]
,6,2,6,2
,,
,
32
02000
2
2
2
2
4
2
0
4
2
00
==
+×
××
×
Ψ
=
ji
dxdxJxJP
xPx
q
j
L
L
L
L
j
i
i
ij
ξξαξααξ
ξα
αρσα
µ
(39)
where
2=q
if
ji =
, otherwise
1=q
,
( )
Hth
Hch
H
0
0
2
0
0
1
α
α
α
α
+
=Ψ
, functions
( )
0
,
α
xP
i
and
( )
0
,
α
xQ
i
are given by (32) (34),
0
J
and
2
J
are
Bessel functions.
For calculation of inertia forces acting on an os-
cillating vessel potential functions in the near field
must be used. To avoid the difficulties of integration
the source-like functions in the vicinity of ship hull
an alternative method is used. The method is based
on the fact proved in (Landau, Lifshits, 1964), dis-
cussed and used in (Kotic, Mangulis, 1962).
It was demonstrated that added masses and damp-
ing coefficients are proportional to integral sine and
cosine transformations of identical functions. It is
enough to find a couple of transformations
( ) ( )
( ) ( )
dx
x
x
ijij
ijij
+=
0
22
2
σ
µµ
π
λσλ
, (40)
( ) ( )
( ) ( )
[ ]
dxx
x
x
ijij
ijij
=
0
22
2
σ
λλ
π
σ
µσµ
, (41)
where
( )
σλ
ij
,
( )
ij
λ
,
( )
σµ
ij
,
( )
ij
µ
= added mass
and damping coefficients for frequency
σ
and infi-
nite frequency consequently.
Integrals in (40), (41) are introduced us principle
value integrals. It is known that mostly
( )
0
ij
µ
.
The value of
( )
ij
λ
for a ship can easily be calculat-
ed using strip method and solving standard integral
equation in the layer
Hz 0
.
The hydrodynamic characteristics of 200000
DWT tanker (Oortmerssen, 1976) for motions in
shallow water conditions
2.1=
T
H
are demonstrated
in Fig. 1-5. The values calculated using the results of
paper are given by solid lines, while the results of
experiments conducted in towing tank Odessa Na-
tional Maritime University are presented by dots.
The coincidence of theoretical and experimental re-
sults is satisfactory for practical uses.
Coefficients of added mass, exciting forces and
damping are plotted against undimensional frequen-
cy
g
L
σν
=
.
420
Figure 1. Longitudinal exciting forces
Figure 2. Transverse exciting forc-
es
Figure 3. Longitudinal damping
Figure 4. Sway added mass
Figure 5. Transverse damping
6 CONCLUSION
The results derived on the base of MAEM were used
for systematic calculations of hydrodynamic charac-
teristics for a ship floating in regular waves under
shallow water conditions.
The calculated values demonstrated good agree-
ment with the results of model experiments conduct-
ed in towing tank of Odessa National Maritime Uni-
versity.
REFERENCES
Vorobyov, Y.L., 2002. Ship hydrodynamics in restricted waters.
St.P., Shipbuilding, 224 p. (in Russian)
Haskind, M.D., 1973. Hydrodynamic theory of ship motions,
M.Science, 327 p. (in Russian)
Newman, J.N., 1959. The damping and wave resistance of
pitching and heaving ships// Journal of Ship Research.
Vol.3, N1, p.p. 1-19.
Landau, L.D . & Lifshits , E.M., 1964. Theoretical physics, v.5,
Statistical physics, M., Science, 567 p. (in Russian)
Kotic, G. & Mangulis, V. 1962. On the Kramers-Kronig rela-
tions for ship motions// International Shipbuilding Pro-
gress. Vol.9. N97, pp.361-368.
Oortmerssen, G.M, 1976. The motions of a ship in shallow wa-
ter// Ocean Engineering. Vol.3. N4, pp.221-255.
.