ABSTRACT
Qr-i
Wave-induced loads on semisubmersible platforms in
operational and survival conditions are usually
evalu-ated from the Morison equation.
If the pontoons are
unusually large, closely-spaced, or near the
sea
sur-face, then interaction effects that are not included in
the Morison equation approach become significant.
In
the transit condition, when the pontoons are floating
in the sea surface, the wave loads must be calculated
by other methods.
An improved strip theory approach is presented
uti-using "opposed motion potentials't.
Interaction
effec-ts between the pontoons are included.
The present
im-provement provides additional information about the
spatial distribution of tue diffraction forces,
en-abling the determination cf the internal forces
between
the pontoons.
Comparisons are shown between results from the
Morison equation approach, the improved strip theory,
and model tests for a recent semisubmersible design at
operational draught. The improved strip theory is
also compared to 3-D sink-source calculations for the
same rig at transit draught.
NOMENCLATURE
A
added-mass matrix
B
damping matrix
B
breadth between pontoon centerlines
C
restoring coefficient matrix
D
centerline sectional diffraction force
Fexcitation force (equations l-3)
Fcenterline sectional force (figures)
Gdiffraction force on starboard hull
Hdiffraction force on port hull
Hwave height
g
acceleration due to gravity
Jimaginary unit
k
wave number
L
characteristic length of semisubmersible
Mgeneralised inertia matrix
N
unit normal vector (toward vessel surface)
n
components of N
Pdynamic pressure
B
position vector for a point on the vessel surface
S
surface region
t
t i meu
coordinate axes/coordinates of a point
V
volume region
Xmotion amplitude
Oincident wave amplitude
B
heating angle of waves (o degrees = head seas)
flmotion vector
O
diffraction potential
Àwave length
P
density of fluid
O
opposed motion potential
incident wave potential
IMPROVED STRIP THEORY FOR WAVE-INDUCED LOADS ON TWIN HULL SEMISUBMERSIBLES
Subscriots
D
diffraction
I
incident wave
i
direction, il,..
.6corresponds to axes in fig.2
surge,sway, heave, roll, pitch, yaw
s
significant crest-to-trough response in irregular
seas
Conventions. Very many of the quantities discussed in
this paper are harmonic functions involving exp(-jwt).
This function is generally omitted in the text, with
the remaining symbols indicating complex amplitudes
(of the motions, potertials, etc.).
When finally
cal-culating the magnitude of physical quantities, it is
understood that the real part is to be taken.
INTRODUCTIONDuring the last few yesr
there has been a great deal of
activity in the design and construction of
semisubmer-sible platforms for many different types of offshore
duty.
The present generation of semisubmersibles
de-parts to some extent from the archetype of the early
seventies, generally having greater payloads
on deck,
larger pontoons , and different arrangements of columns
or bracings.
The basic twin pontoon concept still
re-mainS very popular.
Some development has also been carried Out on the
theoretical methods and computer programs used as
de-sign tools.
Many of the available methods for the
cal-culation of wave-induced motions and loads on
semisub-mersibles were also initially developed in the early
seventies.
It is necessary to ensure that these
tech-niques can adequately handle the new generation of
rigs, or alternatively develop improved methods.
Thetransit condition is now being paid more attention,
placing somewhat greater requirements on the
calcul-ation methbds.
Existing methods for wave-induced motions and, loads
have mainly been based on a HorizOnS equation approach
(eg. [l-21), or on a strip theory approach t3-51.
3-dimensional sink-source techniques [6-'?j are also
sometimes used, but these generally require
consider-ably more computer resources.
The Morison equation
approach has been very successful for survival and
operational draughts, when experience has shown that
hydrodynamic interaction effects between different
parts of the structure can be neglected with respect
to the motions and overall loads.
The strip theory
approach allows interaction between the pontoons to be
taken into account in the calculation of the motions.
This is useful if the pontoons become very large, are
closely spaced or near the surface.
However, recent
investigations have shown serious shortcomings in the
normal strip theory approach, when internal loads
acting on the structure are required [8-9]
.Results
obtained using an improved strip theory to overcome
TECHNISCHE WIIVERSITEIT
Laborum voor
Scheepehydmmschaa
Archief
Mekelweg 2,2628 CD Deift
-K. Lindbrg
'& 015-786813- Fax 018.781es8
Gotaverken Arendal AB
Gothenburg, Sweden
radiation (rigid body motion) potential
w
circular frequency of encounter
J. Mathisen
Det norske Ventas Hovik. Norway
A. Borrasen
Det norske Ventas
this problem are presented in the following. THEOBY
The theoretical basis for the calculation of
wave-induced motions and loads on semisubmersìbles is well known
and will not be repeated here.
Nef.
[8] providesa
review of the available methods. In this paper, an explanation of the present improvement to the usual strip theory for application to semisubmersibles will be given.The major assumptions applied in the theory are: The structure is treated as a rigid body; i.e. in-ertia forces due to wave-induced motions of the whole structure are included, but inertia forces due to elas-tic deformation of the structure are not included;
Linear
(Airy) wave theory is applied; Cc) Both the incoming waves and theplatform
motion are of small amplitude; (d) The pontoons are long compared to theirbeam,
without abrupt changes in cross-section; (e) The fluid is assumed irrotational, allowing potential flow theory to be applied.The equations of motion for the structure may then he written:
-jut
(A+M) + B + C = e (i)
where A is the added mass matrix, M is the generalised inertia matrix, B is the linear damping matrix, C is the restoring coefficient matrix, including both hydrostatic and linearised anchor line effects, F is the excitation force vector, and r is the body motion vector. The origin of the coordinate system is located in the inter-section of the stillvater and centerline planes, with direction i1 (surge) pointing aft, i=2 (sway) pointing to starboard, and i=3 (heave) pointing upwards, passing through the center of gravity. Directions i1 to 6 (roll, pith, yaw) are rotations about the correspond-ing axes. The axes system is indicated in Fig.2.
It is usual practice to split the excitation force into two parts:
F=F1F
(2)
The force
(F1)
due to the pressure distribution of the undistrubed, incident wave is referred to as the Froude-Kriloff force. The diffraction force (Fn) corresponds to the scattering ofthe
incident waves By thestruc-ture.
Note that
both forcesare calculated without
considering motion of the structure.
Hydrodynamic
effects of the motions are taken care of by the
added-nass and damping terms.Potential flow theory allows the use of
three
poten-tial fields to provide complete information about the fluid flow related to the three corresponding wave syst-ems. The potential due to the incident wave () isknown from classical wave theory. The potential due to the radiated waves ()
is usually determined by
2-D, numerical, sink-source techniques f10]. The diffractionpotential is more difficult to handle directly, but it
can be eliminated to provide
an expression (often re-ferred to as the Haskind relation) for the overall diff-raction forces based on the other two potentials:ds (3)
where the i-index indicates direction no.i, p is the
density of the fluid,
SV indicates a field ofintegration
over the entire wetted surface of the semisubmersible, N is theunit normal
vector pointing toward the vessel, and ds is the element of surface area for the integration.Equation 3 supplies the diffraction force acting on
the whole structure. This is sufficient information-for the solution of the equations of motion. However,
more information about the distribution of the
diff-raction force over the various parts of the structure is required for the structural analysis of a semisub-mers ible. Equation 3 cannot be used to provide such information. It is based on a mathematical identity requiring integration over the whole wetted surface of the structure. Application of this identity is not valid for parts of the structure. Attempts to ig-nore this theoretical limitation have been shown to produce erroneous sectional forces in [8,9].
This problem can be overcome be employing an alterna-tive radiation potential
(a)
instead of the normal radiation potential for rigid body motion (). The boundary conditions for this alternative potential are chosen in such a way that integration over the whole structure will provide the contribution of the diff-raction force to the oenterline sectional force. In this case opposed motion of the two pontoons is chosen to give the body boundary condition; eg. when the starboard pontoon heaves upwards, the port pontoon heaves downwards. This does not imply that the actual seniisubmersible behaves in this way, but that the sol-ution of the radiation problem for two pontoons in opposedmotion enables
us to obtain more information about the distribution of the diffraction force on the rigid semisubmersible. The alternative radiation po-tentials are referred to as Opposed Motion Potentials'. This technique was originally suggested by Ogilvie [11]. Mathematical details are given in the appendix.Numerical Methods. The numerical results presented in this paper have been obtained using computer programs
developed at Det norske Ventas.
The same program [2]
was used to obtain results from application of both Morison's equation and improved strip theory. Further
details of the methods employed are given in f8] , with recent implementation of the opposed motion potentials documented in ref.[l2j . 3-D sink-source results have been obtained using L6]
Nesults in long-crested irregular seas were calcul-ated by the usual linear combination of the transfer function in regular waves with the wave spectrum. The short term response operator presented in the figures is the significant crest-to-trough value
of the response
variable. This is equal to four times the standard deviation of the response.MODEL TESTS
The
test rig is a new type of semisubmersible rig
designated the GVA O00, designed by Gøtawerken ArendalAB, Sweden, intended for drilling operations
in the North Sea above the 62nd parallel, or in similar regions. The structural approach utilizes a strong double deck struc-ture to replace the usual complicated configuration of bracings. Figure 1 gives an overall view of the rig,and its main data are given in
Table 1.Design Load Cases.
The structural analysis of the rig
was carried out for a number of lomi cases. Each dyna-mic load case was chosen to provide the extreme value of one parameter critical for the structural response,
together with simultaneously occurring values of all
other loads. These load cases may be briefly character-ised as follows:
Static - all stillwater loads.
Longitudinal racking -
maximum longitudinal shear
forces transmitted from the deck to the rest of the structure, due to longitudinal acceleration of the deck including the component of weight due to pitch angle.trans-Fig.i Cenerai view of semisubmersible GVAOOO The Model. Table 1 gives main dimensions of the rig model. Accelerometers were used to measure the motions of the rig. Figure 2 indicates how the model was split into parts and the sectional forces were measured. The following forces and moments were recorded at the center-line section:
F1 - shear force in the longitudinal direction
F2 - split force in the transverse direction between the two halves of the structure.
F3 - vertical shear force, closely related to the trans-verse racking force (case (e) above).
- bending moment about a longitudinal axis (splitting moment).
3
F5 - torsional moment about a transverse axis (pitch-connecting moment).
- bending moment about a vertical axis.
The horizontal moment axes were located at deck level, with origin on a vertical through the centre of gravity.
At the section through one column at the lower, deck level, forces were measured in order to study the stress in the connection between the column and the deck. Thes forces have not been included in the present paper.
The model was built to a scale of 1:65 in glass-fibr reinforced plastic and aluminium. It ws anchored by 8 chains arranged in a symmetrical pattern with 5 degrees between each anchor line, and with chain weight to the
appropriate model scale.
ig.2 Location of Force Sensors (0U1U2 plane is at stillwater level).
Table 1. Main Data for Semisubmersible at Operating Draught.
Model calculation Test
scale 1:65
-anchor lines (3 inch chain) 8 o
anchor pretension 1280 kN O water depth 195 m 300 draught 20.5 n 20.5 metacentric height 2.1 m 2.76 pontoon length 80.6 n 80.6 pontoon depth 7.5 m 7.5 pontoon width 16.0 n 15.7
distance between pontoon 51.7 m 5I.7 centerlines
longitudinal distance between 514.7 m 514.7
column centers
column diameter 12.9 m 12.9
bracing diameter 3.014 m 3.014
truss height over baseline 11.2 m 11.5 main deck height over baseline 141.0 n ' 37.0
roll 'radius about waterline 29.6 n 29.3 pitch gyradius about waterline 27.3 n 26.9
yaw gyradius 31.2 n '31.2
center of gravity above baseline 20.0 m 19.5
displacement 25307 m3 25320
height of force measurement in
deck 37.0 m 37.0
motions me,sured at centre of gravity water plan verse acceleration and roll.
(t) vertical acceleration - maximum vertical inertia forces acting on the deck structure.
split force - maximum axial forces in the trans-verse bracings due to hydrodynamic forces, on the pontoons. The transverse force acting between the two halves of the structure at a section along the centerline is used as be parameter for this case. pitch connecting moment - causing large bending moments in the deck girders at the connection with the columns. The torsional moment about a trans-verse axis at the centerline section is the critical parameter for this case.
Determination of this type of design load cases is further discussed in [9,13]. The r.odel tests vere designed to
check the values of the critical parameters used for the design load cases.
ce Te5ts
The model tests were carried out in the
Laboratory of the Swedish Maritime
Research Center.
This tank is 88 m long, 39 n wide,
and was filled to a depth
of 3 m, corresponding to
a full scale
water depth of 195 n.
Regular wave tests
were performed
in head, and beam seas for wave periods
of 7,iO,1,l9,21 and 25 seconds
with a Wave height of
7 n.
Irre&'lar wave tests Were carriel out in head,
quarterir.g and beam Seas with both Jonswap and ISSC
type spectra.
Long-crested seas were employed.
Thewave spectra used for
the results presented in this
paper are listed in Table
2.
Draught, anchor
preten-sion and
etacentric height were varied in the tests,
but only the values of these parameters given in Table
1 are employed herein.
The original reports of the
tests are given in
[l!].
Table 2.
Irregular Seas - ISSC spectra
significant wave height (n)
3 6 ' 9RESULTS
Transfer F-nction - ODerational Draught. Figures 3-5 and
7-9 show coparison5 of results obtained using the
Mori-son eouation approach, improved strip theory(indicated
as
2-D sink-source in the figures) and model tests.
Good agreement is shown between the two theoretical
aptrcaches in all cases.
For very long waves, the heave
response shcws some deviation.
This is probably
intro-duced by the increased importance of damping near
reso-nance, where one method applies drag forces and the other
applies wave-making damping only.
Fair agreement is generally shown between model tests
and calculations at short and moderate wave-lengths,
while large discrepancies Occur in long waves.
Diff-erent water depths in model tests and calculations have
influenced, the results in long waves to some extent.
Anchor line forces are another source for this
discre-pancy.
Anchors are present in the model tests, but not
in the calculations.
In regular waves the wave-induced
drift force
is relatively constant, causing a mean
dis-placement of the model from the stillwater position.
This, in turn, affects the anchor line coefficients,
making then unsymmetrical and increasing the restoring
farces on the side of the incoming waves.
The
unsymme-trical restoring forces induce coupling effects between
the mctions.
Figures 3-5 appear to indicate such
coup-ling of heave Into pitch and surge.
A small hump is shown in the model test results for
the vertical shear force (Fig.8) in long waves.
This
hump corresponds to the roll resonance (not shown)
ob-served in the model tests.
The split force (Fig.7) and bending moment about a
long-itudinal axis (Fig.9) are exceptions to the general trend
of agreement.
The calculated split force has been
checked against a simple, reliable formula with good
agreement.
Sway and roll motion results (not shown here)
at moderate wavelengths also indicate good agreement for
the excitation forces.
The three horizontal force
trans-ducers at the centerline section were arranged in such a
manner that a faulty signal form one of these could have
affected F2 and F9 without affecting F6, corresponding
to the trend in Figures 7,9,11.
Short Term ResDonse - ODerational Draught.
Short term
response operators are presented in Fig.6,lO,ll for
re-sponse parameters whose maxima occur in oblique seas.
Model tests and theory agree well for the longitudinal
force (Fig.6) and the bending moment about the vertical
axes (Fig.11).
The poor agreement for the torsional
moment (Fig.lO) is surprising, since much better
agree-4
ment is shown for the underlying forces, longitudinal
shear force (Fig.6) and vertical shear force (Fig.8).
Alt.
Fig.3
Transfer Function for Surge - Operational Draught
1.5 a 10 0.5 Oc. 2.0 4.0 60 135 A IL Fig.14
Transfer Function for Heave - Operating Draught.
z, a/A .o. MORISON 20-S NK-SOURE ® MODEL TEST
p
® MOSEL TEST - MORISOM ---20 5lNK-5OU(EFig. 5
Transfer Function for
Drauge
e
e
001 -4S LOMO-CRESTES SEAS
e
MOSEL TESTS- MORISOM
20 SINK-SOURCE s0 7.'S - T, (s.6
Short Tern Response, Longitudinal Shear Force at Centerline Section - Operating Draught.0 15 F, BL. 0 10 005 003 F, BL, 0 02 001 ,9O. - MORISON 20 SINK- SOURCE
e
MOSEL TEST.1 Transfer Function for Split Force at Centerline Section Operating Draught.
90 MCeISON ----20 SINK-SOURCE e MODEL TEST
e
e e
04 1.0 2.0 4.0 13.5B Tranfer Function for Vertical Shear Force at
Centerline Section - Operating Draught.
Fig.9 Transfer Function for Bending Moment about Long-itudinal Axis at Centerline Section - Operating Draught 0.02 -001 - RO' - MORISON - 20 -SINK- SOURCE MODEL TEST 45 LONG -CRESTED SEAS ® MODEL TESTS - EIORISON 20 SINK-SOURCE LONG - CRESTED SEAS MODEL TESTS M OR SON 20 SINK-0000CI
Fig.11 Short Tern Response, Bending Moment about Verti-cal Axis at Centerline Section - Operating Draught. Transfer Functions - Transit DrauRht. Figures 12-17
show comparisons of results from the improved strip theory (2-D sink-source) and 3-D sink-source
calculat-ions. Reasonable agreement is exhibited in most cases, though the points are a little sparse. The motions at the transit draught (Table 3) are naturally much larger than at the operational draught.
The sway transfer function (Fig.l2)shows a peak at a wavelength (AIL = O.61s) corresponding to the distance between the pontoons.
Pitch resonance (Fig.11s) is slightly displaced in frequency and less severe in the 3-D sink-source calcul-ation. This is due to 3-dimensional effects: the fluid
i
38 5.0
T,(s) 15 0
ig.lO Short Term Response, Torsional Moment about Trans-verse Axis at Centerline Section - Operational Draught.
1O° 15.0
o03
F,, BLM.
notion between the pontoons is allowed to transmit Dut beyond the ends of th pontoons in the 3-D Calculation. This effect is more important for pitch (and yaw) than for the other motions, due to
he long pitch moment arm applicable at the pontoon onds.
At the transit draught, the freeboard is very sml1 'otiOns or waves of moderate amplItude will easily sub-aerge the top of the pontoons. This introduces
signi-icant non-linear effects (e.g. in the buoyancy forces) oat taken into account In the lìnear formulation of the oquations of motion. The results of linear calculations
or transIt are therefore accurate only for relatively omall wave heights. A rough correction to apply these
esults in Somewhat larger amplitude waves may be offected by modifying the notion transfer functions at :he resonant wavelengths, based on experience from iodel tests (cf. [8,9]).
able 3. Altered Data for Semjsubmersible at Transit Draught.
Lraught 7.2 n
Lisplacement 17200 m3
laterplane area 238 n2
;ransverse metacentric height
8.7 n
ongitudinal metacentric height 186.9 n enter of gravity above baseline 25.3 m oll 'radius about waterplane 33.3 n itch rradius about waterplane 32.3 nav rradius 31.5 m C O OS 20 -X, 1.0 A - 9O - 20 SINK-SOURCE , 3D SINK-SOURCE 0.0 0.4 10 20 4.0 AIL NO
Lg.12 Transfer Function Sway - Transit Draught
p go.
-
20 SINK-SOURCE A 32 SINK-SOURCE6
Fig.11o. Transfer Function Pitch - Transit Draught.
Fig.l5. Transfer Function for Split Force at Center-line Section-Transit Draught.
03 F) Pg BL, 020.1 -o
£
-. 1.0p
- 20 SINK-SOURCE£
3D SINK-SOURCE 20 p.90 - 20 SINK-SOURCE A 3D SINK-SOURCE-80
1O 20 Fig.16. .0Lg 13 Transfer Function Heave - rÇansit Draught
Centerline Section
Trsit Drught
PgRL 01 00 O,' 2,0 40 A /1 8U p. 0' -20 SINK-SOURCE 15 L 30 SINK-SOURCE 10-A 04 'U 2.0 40 0. 0 A /L
00
10 20 O
Fig.lT.
Transfer Function for Berdin
Mo=ent about
Longitudinal Axis at Centerline Section
-Transit draught.
CONCLUSION
For operational draught:
Good agreement has been shown between the improved
strip theory and the Morison equation ancroach.
Fair agreement has been shown b- model test
results and theoretical calculations.
Peasonable
hypotheses have been suggested to explain the cases
with larger discrepancies.
The Morison equation approach is recormended for
operational and survival draughts, unless there is
reason to expect more hydrodynsmic interaction between
the elements of the structure than in the present case.
For transit draught:
Fair agreement has been shown between the improved
strip theory and 3-dimensional sink-source calculations.
Sectional loads obtained using strip-theory with
oppos-ed motion potentials provide much better agreement than
the usual strip theory in
[8]
.Pitch motion is affected
by 3-D effects at the ends of the
ontoons and shows
some discrepancy.
Assuming that the 3-D sink-source calculations
pro-vide a valid basis for comparison,
the present results
indicate that the improved strip theory nay be used for
the calculation of motions and loads acting on
semisub-mersibles at transit draught.
Pitch motion is
calcul-ated less accurately than the other motions.
Further
comparison with model tests is desirable.
The
limitat-ions of linear theory are, however, particularly
re-strictive for these conditions, with significant
non-linearities in the buoyancy forces being introduced at
moderate wave heights.
APPENDIX - CTERLINE SECTION DIFFRACTION FORCE
This derivation is only concerned with the
appli-eatlon of opposed motion potentials to determine
the
Contribution of the diffraction force to the sectional
force at the centerline between two pontoons.
Moredetails about the other hydrodynamic
forces may be found
in
[8J,
where the relevant potentials
are treated in a
similar mamner.
We consider two geometrically similar vessels, each
having two pontoons, floating at zero speed.
Vessel
A is rigidly fixed in incoming
waves.
The diffraction
7
forces on this vessel will be equal to the diffraction
forces acting on the semisubmersible we are actually
interested in.
Vessel B is forced to perform harmonic
motion with the two pontoons moving in opposite
direc-tions.
Vessel B is not subject to incoming waves.
Thefluid motion induced by the motionofvesse0 B is
describ-ed by the opposdescrib-ed motion potentials.
The assumptions
previously listed are considered to apply.
The incident
(), diffraction (0), and opposed motion (o) potentials
all must satisfy the Laplace equation.
Boundary Conditions. At the free surface, kinematic and
dynamic considerations lead to the classical linearised
free surface condition, which must be satisfied by all
the potentials (,O,o):
+ g
= Oon u
= O (lo)On the surface of vessel A, the incident and diffracted
potentials must satisfy a kinematic boundary condition
giving zero velocity through the body surface at the
mean position:
on vessel A
(5)
The opposed motion potentials must satisfy a kinematic
boundary condition on the mean position of the surface
of vessel B, giving a normal fluid velocity equal to the
velocity of the hull surface due to the motions:
3h
(x-a.) = - jx.n.
ii
i].
ori vessel B
starboard (SS)
(6)
(xe.) = + joix.n.
on vessel B
3N
ii
ii
port (SP)
(T)
where the generalised normal (n.) is defined by:
(n1,n2,n3) = N and (n,,n5,n)
x N
The bottom condition gives:
(8)
asu
-3u3 3
At large distance from the vessels, both the diffraction
and opposed notion potentials must fulfill a radiation
condition for outgoing waves [151:
hm r (- -jk0) = O
on r = v'u1 + u
(9)
30
where
is the velocity normal to the control surface
in the outward direction.
Determination of the Potentials. The incident wave
pa--tential
may be written:
exp Ck(Ju1 cos
+ ju2sinß +
u3))
The opposed motion potentials may be determined by the
same 2-D sink-source techniques as are normally used
within strip theory [loi.
The body boundary condition
must be appropriately modified, and the symmetry of the
problem is changed.
The diffraction potential is not
determined directly, but is eliminated as imdicated
be-low.
Expression for Sectional Force. The dynamic pressure
due to the diffraction potential may be expressed using
the hinearised Bernoulli equation:
(11)
= j w p e
(12)
A 008-- 2
-S..oUeCE ASX-SuCE
Pg3L 006-00 002 A['he corresponding forces on the starboard (G) and port :H) pontoons of vessel A are found by integrating the Dressure over the aporopriate areas:
f
Pn1 ds = jwpf
Sn. ds (13) J.SS SS
= jwp
f
Sn. ds (la)1 J.
y consideration of the even and odd portions of the liffraction force acting on either side of the center-Line of vessel A, it is easily shown that the centri-)utiOfl of the diffraction force to the sectional force is given by: D. = (G. - H-) J. 1 1 =
jup[ f
On ds -f
Sn ds] (15) SS SP['he opposed motion potential for vessel B may be sub-tituted for the unit normal on vessel A using the body Doundary condition (eq.(6,7)), since the two vessels
re geometrically similar: =
pf
ds -® ds= -p5 S
ds (16)result obtainable from Green's second identity is now ieeded. This identity relates volume and surface inte-rals over a closed region for two potential functions
e ,o. ):
f (OV2a
-
e.V20)dv= f
(5 i - ) ds (17)y 1 j.
SC 3M
iBN
['he region of integration is indicated in Fig.l8. The murface (SC) enclosing the volume (V) includes the ressel surface (SV = SS + SP), the free surface (SF) [istant control surfaces (SR), and the sea bottom (SB).
q.(l7) is then simplified by making use of the proper-;ies of the potentials. Both potentials satisfy
aplace's equation in the fluid domain, thus eliminat-ng the left-hand side of eq. (17). By invoking the ottom, radiation, and free surface conditions, it can e shown that the surface integral of the right-hand ide of eq.(l7) reduces to an integral over the sur-'ace of the vessel:
f (o
-
0. (18)SV
ubstituting in the expression for the sectional diff-action force gives:
D. =
-p
f
a. ds (19)1
sv
inally, the body boundary condition (eq.(5)) is applied o eliminate the diffraction potential
D. = sP
f cr
30as
(20)SV
C10WLEDGNTS
Permission given by Gøtaverken Arendal AB to present he contents of this paper is gratefully acknowledged.
8
Fig.l8. Region of Integratic:. fcr Application of Green's 2nd Identity.
R'EH EN CES
Burke, B.G. , "The Analysis of Motions of Semisub-mersible Drilling Vessels n Waves", Offshore Tech-nology Conference, paper o. OC l024, Houston 1969.
Pedersen, B., Egeland, O., and Langfeldt, J.N., "Calculation of Long Term Values for Motions and Structural Response of Mobile rilling Rigs", Off-shore Technolo' Conference, :aer No. OTC 1881, Houston, 1973, pp.II-539 - Ii-554.
NordenstrØm, N., Faltinsen, O., Pedersen, B., "Prediction of Wave-Induced M:-ions and Loads for Catamarans", Offshore Techrìolcg.' Conference, paper No. OTO 11l8, Houston, 1971, oz.II-l3 II-58.
. Chung, J.S., "Motions cf a Floating Structure in
Water of Uniform depth', Jc.ra1 of Hydronautics, Vol.10, No.3, July 1976, p. 65-73.
Paulling, J.R. et al. , "Analysis of Semisubmer-cible Catamaran-type Platforms ," Offshore Technolo' Conference, paper no. OTO 2975, Houston 1977.
Faltinsen, O.M., and Micì-ielsen, F.C., "Motions of Large Structures in Waves of Zero Froude Number," International S'rmoosium on the namics of Marine Vehicles and Structures in Waves, London, April l97, pp. 99-ilL.
Wichers, J.E.W., and De 3com, W.C., 'The Dynamic Loads for the Strength Design of Moored Offshore Struc-tures under Storm Conditions," Offshore Technolo' Conference, paper No. OTO 32L9, Houston, 1978, Vol.111, p.1701.
Mathisen, J., and Carleen, C.A., "A Comparison of Calculation Methods for Wave Loads on Twin Pontoon Semisubmersibles," SSPA International Ocean Engineer-ing Ship HandlEngineer-ing Symoosium, Gothenburg, Sept. 1980.
Carlsen, C.A., Mathisen, J., "Mydrodynamic Loading for Structural Analysis of Twin H1L11 Semisubmersibles", American Society of Mechanical Engineers, Applied Mechanics Symeosia Series, Vol.37, 1980, pp.35-lS.
Potash, B.L., "Second-Order Theory of Oscillating Cylinders," College of Engineering, University of California, Report No. NA 70-3, Berkely, June 1970.
Ogilivie, T.F., "On the Computation of Wave-Induced Bending and Torsion Moments," Journal of Ship Research Sept. 1971, pp.2i7-22O.
FREE oT s
c-o
SURAC POTOOM
BØrresen, R., Mathisen, J., "Strip Theory Methods for the Prediction of Wave Loads on Twin Pontoon Structures Floating Near the Sea Surface," Det norske Ventas, Report No. 81-0571, Høvik, Norvay Jan.1981. Cansen, C.A., Gundersen, N.B., Gran.'S., 'Envi-ronniental Data jo Operation and Design. Design Case-Mobile Rig," Norwegian Petroleum Society, RØros, Norway, Feb. 1981.
1.
Lundgren, J., "Semisubmersible Drilling Rig. GVAl0O0 Seakeeping Tests." Svedish Maritime Research Centre, Report No.2586, Vol. 1-5, Gothenburg, April 1981 (proprietary).15. Wehausen, J.V., and Laitone, E.V., "Surface Waves" landbuch der Physik, Fluegg, S.(ed), Vol.9, Fluid Dynamics 3, Springerverlag, Berlin 1960.