CHALMERS UNIVERSITY OF TECHNOLOGY DEPARTMENT OF NAVAL ARCHITECTURE
AND MARINE ENGINEERING
GOTHENBURG - SWEDEN
HYDRODYNAMIC FORCES AND MOMENTS FOR
HEAVING SWAYING AND ROLLING CYLINDERS
ON WATER OF FINITE DEPTH.
by
CHEUNG H. KIM
DIVISION OF SHIP HYDROMECHANICS REPORT NO. 43
Gôteborg, April 1968
CONTENTS
Pae
Abstract
NOmene1ature Introduction Ettén±ón óf poténtials 2HödynamiÔ föröéà àrid moments
...
9 Da ping and. excitrg forces and FórnentsNumerica1 oa1ct1atión and discussIon
..,..
n.Pigu.res
Acknowledgments.
Reférenoes
ABSTRACT
The potentials for forced heaving swaying and rolling cyiirders
on the càlm water surface. of deep vater used by Grim and Tamura
were extendedto
b.àppiiedfor the oòi11tiofi o1aetjn
shallow water by Thorne'smethòd!P-irstly the hydrodynamic forces and moments on oscillating
Lewis cylinders were calculated by Grim's method; secondly the exciting forces and moments on a fixed cylinder in a transverse incident wave system were calculated according to the H.skird newman method; and finally the influencè of the
shallow
watèr effect on the forces were illustraded in tiures and d.iscussedaNOMENCLATURE
a amplitude of oscillation
A wave aplitude ratio
A source intensity in complex number
B beam
C äddes mass coefficient E éxciting force and moment
F force
gravity constant
water depth wave amplitude
half
beam draft ratio or subscript designating heaveLITT
or subscript designating imaginary partIm imaginary part of
I" added moment of inertia
1 moment
arm
added mass M moment n integer N damping coefficient I r subscript designating real part ori/xRe real part of
subscript designating roll
S subscript designating sway or sectional area
t time.
T draft
U velocity amplitude of sway
V velocity amplitude of heave
a phase 1ag
or
leadw
polar cbordinate tan1
(L)or
uliness cylinderdamping parameter wave elevation
2.
deep water wave number (ci, ¡g)
shallow water wave number density of water
veloeity potential stream fu.nction
cirkular frequency
¿giiiar ëlocity amplitude of roll subscript designating infinite depth
5 T)
INTRODUCTION
We consider two problems: (a) the problem of forced oscilla-tions have sway and roll of a cylinder on the calm water sur-face of shallow water and(b) the problem of a fixed cylinder in a transverse incident wave system of shallow wier. Our
problems are. to determine the hydrodynamic forces and moments
on the cylinder in both cases and to determine the influenbe of shallow water efíeòt on the forces and moments. There are
two reports on the first problem b31 Yu - Ursell [5] and Wang [8]
and two reports on the second problem by Haskind
16]
and New-man [7].Firstly the potentials of the forced oscillations on the calm water surface of deep water used by Grim and Tamura [1] [2]
are extended tó those of shallow water by Thorne's method [3]. There are two reports on such extensions [4] [5]
Secondly by making use of the potential of shallow water
oscillation, the hydrodynamic förces and moments are calculated.
Thirdly the exciting fòrces and moments on a fixed cylinder in beam waves are calculated by using the preceding calculations
for force.d oscillations äccording to the Haskind - Newman method. [6] [7]; alternatively the exciting forces and moments can be
calculated by Grim's method [1] [2] and a comparison of the re-sults o,f both methods shows that they are in good agreement.
Finally some calcúlated results are represented in conventional dimensionless forms including the depth parameter as functions of
EXTENSION OF POTENTIALS
First of all we define our rectangular coordinate system O - xy: x - axIs, on the calm water level, is pointing to the
right and y - .xis, in the centerline of the cylinder at rest, is. pointing, downward. In the following discussion the
irrotatio-nal motion of incompressible inviscid fluid and the linearized boundary conditions and linear hydrodynamic pressure are assumed.
To begin with, the potentials for oscillations in deep water
used by the authors [i] and [2] mu.st be reproduced. They are
ge-nerally represented in the following form
rv
+ ioo = U
et
A (p00 '+ 1'floo . . . (i)., where V,U,Q: linear velocity amplitude of heave and sway. and
angular velocity amplitude of roll; A : complex cource 'intensi.''
ties to be dètermiied by the bounda'y condition on the cylinder
surface; cp cp
+ i
CP : partial velocity potential whichsatisf.ie,s the laW.of continuity everywhere in the liquid, the
free surface condition at y o, the condition of rest of water,
at y co and radiation condition at bcH co.
. +
floe flroe ruco: partial stream function.
.The partial potentials are for heave
° -ky.
e -v
oroc + = COS kx. dic - lire ' ces. vx
o k-v
and for sway and roll:
+ lcD'fl]ooooky
± sin ß + e sth kx dk - sin vxr
ok-y
vi
Ue1t
nfcos2n.
y Cos (2n_1)ß 2fl i 2fl-1 r r-3-nr
+ r-2n s:in (2n+)1
+ 2n r21r2'1
where Anh
+ loO"
()
y = w2/g, r y2 =
tan1
(x/y) , andik(x+iy)
the wave source integrai dk expanded by G-rim may
o k-v be seen in [9].
The aböve potentials for infinitely deep water aise extended
to those of limited water depth by making use of Thorne's method
[]
[4]
[5].
We set the complete potential for the osc±llat±onCin shallow water, wbi,eh are to be extended, in the following
form.
)
, Where. the subsöript. h designates the potential for limited depth
of water and cp. = c + 1w mu.st satisfy the following
condi-nh
nrh
Tflihnr ad,
4)
( +Vonh )
, x \Ix2,y = y0 tanh v0i,
ôx
: shallow water number.
Since the pötential cpdoes iot satisfy the bottöm conditiOn 3
it is to. be extended, by introducing an adjusting potential nr aci,, to the corresponding potential oÍ' finite water depth, i.e.
nh =
+.ad) +
'nih'
The adjusting potentaials
nr ad.
fOr
heave and sway and rollare asumed in the
following
forms respectively.' POr' heave:o
for sway and roil:
Pnr ad. =
f[y(k) sinh cy + ô(k) cash k(h_y)] sin kx dk
where h: depth
of
wa.ter;'(k),
(k), y(k), 5(Ïc): un.lrnownoitat .
-4-.
evereywherè in the liquid:,
at y = o;
aty='h;
(k) sinh ky-- i1(k)
cosh k.(h-y)] cos kx dkA n h
'nh +
= oÖPnh
Firstly the unkriknown constants (k.) and (k) are
elimina-ted by satisfying the free surface condition 2) by the
poten-tials dalone. Secondly the unknown constants (k) and.
are determined by fulfilling the bottom condition 3) by the potentials (p
nr
+ p ). T}nis we determine the requirednrad.
adjusting pOtential
nr ad, and the
ötenal
h in he fol1oying f:orws. Namely,for heave:
y sinh_k
- kcbshk
cos icx dic
= o 1E- y cosh ki -
k
sinh ich-ki'l VSIflLI ky-kcosh icy
voosh kh-icsiith ich or a orh = nr ad.. co (p = (2n-1.) o -5-co
(-1)
k2(1_1) (v2-k2
cash k(h-y) dk o V öosh kh - k sinh kh i(k+v)e vsinh. ky-iccosh icy sin kx dic (2n)i
vcosh kh-ksjnh ich
- k cosh k(h-y).
sin kx dk o y cash kh - k sinh ici.
co k (h.--y)
cas kx dk vcosh ich - kinh ich
for sway and röll:
co
p '
=- e
y sinh ky - k cosh icykx dk orad, o k-v
y cash ich - k sixth kh
t 2 coshk(h-y)
/
(2n) o y ÒOS1'i kh - k sinh kìi
sin kx ilc X dic rn' ad.
::zt)-''
.. n-i) (k±v ofor heave:
nrh
= Re['ti Res(v0)]
and for sway and roll:
nrh
=Im [7cl Res(v0)]
By limitting process, the residues of the function
F(k)e1
at k = y0
i.e. Res
(v0) are calculated and thus the
asymp-totic expressions for X± are
for heave:
- 2it
coh2
y h
.0
cosh y (h-y)
. O
sin y
2v .h + smb 2v h
cosh 'j
ho... -o o
n
2c cosh2v h
cosh y (h_y)
y
2(-tanh2y h,)
° 9 -Sin v
°2v h+sinh 2v h
cosh y h
'o
o. oJ
orh
-6-(2n-i)1
°Finally the potential
Piih
is determined by satisfri..ng
the radiation condition 4). Before fuÍilhing the con4tion
We rieed the asymptotiò expression of the potential cpflrhfor X--+oo
Por this purpose we consider the äomplex contour integra
of the function of the form
p(k)1
,which may generally
re±esent the potentials
Pnrhin k-complex pihne.
As the
eon-tour we take the quadrant Re(k)>o
,I(k)>o
Which pases
over the singular point k=v0 (v>o),v
being the only positive
root of the equation y cosh v0h - y
sinh. y h = o.
Taking the radius of the quadrant
infinitely large and the identation
radius infinitely small, we find
for sway and roll:
2itoosh2v h cash v(h-y)
(p -s ' o . cos V lxi
orh . - 0
2v h + sjnh 2v h cosh y h
o o o
2it cosh2v h cosh y (h-y)
cp +
v2cth2v h1)
0 065 V lxnrh
-
(2n)j2v h+sjnh 2v h Cc)sh y h °
o o o
We now return to the radiation condition 4) and substitute the above potentials in the condition and thus obtain the
potential
h1
the following foms,for heave:
oih
=
-and. for sway and roll:
27c coshv h cash y (h-y)
y
. . 0.0
sinvjxt oih -+02v h
+ sinh 2v hcoshv h
o o o27t cosh h cosh y (h-y)
= -
v21+l(tanh2v h.i) 0 Osj v!
Tnih + O . O
2v h+sinh 2v h cash y h
7..
27t cosh2vh cosh v0(h-y)
vh+sjnh2vh
coshvh
o. . o o
cas vc
" i\
2fl 2 cosh2v h co.h y (h-y)
nih - '- I. y (1-tanh y
h)-'--. O 0.
cas y
(2n-1)i
°
2v h+sinh 2v h cosh y ho o o
-8-, where
corresponds to x±
The extension is now conp1ete. The two sets oÍ' the equations (6) and 11) and (8) and (12) are the extended potentials p for heave and sway or roll respectively. Since the adjusting potential p ) are obtained, in
theform..öf..Qauchy-nr ad.
rLr ad.
integral, they are expanded in series to be used for numerical
The condition of
zero relative normal véióoity to be
satis-fied on the cylindeÌ surface
for heave sway and xoIl
my be
wr.tten ii the following form
X
=- ow
HYDRODYNÀMIC FORCES AND MOMENTS
where. the stream
ftntiônsEAflnh
tion. This condition determines the unknown source intensities
and conseuentiy the velocity potential
h
desigiiated in
advance in theequation(4).
Having obtained the velocity
potential
,one. may integrate
r
i
the hydrodynamic pressure
distributioñ Re
rp-J
on the
sub-Lät
i
merd cylinder surface and determine
the hydrodynamic forces
and moments:
vetkicai forces
in heaving
horizontal forces in swaying.
and rolling
longitudinal moments in swaying
and rolling
J
_v_
clx -T,Qfre[
E A f
h dy]sin wt +
u; 2 n=o Sxdx+ydy
cos wt
'(13)
depend on the mode Of
mo-dx
dy Ç dx+ydy 7]cos wt
Re.,31WtA
1y
00 -nh
-lo-where the constants A depend on each tode of motion. The förces (moment) consist of' inertial and damping part, both of which are in phase with the ¿cceleratiòn and velocity Of' öscillation.
They are called respectively hydrodynamic inertial fo'ces
(mo-ents) and hydrodynamic damping forces (mom(mo-ents).
From the inèrtial and damping forces (moments) we define the added mass and added moment of Inertia and damping force (moment) coefficient and they are represented in dimensionless forms.
In case of sway and roll, it is necessary, in addition to the above, to define added moment arm and damping moment arm, which
relate the moment and force of inertial an.d damping part
respec-tively. For our convenience the above mentioned may be
-11-heave sway roll
inertial force
Rr
damping force FHI .
inertial mment Me..,
M
__
Ri added massm}= r
Hr m,, Sr = added moment of inertia . I -damping force coefficient NH = N = -damping moment coefficient . . MRI 'R = addèd mass coefficient 0SpT
CHpB
adde:mom:of
inertia .coeffjcjen-. . .. . c R T4 damping ferceparmeer
o- ptB2
pwT2
damping moment parameter . . RpwT4
added moment arm
-i
Sr_
MSr 1Rr
MHr
T
- Fc'..
T T - Tdamping moment arm M
Ps±T
1
T T F5.T
, where B: beam T: draft.
It is customary to represent the damping force and moment
coefficients N11, N
and NR
by wave amplitade ratios AH,s and
.where
-12-DA1VJPING AND EXCITIN PORCESÂNID MOMENS
The aymptotic expressions of the velocity potentials for heave sway and roll are easily obtained by
combiniig the equations (9) and (ii) and. (i0) arid (12). They are, omitting the subscript h,
for heave:
00 cosh y (h-y)
iVE
°ei(_wt)
X4+co fl=o
'
cash y ho H.
(_1)fl
v (i - tanh2v0h.)fl ri (2n-1).for Sa3r and roll.:
,: eos.h v(h-y) H --
cosh vh
H'=v
2iEcoshv h -o o o___. 2v h + sirth 2v h o o i 2fl (tanh2v h -(2n) ° o o ± : corresponds to X-?+oosource 1.ntensïtios, depending on sway and roll.
(15) + E
flo
2it cosh2y h , where o 2v h-i-sinh 2v h0
o + wt) (16)The gei.erated wavès by the oscillations progressing at far
dstänOe from the body r = -
fi
at y = o are obtained from the. above asymptotic expressions in complex number, i.e.for heave:
= - vaFI
flEO
A HeH?
wt) fOr sway and roll:.(17') i v.a 00 E A
fin
IF n=o 00 = ;iva/B/2
E A HAH
/B/2 13-+ wt)xI+ wt)
whoro depend on the mcde o motion.
, where a : linear amplitude of heave and sway, B
: correspond to
x.-Consequently the wave amplitude 'atios for } 'r qwav and roll
are written in the following form.
00
=.v EAH
n n00
-14-Ii addition, bt equating the mean power dissipated by the damping force in the forced oscillation and the mean power used in forming the progressive wave system in both positive and negative direc-tion of x- axis, we obtain the reladirec-tion between damping coeffi-cient N and wave amplitude rtio A in the following form:
Ti
2(13
Next we consider the vertical and horizontal exciting forces and longitudinal exciting moment on a fixed cylinder in a trans-verse incident Wave system. Haskind's theory [6] sta
dthat
the exciting forces and moments depend only on the asymptotic
behaviöur of the potential for forced oscillations of the body
with unit veloCity amplitude.. Newman[7] extended tI'e theory and further established the formula:e relating between exciting
forces änd moments and wave amplitude ratios in two dim.ensirinal case. The exc±ting force (moment) in our case is represented by
the following óontour integral [7],
, where : potential of transverse wave system
p : asymptotic potential of unit velocity amplitude.
We take two incident waves o± the ollöwing form, each of which
is oncoming from the positive and negative end of x-axis;
pg +
2vh
o(1g)
wv
sinh2vh
h
- cosh
y (h-y)
e- o
CP
-cosh vh
Each asymptotic potential p is obtained from the potentials
and by taking unit velocity amplitude (seo eq. (15),(lG)),:
Substituting the above defined potentials in the equation (20)
and executing the integral we obtain the heave exciting and
sway exciting forces. EH , E5 and roll exciting moment ER:
JJ
pgv0ST
T : draft. -15-r' -V 1+ ° ) smb 2v h o O 00 + i E A H'- n=onn
where ± correspond to the waves which are oncoming from the
positive and negative end of x - àxis A : depend on the moae
of motion. Making use of the relation
y = y
tanh and the formula of the wave amplitude ratios [eq. (18)1 we obtaii themagnitude of E in conventional dimensionless forms:
IEHÌ AH (J )
pgB
v0B smb 2v0h lES=(1+
2vh
°
)pgv0S
vS
smb 2v0ri (21 )(23)
.,
where S : submerged section area; H : half beam draft ratio;EH IJs --iwt = pghe E A H n n 00
+ i E A H'
-y h + sinh 2v h o o(22)
2 cosh2v h-1
6-The phase diffcr-ence. bctween th ct,ng forces (momonts)
and both oncoming waves from right and left are obtained by comparing the phase angles of thewave elevations
Re[_. pie1t1
with those of exciting forces (moments) Re [EH,ES,E1, j.
They are for heave always
H,
while for sway and rolland R±
, wheres co
= arg( E A H ), = arg(E A H').
(25)
n=o
It should be noted that the minus sign of phase difference. means
the phase lag and vice versa. The wave force on a fixed cylinder consists of vertical and horizontal component and the former con-tributes to the heave exciting, while the latter does to bOth sway and roll exciting at the same instant. Thus the identity
a0 is valid and therefore we need to calculate heave and
sway exciting force together with the roll exciting moment arm
nh
(a,b,G)
= b0 (
-
G)and in odd sine series for sway and roll:
4
nh
(a,b,@) =
E csin (2m.-1)e
-17-NUMERICAL CALCULATION AND DISCUSSION
By the transformation x-4-iy = e-ae©+be'
the stream ftinlctions in the boundary condition [the equation (13)]
are represented as finitions of three variables
,a and b. The
functions are expanded in finite trigonometric series on the
cylinder contour, namely in even sine series for heave:
4,
E b
sin2m8
nia
The boùndary conditions are thus reduced to 10 and 8 simultaneous
-
linear equation systems respectively, from which the source
in-tensities are determined.
The adjusting potentials or stream functions are given in
in-finite trigonometric series (Appendix) and in our calculation the
first 9 terms were taken. In the numerical integration of the
sin-gular functions G(h) andF251(vh)the.limits were takeii at
and 30 and the increment of (2p) was o.5 (see Pig. 2). The
cal-culated forces and moments were represented as the functions of
dimensionless frequency in Figures. The numerical calculations
were carried out by the computer IBM 360 at Chalmers University.
Our discussion will be primarily concerned with the influence
of finite depth effect upon the hydrodynaniic behaviours of forces
-18-WAVE LENGTH: To begin with we consider the lengths of the waves generated by the oscillations on the surface of limited Water depth. The formula for shallow water wave number v= tanh y h
o o
reveals that at low frequency rango 'the relation y>y is valid. This explains that at the sathe frequency of oscillation the generatd wave length of shallow water is shorter than that
of deep water.. It s'höud be noted that the approximate relation is valid at
voo
SOURCE INTENSITIES: In our discussion we are obliged to depend on the calculated source strengths. Por vanishing frequency
v-o
it is needed for us to consider only the significant source in-tensity A. From Fig. 3 we see that firstly at y the nondimen-sionài source intensities for heave A 7/B and A .,t/B approachtoor
unit and zero respectively for any depth of water; secondly in the vicinity of
vo
the intensity A0r/B for finite depth becomes higher than that of infinite depth as the depth decreases, whilefor finite depth decreases first and then increases as y increases. Although Fig 3 hows the calculated result of a
oir-oflar cylinder, the above statements are valid for any form of
cylinder. As to the swaying oscillation it is known from seve-rai calculations that the intensities A0 for finite depth are generally higher than those of infinite depth when
ADDED MASS COEFICIENTS: One may obtain the approximate formula of the added mass coeff±cient for heavthg oscillation of 'a
oir-iar. cylinder in the following form
+ 92S+1 (vh)
h=h h-oo v-o
o
2L_i
h-oo 0'H h=h h4od + 1ÇT\2 2'h1 -19-- 0.577From the above formulae we see that the influence of shallow water effect on the behaviour of added mass coefficients at
may be explained by the behaviour of the singtlar func-tion G251 (vh) See Fig. 4, 5, 6, 7 in connection with 2. It is stated that CH for finite depth is higher than that of infinite depth of water at v-o and tl4s is valid fOr
any form of cylinder. For a moment we observe the addes mass
coeffic.ent at high frequency. Pig. 5 and 7 illustrate the
added mass coefficients C at wide frequency range. We se.e
frOm them that at high frequency the values o± CH for finite
depth are generally higher than those of deep water and from.
Pig. 5 that the values of CH tend to approach the known values
of CH for v->o by Havelock
tu]
i.e.Fig, 7 also illustrates the tendency of CH at very high frequen-cy range, which, seems reasonable. Now we come to the discussion
on the added mass coefficient C in swaying oscillation. For
infinite depth.of water at v-e-o the exact formula. of C is
(1 - a)2 + 3b2
(i - a + b)2
This value is also obtaiied numeridally by applying the potential of infinite water depth at the vanishing frequency i.e.
-
4m Ash-boo B
and for sway:
2 2 or oi. v.-o li =(;; h=h VB
2'
-20-Por the finite depth of water at , on the other hand,
the velocity poteiltial is approximately written by
A[ si:
13G251(vh)
s=1
r sin
I
and since the source intensity Aor for finite water depth is in general relatively higher than that of infinite depthand since we see the behaviour of the singular function
at v-o (see Pig. 2), we come to the conclusion that for
finite depth is higher than
tha.t
of infinite depth whenv-o
(see Fig. 8) and the behaviour of C in the vicinity of is caused by the contribution of the singular function
G25+1
(vh)1
WAVE AIVifLITUDE RATIO: The influence of the shallow Water effect
on the WaVe amplitude ratio Ä11 and
at vo
may be easilydiscussed by observing the asymptotic formula for y o ,
namely for heave:
(vB
v-.o
=l/or
A0 V -.O (VB '2The slope of the curves A. aiad at the origin are
respec--i
hh
tively 2 and , the value of Which is infinitely large
(Pig, 1). It Is obvious therefore that the amplitude ratio for shallow water is higher than that of deep water at y. (Pig. 10,
ii, 12). Further it is stated that theamplitude ratio for Challow water is higher
than
that of deep water at the whóleÌ-I ) ;
-21-frequency range (Pig. ii). This is due to the cont-ribution of
the higher order potentials to forming the progressive wave
system [eq. (18)]
As to the amplitude ratio for sway it is easily observed from. the above formula that at vo A is a 2nd order
para-h
bola with zero slope ,while is a s±raight line with finite
hh
positive slope and tIs both curves must cross each other
(Pig. 13, 14). It should be. noted that the coefficients for roll and must have similar characters to those of sway,
for both oscillations are essen±ially similar from the point of view of antisymmetry about the y - axis. (Fig. 9, 14).
ADDED MOMENT AND DA]VIPING MMENT ARM: The added moment arms 'Sr i
and Rr for shallow water are generally shorter than those T
of deep water at v-o but at the other low frequency range in the vicinity of v-o the Opposite phenomena appear (Fig. 15, 16). The damping rnoment arms l l and the exciting moment arm
T T
coincide with each other and decrease as the depth of water
decreases (Pig. 17).
EXCITING FORCES: In the preceding section the discussion was confined to the Haskind - Newman method. According to Grim's
method, we can also easily calculate. the exciting forces and
moments. By applying the latter method the.same calculations were carried out and both results were compared. It was found that they were in good agreement. In this report the results by the Haskind - Newman method were representd in Pig. 18, 19 and 20. It is obvious from the wave amplitude ratios
H Fig.
14) that the- heave éxciting forces of shallow water are
generally higher than those of deep water. Similary the expia-natiön o± the behaviöur pf the sway exciting force may be
ob-tained from the behaviour of the wave amplitude ratio for sway
-22-MINIMUM DTH: To
find the mininum allowable depth parameter for which our solution converges the calculation bas een. carried oi.t for several widely varying forms of cylinders.From the comparison of the results it was conclued that:
or deep draft cylinders the minimu parameters e very low0
For shallow draft cylinders the values of minimum parameter
are relatively high.
The influence of fullness coefficient on the minimum
allow-able depth is also signifïcent when the shallow draft
cylin-ders are considered.
The minithum parameters for sway and roll are lower than those of heave.
CONCLUSION: In general the influence of shállow water effect on the hydrodynamic forces and moments are remarkable. The curve of added mass coefficient C(CH, C, CR) for finite depth gener1-ly örosses the curve of C for infinite depthtwLce añdthus:the
two crossing points divide the frequency range into three parts. The values of are first higher and then lôwer and higher
again than those of Ch at the ist and 2nd and 3rd frequency range respectively. As to the wave damping or wave amplitude
ratio Ä, is generally highe:r than at whole frequency
hzho.. -. 1'ioo
-range1while (As or ÄR is higher and hen lower than (A5 or A,) =h
CHALMERS
TEKNISKA HOGSKOLA
Shallow water wave number y0
as
functïon of frequency y and
depth b
I
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I
VA
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k!.
-ru
dVA
r.
vbv0h.tanh.
V11 IPig.
i'CTE-SR
Report 43
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0.4
0.0
C HA LM ER s
Ovesof the
inguiar. integrai
TEKN5KA GSKOLA
G21 (vii)
15
I
O 5 GO5
1.5
2.0
o0 0) E
'AA
CHALME RS
TEKNISKA HOGSKOLA Ào11.0
0.9
008
0.7
0.6
005
094
0. 3
0,.2
0910.0
0.0
0,2
Source intensities for Heave
0.4
or
0.6
0.8.
.41.0
Fig. 3
OTFI-SH
Report 43
H=1
= 0.785
1.2
h
= 1.5
o C3A4e
C H AtM E R
Added Miss Coefficient. for Heave
0.0
0.0
0.4
0.6
0.8
1,0
E1.
p0.755
1,2 I 41epo143
TEKNtSKA HGSKOLAP3 M A
Ij_
-ar1
I-Ij
CHALMERS
TEKNISKA HOGSKOIA p.- tJrse].1
= pH=1
= 0.785
h
- 1.5
2,0
4.0
lo
2 B.1,6
1.4
1.2
1.0
0.8
0.6
0.4
0.2
0.0
0.0.
1,0
2.0
340
40
5.0
60
Pig5_-CTHSH
Report 43
Added Mass Ooeficient Íor Heave
PiA
CHALMERS
TEKNISKA HOGSKOLA
Added
ass Coefficient for Heave
1.75
ri=i
CHALMERS
TEKNtSKA H$GSKÓLA
Added Mass Coefficient for:, Heave
H=1
p= i
Pig. 7
0TH-SN
Report 43
0.0
- '10.0
1.0
2.0
3,0
4.0
r5.0
*4
CHALMERS
TEKNISKA .HOGSKOLA
,.
50.0
0.2
Ade
MaseCoefficient for Sway
0.4
0.6
0.8
1.0
K=1
i1.2
Pig.8
CTE - SE
Report 43
yB
Added Moment of Inertia for.. Rbll
CHALME RS
TEKNISKA HCGSKOLA
0.3
Ursell
theory
CHALME RS
TEKNSKA HOGSKOLAFig0 10
CTR Sii
Report 43
H=1
= 0.785
JCHALMERS
TEKNISKA HOGSKOLA
Wave Amplitude Ratio Íor Heave
1.0
0.8
0.6
0,4
0.2
.0
0,0
1.0
2.0
B=1
p0.785
Yu - Ursefl
I.
= 2.0
'1 .510.0
9
vB
3.0
4.0
5.0
6.0
CHALMERS
CHALMERS
TEKNSKA HOSKOLA2.0
4.0
6.0
Pig.. 13
CTE-SH
TEKNISKA HDGSKOLA
CHALMERS
Wave Amplitude Ratio for R11
0.0
0.2
0.4
0.6
0.8
1.0
1.2
Fig. 14
CTH - SU
Report 43
C HALME R
TEKNISKA HOGSKOLA
Added Moment Arm for Sway
0.8
1.0
1.2
Pig, 15
CTH- SR
Report 43
CHALME RS
TEKNISKA HDGSKOtA
Added Moment Arm
Or Roll
H=1
= i
Pig. 16
0TH
-Report 4
.. . . . R R i . I i i0.0.
0..2
0.4
0.6
0.8
1.0
1.2
CHALME RS
TEKNISKA HOGSKOLA 203A4'Si
1Ri
'E
Tr
0,35
4.Q
0.30
0.25
0.20
0. 10
0.0
0.2
Damp ihg Moment Arm l'or Sway and
Roll and Exciting Moment Arm
= ,10.0.,6.0
2.0
1.5
I I-O4
0.6
0.8
1.0
1.2
Fig. 17
CTII-SH
j
Resort 43
C.H A 1M E RS
TEKNISKA HOGSKOLA90
80
70
1 .Ç:::l5.
60
.2
50
40 0.2
3:
20 0.1.
He
Exciting Force Coefficient
Pig. 18
Report 43
Oj0,
. .I i
j
iCHALME RS
TEKNISKA HOGSKOLAIfiL
pgB
1,0
Q.90.8
0.7
0.6
go
50 O4
70
60 0.3
50
40 0.2
30
20 04
100 0.0
0,5
HeaiExcitin Porce Coefficient
= 1 .75
11=1
Pig, 19
0TH SN
0.0
0.4.
0.6
0.8
1.0
1.2
1.4
Rort 4.3
CHALMERS
TEKNISKA HOGSKOLA
lEsi
p g y0
S s
Sway Exciting
PoTheCoefficient
H=1
i
Pig. 20
CTHSH
Report 43
ACKNO1NIEDGEMENT S
The author expresses sincerely his gradlt'u.de to the head
f the institute, Prof. Palkerno, who has supported this work,
Aböve ¿il, thê author is deeply indebted to
G'im
furnihing his inpublished computer progt'am for heave and pitch
of ships in regular waves and also Prof. porter, Whö allowed
eto copt the work of u and Ursell from his own library and
wil-lingly hiped me by
ending the rescent report on a heave theory
of a sphere in shallow water by Dr. Wang.
This'work has been financially supported
y
Swêdib.
REFERENCES
[i]. Grim, 0.: "Eine Methöde für eine genauere Berechnung
der Tauch.- und Stamph-bewegungen in glattem Wasser." H.S.V.A. Bericht No. 1217, 1960.
[21.
Tamura, K.: "The öalculation of hydrodynamical forces and moments acting on the two dimensional body:- according to the Grim's theory -." Jour. SZK, No. 26, Sept.
1963.
-Thöre, R,C.: "Multiple expansions in theory of surface
waves." Proc. Camb. Philos. Soc. 69,
1953.
Porter, W.R,: "Pressure Distributions, Added Mass, and Damping CoeffIcient for Crlinders Oscillating in a Free Surface." Report 8216, Inst. Eng. Res., University of
CalifOrnia, 1960.
Yu, Y.S. and Ursell, F.: "Surface waves generated by an
oscillating circular cylinder on water of finite depth: theory and experiment". J. Fluid Mech. 11 (1961), 529-551.
Haskind, MiD.:" The exciting forces and wetting of ships
in waves." DTME Translation
307
by J.N. Newrnan Nov. 1962.Newman, J.N.: "The exciting foròes on fixed bodies in
[8]. Wang, S.: "The hydrodynamic forces and pressure
distributions for a oscillating sphere in a fluid of 'irite depth0t' Dissertation, M.14. Çambridge, June 1
966.
Kim, C.H.: "Uber den Einfluss njcht linearer Ef ekte auf hydrodynamische Kräfte bei erzwungenen
Tauch-bewegangen prismatischer Krper.' Shiffstecbiìik 73. Heft, Sept.
1967.
[io Wehausen, J.V.: "Surface Wàves." Handbuch der Physik,, Band IX, Springer Verlag 1960.
[ii]. Havelock, T.H..: "Ship Vibrations the Virttal Inertia of' a Spheroid in Shallow Water." INA, Jan, 1953.
Haskind, M.D0: "Wayes arising from osc-illation of bodies in shallow water", SNAME T.R,B. No..
1961.
Appenlix
1. Adjusting potentials and. stream functions, for heve.
G (vh)
-vE
2S+1 2S+1 br ad. - s=Ç2s+1) h2S S1fl(2s1)-.2(s+1)+1
r22
sin (2s-i-2).
(-i
)fl
i
'2fl+2S-1 (vh) 2S2s+
d..(2n-i)Ls=o(2z»
.1 r25 Cos (2s+1)p, T2n-1)L"s=o(2s+1)t h2fl+2S î, = ______i
2fl+2S-1 (vh) 25+1nr ad, (21)t s=o(2s+1) h2fl+2S
r
sin (2s-i-1) +(_1)h1
i
(2n-F)Ls=o(2s+2), sin (2z2)j3.L
¶ad. so(T
G 2S+ (V h) r2S cos 2s -i G251(vh) 2S+1 Cos (2s+1).2. Adjusting potentials and stream functions for sway and roll.
G (v'h) = V E 25+3
r22sin (2s+2)
+ or ad.(2s+2)L h22
G .(vh) +So
(2+1)Vh22:
r2S+t sin (2s+1)ß. r ad. ad. 4,nr
adG251 (y)
P2S+1 = = EG251
(vh) (2s)L h2:8 G(vb)
+80
E .28 3(2s+i)
h2Sl2 ?n) r2S.cos?s.+
28+1 r (vb 2fl+28+1 (2s-i-2)Lh2+2S+2
(vh) i 2X1+25+1 4(2n)1 °(2s+1)L h2hl+2S+2 ø P (vh) V2n+2S-1
= .(2ñJT 80 (2z}1 'b228 e S+1.(ii)(v.
Oosh u-u
slnhu
ju11
y coshu-usjnhu
cos (2s+1)3, sin (.2s+2) + sin (2s+1). cos 2s + F.. + E 2X1+28+1 .. 8+1Ç2n).
So(2+1yh2n+2s+2
i,2cos (2s+U.
du
The epansion of the :ábove. Caucy integrals for numerical calculations are obtained from the reference [