DAVID W TAYLOR NAVAL SHIP
RESEARCH AND DEVELOPMENT CENTER
TECHNISCHE UNIVERSI Laboratorium voor Scheepshydromechanica Archief Mekelweg 2, 2628 CD Deift Tel.: 015-786873-Fax: 015-781838, Z1
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1t t±ze
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Zr
veiccity etveer crc5-trtcttre ard free
A study was
xade of etb&4s
for iprof ng the nteans ofestinatirtg
the expected cttherof wa-ge i=pacts per
unit tine ofthe SWAT3 ship cross-s trtxcture. To avenrnes
were explored:(t) inprovennt
of relative
notion esUnates by adding thecon-poe-tirs of ship-generated wave atid diffracted wave to the
md-- dent wave in describing the free
surface:
and, (2) inclndirtg a limiting impact angle in the criteria defining the occurrence of a saim in the fornalation of the level-crossing definition from which the expected ntuaber of impactsis derived.
The
results ofthis study sfii that including the ship-generated we and
diffracted wave does not improve the correlation of the ccmpcted relative notion with results obtained from
experiments.
Imposing a limiting impactangle on the
definitfon of cross-strttureslamming, as expected, reduces the estimated frequency of slaiiming.
Mditiocal
model exerLxtents
are recommended to obtain a moredefinitive estimate of threshold velocity and limiting impact angle for estimating SWATH cross-structure sIamrdtrg frecencies of
occurrence
-A1NTSTAflVE IGtLTIO
This work was performed under the aval Sea Systems Cotmirand General
Hydrody-namie
!asearchProgram a ministered
by the DTSDC Ship PerformanceDepartment. Funding was provided under Program Element 611 533g, Task Area SP23O1!O1, and Work Unit 1562-500.
INWc3CTIO
A potentially serious problem inherent in the SWATH ship concept is its propensity for sustaining wave impacts on the underside of the structure con-nectirig the twin hulls while operating in * heavy seaway. The Impacts not only can Impose large tertiary loads on the loç Cross-structure, irzcreasirrg'ship structure and weight, but can also induce iibratiorrs and accelerations
resulting in serious
structural fatigue problems. ecent experience suggests that methods developed for monohzzll slamrdrtg are inadequate for SWATH ships.ThIs should come
as no surprise since the noriohull method was developed topre-dict sLams on the ship's bottom: whereas, SWATH Impacts take pace on the upper
structure connecírig the two struts. Obviously, new tools are needed by the
designer to establish conditions under which wave Impacts occur, and to
An iiportant indicator of a sMp's susceptibility to slamniing is the noether of occurreeces of slzimdrig per unit tíie. This not only provides a relative
measure of
the merit of different STJAIH designs fron the perspective of slamning, but also helps to identify those factors influencing the ship'ssla=ing characteristics.
The
occurrence of a cross-structure slam Is dependentupon at least three conditions. They are:
I. Entry of the cross structure Into the water (An obvious requirament.)
An entry velocity exceeding some threshold velocity.
A si'fl. angle between the cross-structure and free surface at point of impact.
As can be seen frein the above criteria, the relative motion between the
peint of impact arid
the
free surface is an important parameter in determiningthe occurrence of a cr055-structure slaza. if it is assumed that the relative motion and the angle between the cross-structure arid free surface at the point
o f i mp.ac t a re s ta ti oria ry Cuass Ian processes, t hem the number of si aus per unit
of time can be determined from the computed statistical properties of these variables. The above assumption is reasonable in the context of linear ship
motion theory even thuh in reality the impacts produce sharp nonlinear peaks
in the acceleration. These impacts occur in a short interval of time arid the effect upon the ship displacement and velocity are minimal.
Since it is reasonable to expect that a more precise determination of the relative motion would provide a more accurate estimate of
the
occurrence of slxmirrg, a procedure vas developed for includingthe
ship-generated waves amid che diffracted wavesfri the
coorpitatíons of the relatíve motions. Routine com-putatiorts only consider the incident wave as part of the free surface andneglect ship-generated waves and corresponding diffracted waves. Computations were also made to determine the effect of assuming that impacts occur for a limited range of angles between the deck and the free surface at the point of
impact. This also has not been considered la routine computations. BACKGROUND
A method for estimating the expected number of slams per second of a
mono-hull or conventional ships bottom was developed by !ick', based upon the
rela-tive bow motion and angle between wave and keel at the contact point. lt was
:»
assuzited that the slaai occurred when the relative velocity between the bou ai
the sea surface exceeded a critical aniomt at the tizne of contact, the bou ce
out of the water previous to contact, and the angle between the wave and keel at
se chosen contact point vas small.
In addition, the relative motion and angle
between keel and wave were assed to be stationary randora Cuassiart processes.
arrived at the se formulation, excluding the effects of liimiting the
angle between wave and keel, by assuming a
ore restricting narrow band process,
arid was able to obtain other important statistical properties of the slaanirtg
phenomnezion.
Ochi was also able to derive empirically a threshold velocity of 12
f tfsec (3.7 nt/sec) for a 520 foot (158 meters) Mariner Class ship f
ro
nodel
experinments in irregular waves.
Ochi's data are show in Figure 1.
In a
sub-sequent paper, Ochi3 proposed that the threshold velocity of 12 ft/sec (3.7 nt/sec)
found for the Mariner Class be Froude scaled for ships of different lengths.
This is the general practice currently in use for computing the
expected nuzitber
of occurrences of nonohull bott
sllng.
Application of the above criteria to the botton of the deck structure
con-necting the twin hulls of a SAIH ship has not been verified and
a procedure for
scaling the thresbold velocity fron the botton slannning of
a Mariner Class hull
to the cross-structure of a SWAIH ship is not readily apparent.
Figure 2 sbous
a plot of the cross-structure slazmaing pressure variation with respect to the
relative velocity obtained fron model experiaents with a 1/32 scale
SWATH T-A()Sin waves.
These data show sic occurring at relative velocities
as low as 1/2
ft/sec (.15 nt/sec) at a ship speed of 3 knots in head
waves and as low as 2
ft/sec (.60 nt/sec) at a ship speed of 8 knots.
The threshold velocity obtained
by Fraude scaling the value for the Mariner Class (based
upon length) is larger
than the velocities at which slants were recorded for the T-ACOS tirodel.
Another
paradox is that the expected number of occurrences of slazrmdng conputed frani the
relative notions arid the observed threshold velocities do
riot coincide with the
actual tneasured values.
It is guite evident that the conventional formulation
used in estimating the expected number of occurrences for nonohulls
is not
directly applicable to the SWATH cross-structure problem, and the influence of
other parameters such as the angle between the structure and free surface
needs
...
M,
T
:'
r
PROBABiLiTY OF SLAMMING ThCLITDINC A1'iGLE OF IMPACT
Chuang4 developed a relationship between pressure and velocity for enti-mating maximum slamming loads ori high speed craft which is given by
Max pj 12V
where k is an arbitrary constant
P is the mass density of the fluid and
IT is the velocity normal to the wave surface
The impact pressure p1 is that part due to the velocity component of the craft normal to the wave surface. The total impact pressure includes a contribution
due
to the forward velocity of the craft. Of particular interest is the fact that the constant k is actually a function of the impact angle. i.e., the angle between the structure and the free surface at the point of contact. Figure 3 presents the relationship between the constant k and the impact angle as established by Chuang. Chuang5 has applied this method to the cross-structure slamiririg of a catamaran with good results. In this case, the slamming pressure due to the horizontal velocity component of the ship could be neglected without serious error because of the relatively loz speed of the ship. Since thecross-structure of the catamaran is very nearly the s as that of a SWATB ship, it can be reasonably assumed that the expected number of occurrences of slamming per unit tine is also dependent upon the angle of impact.
As previously indicated, Tick developed an analytical expression for
cori-puting the expected number of slams per unit of time of a ship's bottom based on the conditions that at the time of impact: the
relative
motion Zr(t) passes through the value -k; the relative velocity Zr(t) exceeds none threshold velo-city v>O; andFF.í<.
where is the difference between the angle of the keel and the slope of the wave at the bow. It is assumed that the relative motion Zr(t) and the angle (t) are stationary Guasian processes.The development is
a generalization of the method of RiCeb and establishes the probability of an level crossing in the inter-val between times t, and t + dt, under the specified conditions. In the following notation, x1, x2, X3
correspond to the relative motion, relative velocity, and relative angle, i.e., w1 Zr(t) x2 Z.(t),
r
«t).
For dtsufficiently sa1l x1(t) can be
considered as a straight linein the
interval andx1(t) - x (t3) +
2
(t3)(t - t0)
Then, if p(x1,x2,x3) is the
joint
probability of the randoc variables, thepro-bability of a k-crossing with the required properties in the interval dt is
given by
=
f(dt)
dt
3f(x, 12, 13)
"
3-x2dtand since the irttegrand is continuous this reduces to
2
f(dt)
-dfdx3Jdx2x2
f(10,
X,
13)for Gaussian variables
f(x1, 12, 13) 1
exp(WQ)
(21»312 Dh12
where
Q
:cTijXizj
is the
elenent of matrix inverse to he matrix (ajj) of the covariances and D is the Determinant of the matrixIntegrating the above equation for the case
o2 =
over the interval from O to T gives the expected tunber of slams in the interval.Dividing by T gives
the expected number o slams per unit timef
[
c ]V2
exP[_V2(+)]tD(o2)
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023 013
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o'
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Nall 033 -
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Z2 N°22 N -
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r&1 otlo, aM dtf(ratlo
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oteritlala
,,r
plb aM yai
tiot are
li&-r by
fa the forvard ape4 of the VATØ ahí p and
fa the encounter frequency.
The au-rge voce-nt fai,
,
fa aaat
to be zero.
The
1itfôri
of 4j (J -
1, 2, 3, 4, asid 7) baa been preaented by
(n,)
(y,z;n,)di j'-2, 3, 4, 7
()
vhere
fa the source strength dfctrfbuted ou the
ATh ship's contour and
fa
t-1nefona1 creen function due to a unit source on the contour
The Creen
f n tión, C, Is giren by 1ehatzaen and Lai
'-
Jiog(y+z-i-f)
- 1og(y+1z-iw1)
+ 2
-ihere b',z
la the point ihere the potential f. sought and (n, ) is a source
point at the SWATh .hlp' a contour.. The source strength,
fa deteriifned by
the body boundary condftlon. as foiltws
- -iri, for
J2, 3, 4
(10)
,for
J1* the
ip&nent of the unit nrma1 'ector directed into the fluid.
11
The absolute i't-ttical
otioii of the
IAT1 ship f. cputed by
-
4- y4 -
(11)
The relaeie bo
zotion (ZM) is sfly the difference between
atfons (5) and (11)
-
+ y
x)
-In the nuerfcal côntatf on of 4uation (12),
the aplitude ofuotfon, ci,
is cçsxted with SWATh ôtfii progra
and the velocity poential,
f.
c-puted with WtTRO2 (ship iiotion prograzn) at
a gí'ien point (y,z)
located ouC;fdethe wetted bOdy.
Ciparison with Ezperfnents
A copaxf son of the coaputed
relative øotfons with ezperfenta1 results for
three lc
f oms ori T-AiS SWATH i. presented fri FIgure. 3 through 1(.
The
location. corrspond to the forward, aidshfp and after portion of the
cross-structure along the center line of the ship. Figure 3 shi's the coputatfous
of relative
tbon in head waves at a shf p spee4 of 3 biots with only the
md-dent vve representing the free surface and again with all three
coiiiponents:
incident wave, ship generated wave, arid diffracted wave Included. These results
shw chat the coputatforns vi th Just incident waves are very close to the
experi-ental results and paradoxically, including the ship-generated
wave and
diffracted valles, fri general, degrades the correlation between the co«iputed and
eperírental result..
The zaae trend is evident at a heading angle of 135 degre.e
and a speed of 3 knots as shown fn
Figure9..
In beari vives at a speed of 3
knots, Figure 1C, the incident wave vas the doninant free surface factor and the
ship-generated waves arid diffracted wave corponerits had ari insignificant effect
upon the cop'uted results.
It is interesting to note that Lee, et al.,7 in their re exteisive studies
of the relative notion conputations of co1iulls
concluded
that there is noconclusive evidence
that the inclusion of diffracted and notion-generated waves, as conprited by strip theory, inproves the results. Apparently, the sconclu-sin can be
nade in
regard to SWATH-type ships.StAZT AXD COCLUSIOS
An rigatfn vas nade to mnprove nethods for estinating the expected
number of occurrences of SWATH ship cross-structure slannløg per unit tine. Slamming of che cross structure Is an inportaut consideration in the assessnent of the operability of SWATH ships in waves and the utther of occurrences per unir
cine provides a
quantitative ncasure of the slamnlng characteristics ofSWATH ships. A nethod fr conpucíng the mber of occurrences of slans for
nönohulls fron relative ship notion has been in use by the ship designer for nany years. lt is essentially a level-crossing problen based upon the
asstp-tin char a sian occurs when the
keel
at the point of inpact, enters the waterwith a velocIty greater than sone uniting threshold velocity. The threshold
vlocíty has been deter'nined fron nudel experfnents for a Mariner Class ship in waves. This threshold velocity is Fronda scaled for ships of different lengths.
The same approach is dfrcctly applicable to the cross-structure slaing of
SWATH ships. -er, it is not readily apparent how to scale a thri,shold velo-'ity value for keel slaing of a Mariner Class ship to the cross-structure
slanrIng of a SWATH.
In addition, it is believed that other paraneters such as the inpact angle nay also gci7ern the occurrence of a slan on the SWATH cross structure.
Calcula-tion of the expected number of slans for a SWATH T-ACÛS fron the relative noCalcula-tion using the lowest Imnpact velocity recorded, as the threshold velocity resulted in a value niich higher than the observed value. It vas concluded that other
para-neters,
such as the uniting impact angle, contributed to thís discrepancy.Calculations
were nade showing the
extent to which the uniting fnpact anglereduces the estinated nunber of occurrences of slams, but there was insufficient experine-r-mcal data to definitively define a uniting impact angle and, therefore, the results of this aspect are inconclusive.
13
Since the relative notion
is
an important parameterfor estinatf
ng thef
re-quency of slaing, an exa1nation was iade to deter1ne the effects of
including ship-generated waves and diffracted waves
in the
cputation of the
relative notion. Strip theory vas used to coute
the
ship-generated wave ariddiffracted wave which vas added to the incident wave in describing the free sur-face away
fron
the hull at the pointof furpact of
the cross structure.Copu-tatfons nornally include only the Incident wave.
The results of this frwestfgatforz showed tb-at there vas no Itnproveiment in the
co-nputed
relative notion (when con-pared to expermnental results) by theInclusion of the sb-f p-generated wave arid diffracted wave In the free surface
elevation.
In the cases exaialried, the ase of the incident wave alone gavebetter results or the sane as that obtained by Including the ship-generated wave arid diffracted wave.
In sary, che following conclusions can be nade based o-ri these studies: The frequency of slaiiimlrtg of SWATH cross-structure is not only dependent upon the relative notion, relatIve velocIty, ar4 a threshold velocity as fri the case of uionohull keel slaimning, but is also dependent
upon so-ne uniting Iriipact angle.
There is insufficient experinental data to establish lfiting Inpact
angles for SWATH ships or other paraneters influencIng the frequency of
slnnIng.
The inclusioni of ship-generated wave and diffracted wave in the con-putation of relative notion, which is needed for the estination of the
frequency of slarinIng, do-es riot in-prove the correlation with nadel
experinent results.
lt can be
concluded
fro-n the above that additional nadel experinents are required on a SWATH ship to obtain data to specificallyaddress
the problen of estinatinig the expected nunb-er of inpacts per unít of tine by obtaining, in addi-tion to the custonary neasure-nents, other inportarit nesureitents, such as cheangle of liipaot.
Tick. Leo J..
Certain Probabilities Associated with Bow Su1rgence
and SMp Slazning in Irregular Seas,
Journal of Ship Research, Vol 2, No 1, 1958.
Ochi, M. K..
Predíction of Occurrence and Severity' of Ship Slaing at
Sea,'
Fifth Symposiuzx on Naval Hydrodynaiics, Office of Naval Research, ACR112,
1964.
0cM.. M. K. and Motter, L. E.,
Predictfon of S1Ing Characteristics
and Hull Responses for Ship Design,
Trans. S!AME, vol 1, 1974.
Chuang, Sheng-Lun,
Slamnfng Test of Three-Dimensional Models in Calm
Water and taves,
SRDC Report 4095, Septeiber 1973.
Chuang, Sheng-Lun, et al.,
Experiental Investigation of Cataaran
Cross-Structure Slazxmdng,
NSRDC Report 4653, Septeeber 1975.
Rice, S. O.,
Mathematical Analysis of Rando %oise,
Bell Sys. Tech.
Journal, vol 24 arid 25, 1944 - 1945.
Lee, Choung M.. et al,
Prediction of Relative Motion of Ships in
Vaves,
Fourteenth Syinposimi on Naval Hydrodynamics, Office of Naval Research,
National Acadetny Press, 1983.
Frank, W..
Oscil1ation of Cylinder in or briow the Free Surface of
Deep Fluid,
David Taylor Model Basin Report 2375, October 1967.
Uehausen, J.V., and Laitone, E. V.,
Surface Waves,
Handbook der
Physik, vol 9, pp 446 - 778, 1960.
15
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j
IP..
.
.
.
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'e J/
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FL1Figure 1 - Mariner Class Slai
Data (Ochi2)
200 100 80 60 40 20
io
-40.0 20.0z 8.0
.0 2.0 1.0 0.4 0.6 0.8 1.0 2 0 4.0 6.0 8.0 10.0LATIVE VELOCITY IN }Tïi/SECCD
t e
i
t I I J0.12 0.2 0.4 0.6 0.8 1.0 2.0 3.0 RELAiIVE VELOCITf IN NETtRS/SECOND
FI gure 2 - Cross-Structure Slaia Data for T-AßOS SWATH
17 SHIP
-
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12
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SEA STATE 7. PROGRAM A
Figure 4 - Wave Speetru for Relative Motion Calculations
140
120
100
cIso
0 3
0.4
0.5
0.6
0.7
0.8
0.9
1.0
FREQUENCY OF ENCOUNTER IN RAD/SEC
180
PHASE
160
6003
0.4
I0.5
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tFREQUENCY OF ENCOUNTER IN RAD/SEC
Figure 5 - Relative Motiork Response Operator for TAGOS at 3 Knots
in Head Waves
20
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