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America Cup Update
By Johan Vaentijn
Since the use of 12-Metre racing
sloops tor the Americas Cup series in1958, millions of dollars have been
spent ori research and develcpment. In the programs of various designers,many "breakthrough" shapes and
forms have been invented. Most of the
odd shapes actually built have been
unsuccessful partly because of
unpre-dictable scale effects with the use of
small models and partly because of the many restrict ions of the rule itself. Tank tasting simple shapes hasproven to be more successful.
When commissioned to design the nC'N West Australian America's Cup challenger by Alan Bond, Bob Miller and I were given about seven months
to come up with a fast boat. This short
period demanded proper planning
and a systematic approach. In the fol-owing our basic approach is outlined although some of the parameters andnLimbers shown are changed 1rori the values for the neviAustra/ia (Fig. 1).
To minimise the scale effects we
de-cided to t'y for the largest possible
model size. This brought us to Deift
University. Holland. Here the tack can
hancle 12-Metre models at a scale of
1:9 which gives a LWL of about 165m
with an overall model length of about
225m. This larger model size avoids a
lot of scale effects that appear on
smaller models. The models 'Nere
towed by a special carriage which car-ried the operator and the instruments. These instruments are specia!iy
devel-oped and built by the University for
yacht testing and this facility ¡s among the best available in the world.
First, data was compiled of the wind
conditions off Newport, Rhode Island. During July the wind is anywhere
be-tween six to 15 knots 70 percent of the time.
During August, the range of
about six
to10 knots is favoured.
In September the America's CUP races are sailed in winds ranging between 11and 15 knots 43 percent of the time
with 27 percent below this and the rest
above. Consequently, we would need
a hoal that has her best ¿hi-round per. formance in winds between 11 arid 15 140
t
fr7 /9
knots, better performance below 11
knots than the present 12-Metres, and
similar windward performance
in winds over 15 knots.Analysis was also made cl the spe-cific sea conditions at Newport in the
area ot the race course. In the 10 to 15
knots true wind range, the average
wave height is two to three feet. A
measured spectrUm corresponding t
this range was used in calculating the
rough-water characteristics of the
models.
At tirst an intensive study was made of aU ot the successful and a number of less successful 12-Metre yachts of the
past. Comparisons were made on
paper to try to determine what rriakes a
winning Twelve. Analysing all of the
The rw bc.at h oniy
faer up to thout
20 not ofbeze.
if you couki b
cer-tdr. t woud ;ow,
Southn Cross
vud
th boat
to take to Newport
1974 races and allowing for tactical
er-rors, we decided that Southern Cross
was about 25 seconds slower than
Courageous on a 4.5-mile windwardleg and 15 seconds slower downwind in 12 knots of breeze.
From all the comparisons two
mod-els were developed primarily to try
lighter boats, but which also had a
number of basic different features inlength, beam, longitudinal centre of
buoyancy (1.CB), prismatic coefticient
(PC), etc, Thuse models were
corn-pared against a model of Southern
Cross, 1974. Model two was five per-cent lighter than Southern Cross, and model three, 10 parcent lighter thanSouthern Cross. All three models were
then tank tested in smooth water
and computer tested in rough wafer. In addition, flow studies were made. The
Lab.
y. Scheepsbouwkund
Technische HogschooI
Deift
C);-t'i
'c;-)
¿aLt
\
i
/J
principal result ot these tests was that
model three was slightly
laster allround than model one, Southern
Cross, while model two was similar to
model one in most conditions. After reviewing the firstthree models
in various ways, we decided that we
should design a very light 12-Metre. A
light displacement would be favoured in light air for quicker tacking, better acceleration and better rough-water
performance. lt would also have more sail area per pound displacement and
per square foot of wetted area,
all speed-making factors.Light displacement however, gets heavily penalised n the rule with the
chain girth difference. Yet testing a
very tight model with a large chain girth
penalty would give some more insiaht as to what the intluence is. The fourth
model was tobe 20 percent liglr ter than Southern Cross and would incorporate
the good features troni the previous
models.
The big problem with light-displacemnu'nt boats is thou stabilit'j Stability iS the most important tactorfor
windward performance. Thus, when reducing the displacement by 20
per-cent overSou'themn Cross without alter-ng beam, we would lose some 20 per-cent stability. This decrease would kill the windward performance as was
al-ready proven with the various studies
ot the first three models.
To geta handle on stability, a special
study was made. The most important
factors For stability are: Displacement
BWL and BWt./Tc (BWL = Beam
waterline; Te
Canoe body draft
below the waterline)
o) Vertical centre of gravity location
With a computer program, stability
curves like those shown in Figure 2
were calculated for various models.With all the data obtained, graphs werd
developed thaI would allow predicting
the stability at 25 degrees heel angle of
a proposed model within one to two
porcenit(Fig. 3).
The graphs amo developed in such a
displacement, a BWL and BWL/Tc can
be selected. As the relative centre of
gravity of 12-Metres is more or less
es-tablished, the stability arm NG sin
could be read and a cross-check on stability made. If it fell within two per-cent of the required righting moment,the midship section could be drawn up using BWL and Tc from the graphs.
In-creasing the BWL increases stability
but also increases fhe resistance. The
idea was to find the optimum stability
for the least resistance.
The overall stability of the boaf also
depends on the rig size. The larger the
sail area, the larger the heeling
mo-ment. As reducing the displacementalso increases the chain girfh penalty,
the total sail area for the fourth model
would become, therefore, similar fo the original Southern Cross.
Test data for each of the four niodols was compared to investigate the
influ-ence of various parameters on
resist-ance.
Upright resistance of the boat can be divided info three main groups:
a) Frictional resistance
b) Residuary resistance
C) Added resistance because of
waves
Frictional resistance is dependent on
the wetted surface and is easily
pre-dictable. To reduce frictional
resist-ance, the wetted area should be
minirnised where possible.The residuary or wave-forming
re-sistance is more difficult to control. The significant parameters include BWL vs
LWL, PC, LCB, displacement,
wa-terline entrance and exit angles, and the shape of stations, waterlines, anddiagonals. The relative influence of
these parameters also depend on the speed range. As mentioned, we weredesigning for a wind range up to 15
knots. The maximum downwind or
reaching speed
a 12-Metre will achieve under those conditions will be eighf fo nine knots. Up to about eight fonine knots, the waterline length of the
boat is not the mosf important factor as
this range still falls within maximum
hull speed.
Above this speed the waterline
length becomes increasingly
impor-- .
'. ,r,'
"t'
._tant. One graph developed after the fourth model was tested plots
LWL/BWL versus residuary resistance
per ton displacement (Fig. 4). In the
low speed range there
is little dif-ference between the narrower boats and the beamier boats. However, as speed increases, resistance increa-ses. The beamier the boat the greaterthe increase. For a boat speed of eigi
to nine knots the narrower waterline
boat has the advantage.
The second graph developed shows
displacement vers':s resistance (Fig. 5). After plotting the first four models
we saw a tendency toward an optimum
displacement around 58,000 pounds in the curves. This graph can only be
used here as the stability falls within a small range which keeps the models n a close relationship.
Similar indications in regard to beam
and displacement came oui of the
rough-water studios. To get an indica-tion of the performance in a seaway, a
Deltt computer program for yachts in sea conditions was used. This pro-gram calculates
for' any given sea
141
-I
_7
---
-Figure 1: Profile of the new Australia superimposed on larger profile of Southern Cross
X 10'
x JO Static Sta biltty SJab,iity_PaiarnCterS
A
160-
/ ,<
72 20.A 2.5
140-+
'°
Figures 2 arid 3:= 5.67' 68 NG Si' Examples of stahl/it)' 120- 11 2 0 curves used in developing
- the new 12-MatTe
GM = 4 60' Mx
..RM:''
,±'-S4OO/
0 64 0) 'Q FJ°M28 9 8 97 57.4f
'
80-/
2ì62 11.0 -96 S/
0) 960"r
95 94/
::"
1
)5 0 10 200 30: 2(1 .1 2.2 2.3 2.4 . .. .7 Heel-angle BWL/TcI
14212
0
HRS/Disphiccment tons Vs= 2.10M/sec 3.8 3.9 4 4.1 t I 4.2 4.3 4,4 LWL/81'VLspectrum the added resistance, the
pitch motion, the heave motion, etc.For two different sized models the radii
of gyration were calculated. This
radius seems to vary with the LOA
which in turn varies with the LWL. For comparison's sake an cverae raaius of gyration of 21.5 percent LWL wasused for all the models. In addition, two
additional radii of gyration were
cho-sen, one 10 percent larger and one 10
percent smaller. The principal result was that for a 10-percent increase in
radius of gyration a 10-percent
in-crease of added resistance was found.
The added resistance versus
dis-placement is plotted in Figure 6. From this graph we noted that the added re-sistance goes down with the displace-ment. In addition, it seems to vary with
the beam. The bearnier model has
more resistance than
the narrowermodel. This ditterenco is worse at
lower speeds and diminishes more orless in the high-speed range.
Model one seemed to have more
added resistance than the othermod-els. The reason for this could have
been her relative fineness at stations one-halt and one, just forward of the drastic displacement increase alsta-tion two. The fine entry provides
minimal damping of
motion and
Mo3t
of the odd
shapes actually
bLt have been
imsuccesfu pariy
becau
of
tm-predkbbk scie
effects with th use
of sm
mackls
RTS!Vs
22
20
seemed to be the cause of the extra
added resistance. The last model had
relatively less added resistance than
the other models. This was caused by
her having more displacement in the bow with steeper profile in this area than ay other model. In absolute sea-keeping values
it appeared that the
lightest model (model four) was the
best of all according fo the computer.
However, in the test tank, although the very light model did not quite live up to expectations in performance, it
- 12
Upright resistance vs Displacement
Vs= 4,5MI5
54 58 62 66 '- 70
i i I i t I I i t
Displacement in pounds
showed that we were going in the right
direction. Model tour was a rather big
step towards lighter displacement.
This step was necessary to investigate
the much-discussed
light-displace-ment concept as well as trying to find a lower displacement limit.
From the resistance studies
'concluded that the optimum
displace-ment should be around 58,000
pounds. Model five was of a design
having this displacement. The ratingparameters were chosen based ort
s,tudies done by computer. The sailarea was increased by four percent
over Southern Cross
for improved light-air performance. From thevari-ous studies we decided to take a
freeboard penalty of 15 cm. Lowering the freeboard would increase the
sta-bility by towering the centre of gravity,
decreasing heeling moment decreas-ing of the heeldecreas-ing arm (for similar sail area), reduction of wind resistance of
the hull, and reducing gyradius for
improved rough-water performance.The chain girth was kept loa minimum
while the midship section was
devel-oped using the stability parameters
graph.
At the same time we designed the sixth and last model. The rule 'length" and freeboard were kept the same as
i t e
io
8
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2O CZ CZ''l
3.90 CZ 3.45 3.00model five. This model was slightly
more radical in hull shape and slightly heavier. The bow was made steeper,thus tilling the forward stations with
more displacement farther below the waterline. The reason for this was an expected rough-wafer improvement.The rest of the hufl was much more
veed than the other models. All other parameters were developed from thevarious graphs used in the design
sys-tem. Making an additional model
allowed us to study within reasonable displacemont and stability limits two
rather opposite hull shapes.
The keel has two principal jobs:
keeping the boat from going sideways;
and providing a place for the ballast
necessary for low centre of gravity.
From the first model tests model
three appeared to have the smallestleeway angle. Model two made about 10 percent more leeway. Model one made about 20 percent more leeway
than model three over the whole
Operating range.To get a handle on what size keel is needed, we used a calculation method based on the test results as well as
vari-ous papers and theories of
aerody-namics and fluid dyaerody-namics. This
method calculates the theoretical side force developed by both keel andrud.., rr'
-der. The same total results for side
force were measured in the tank in aspecial series of tests. From testing
model nne appeared to develop about
11 percent less total side force than
both models two and three. This
allowed for the big rudder on model one. From the calculation method the
same total difference was found.
This diflerence can be further
ana-lysed with the calculation method.
Allowing for the bigger rudder, the keel
for model one was producing 15 per-cent less side force than the keel of
model three for a constant
speed-length ratio. At the same speed for
model three as model one this
dif-ference increased to about 20 percent.
The keel appeared the main tool for
controlling side force and thus leeway.
Any deviation in
side force in
thecalculation method was therefore
as-sumed to give a similar percent devia-tion on the leeway angle.
The rudder we see only as a means
of controlling the direction of the boat
and not for controlling leeway. A large skeg and rudder combination
theoreti-cally would be more efficient with a
smaller keel to obtain the required side force. However, a combination like this does not allow a boat to turn quickly, a
very important factor
in successfulmatch racing. This combinatìon was therefore not considered. The larger
leeway on model one increased the in-duced drag of the model and is one of
the main reasons for the difference in windward performance between model one and three.
To aid stability one should like the biggest possible koel for a low centre
of gravity. Lengthening the keel
in-creases the induced drag while at thesame time increasing the wetted area.
The exact happy medium is difficult to predict. However, with the calculating method as a guide, we were able to
come within a few percent for this type of boat in plantorm area and leeway.
From the video tapes taken during
lank testing, we saw thatthe flat bottom
on model one is superior over the V-bottomed keels ofthe other designs. n the case of the flat bottom. hardly any crossflow occurred atthe tip, while the
crossflow on the V-bottomed keel was
very noticeable. In the calculation'
method this decreased the developed
side force by about iwo percent. An ad-vantage of the flat bottom is that it
low-ered the centré of gravity of the boat and therefore increased the stability and thus the windward performance. However, from the various tests it
ap-peared that a V-bottom seemed to give
less resistance and tended to
encour-age a vortex coming from the keel.
A comparison was made between
the most common airfoil
sections.Based on various investigations the
keel appeared to develop up to 50 per-cent of the total side force. This would
mean that the design section lift coef-ficient 1er 12-Metre keels varies
be-tween 0.10 and 0.15, favoring the
lower end of the scale. Factors that
helped to decide what type of sectionto use included tow drag, good lift
characteristics with and without trimtab, and relative centre of gravity loca-tion.
Among the many hydrodynamic
comparisons that were made, a few of the rnost.important are: sectional area
curves, longitudinal centre of
buoy-ancy(LCB), prismatic coefficient(PC). There were many possible shapesthat were considered good. When
comparing those curves, the keel is
taken oft and all areas were taken to the
farbody of the boat After testing the
first three models, we discovered a
no-table difference regarding the starting
point of the bow wave. At low and
medium speeds, the Southern Cross model showed the bow wave startingrelatively farther aft of station O than the other models. At very high speeds this
tendency was reversed.
The effective waterline length that a
hull sees in the water at various speeds
depends on the shape of the area
curve in the ends and not where theprofite of the hull intersects the
wa-143
r
r,
t. Added i esistance 4/VS vs Displacement Figures 4, 5 and 6:vs Tank- lest data for models
one Through four is plotted in these design curves for se/cc fing optimum values of beam and dis placement
o
-58 62 66 70 74x10
mt iii? iiili t_i li
i
I
terifle. The foIIowng approach to
cor-rect for the fullness of the area curves in the bow seemed to give sorno proof
and insight of this commonly
misun-deistood problem. One can draw
tangent lines at the area curves wherethe curve is two-and-a-half percent of
the maximum area(Fig. 7). The LWL of
Southern Cross would become about
three percent shorter while the best of
the other models would shorten the
LWL by about one percent. Theper-centages derived
inthis manner
agreed with the observations made on the various models.
The after ending of the area curves were all similar. The curves are steep
on the 12-Metre yachts in this area and no correction such as the one forward could be justified.
When studying the flow around the
afterbody we found that model one had
the cleanest flow with the least
turbu-lence.
Models two and three had
slightly more turbulence with fuller andshallower bushes, but this turbulence
did not seem to slow them down.
Successful yachts, 12-Metres as
well as medium and large ocean racing yachts, all have similar prismatic
coef-ficients and longitudinal centers of
buoyancy. Boats with the LCB forward tend to go better on running and reach-ing legs forsimilar POs. Boatswith high POs tend to go better in the high-speed
range with less driving power. For a
12-Metre this would be heavy weather reaching and running in winds over 25
knots. A high PC will hurt light and
moderate air performance anddown-wind performance in general.
Both LCB and PC are dependent on the shape of the area curves and have to be combined with those when com-paring them. In studyingfheareacurves
the LWL for model one was actually considerably shorter. AIowing for this,
LOB went relatively farther forward and
the PC went up drastically. This actu-ally says that Southern Cross should
be a good heavy-weather boat.
The upright resistance at all
com-mon sailing speeds were the highestfor model one: except at very high
speeds she was better than all
themodels. A general tendency was that
the heavy-displacement-type boat had
more favourable resistances per fon displacement than her lighter sister.
Model one had the best
ratio forLWL/BWL of all the models and with the heavy displacement should there-fore have better resistances per ton. Having a relatively higher PC and
far-ther forward LOB we reasoned that she therefore got her worst performance in
the regular operating speed range. The driving power as well as heeling torce of a boat is dependent on the rel-ative amount of sail. Each boat has an
ideal combination for a particular wind range.
lt was therefore important to
144
decide viheii the boat should perform
to her optimum.
For easy comparison, we plotted
ratios of sail area (SA) to wetted area (WA) and displacement against boatspeeds for various particular wind
speeds. As we have used different
scales for each model, small speed
curves for wind conditions were made by plotung boat speed agmnst relative
sail area. Downwind it was simple as each model went more quickly when
the sail area was increased.
lt wasclear that the lightest boat with the least
wetted area would be the fastest in
winds up to about 20 knots. Thereafter,
the length would start to count and
make the bigger boat faster.
Close-hauled, the problem was
more complicated as the stability
became an important factor. Bolow fiveknots of true wind, stability won't do
much but in winds of 12 to 14 knots, it is
critical. Decreasing the size of a boat by one percent allows an increase of
about two percent in sail area.
The resulting change in the absolute
values of the hull will be: First, a de-crease in stability because of loss of
We decided that
j9
cFispiacement
o1d be fvred
in liht ar
or çukher thckin.,
ber aCCerØ
ad better
rough-wi:er p&krmince
beam, loss of displacement, loss of
ballast with a rise in the centre of grav-ity of the boat. Second, a stabilgrav-ity loss occurs because the sail area increases
thus increasing the heeling moment
(sail area x heeling arm). With the vari-ous scale models the speeds could be
plotted against sail area ratios for a
wind condition. t clearly showed at achosen wind speed what the optimum size for the boat should be.
Reviewing the test results with dif-ferent scale models, we decided that
the chain girth was a 'killing" factor.
When we even arbitrarily tilled in thegamboards, the sail area could be
in-creased drastically improving
per-formance. This minimum chain girthhad to be taken lar any chosen
dis-placement. As the stability had to beincreased for the
lighter boat, thefreeboard penalty could be taken to
our advantage. Theoretically, in the
tank performance improved without
counting on surTh factors as windage, reduction of pitching radius, etc.
Speed Made Good (VMG) is one of
the iiiost important numbers when
test-ing. This VMG is the speed, including
leeway, yaw, etc. , that a boat actually
makes going to the weather mark. In
America's Cup racing 60 percent of the
race is to windward. If the opposition can be beaten to windward, one can
stay ahead on the other legs. The VMG was calculated by the computer at 10,
20 and 30 degrees of heel by balanc-ing all the torces and seekbalanc-ing the ap-timum. The VMG curve was obtained
by fairing a curve through the three
known points.
The flow around the aft part of the
hull in the busme and the keel is impar-tant. To make a detailed study, the first
three models were painted white, and small tufts about one inch long were
glued to the hull. A special underwater
video camera was set up. During the
runs we could see what was happening en a TV screen: and also recorded on a
video tape for later re-play and direct
comparisons between the various
models.
A number of selected runs were
made with the cameras in various
places. The runs included upright an-gles attive different speeds and underheel at 10, 20 and 30 degrees atthe
ex-pected boat sped with corresponding
leeway angle for
those conditions,covering in this way all realistic sailing possibilities.
The atterbodies of both two and
three were pulled
in to different degrees, because al the rudder stock being far forward. Model one, on theother hand, had the rudder well alt and
clean flowing buttock
lines. In theupright conditions two and three had
considerable turbulence around the
rudder stock, and at speeds of seven to
eight knots this turbulence would
ex-tend about four to five feet aft in full
size. The part of the rudder extendedbelow the skeg had little turbulence
and seemed to be efficient as a control surface.
Model one,
in contrast, had little
turbulence in the rudder-stock area athigh speeds as well as at low speeds in
upright condihons. However, at the
middle and upper speed range, turbu-lence started to occur close to the
rud-der tip. This appeared again unrud-der
heeled conditions, apparently from a'/ortex coming from the keel.
This turbulence did not appear on the other models because of their shallower rud-der. On all models there seemed to bea strong crossflow going under the
counter directly aft of the rudders under heeled conditions.
Another noticeable difference was at
the keel tips. A tip crossf low was
ap-parent on model three, and tufts
started to change direction as high as two feet above the knuckle line in the
torward part of the keel. On model one,
on the other hand, the crosstlow did
not start until about one toot above the
condi-e;
io
8
2
lions.. Model two had crossflow some-where in between. For similar draft this would mean that 15 to 20 percent of the draft of model three was not working as
efficiently as the keel of model one.
From this if could be concluded that
the flat-bottom ti would be better than the V-bottom tip. However, other
fac-tors were also involved that do not
make this decision this simple.
The final model (model five) was
some 8,000 pounds lighter in
displace-ment and with about 70 square feet
more sail area than Southern Cross. In Figure 8the VMD curves are plotted for
both Southern Cross and Australia in both smooth water and rough water. From the graph note that a large gain has been made in rough-water
per-formance in light airs. In a simulated
T7iïi>
100%LWL.America's Cup race of, say, 12 knots
(first race of 1974 series) Australia
would be 0.06 m/sec. faster than
Southern Cross, 50 seconds on a 42-mile windward leg. Downwind in the same breeze, Australia would be 37
seconds faster than Southern Cross on
a 4k-mile leg.
In Figure 1 Australia s
superim-posed on Southern Cross to show the basic dìfferences. The new boat is a lot
smaller than Southern Cross.
Howev-er, it should be pointed ouf that the new boat is only faster up to about 20 knots of breeze.
If you could be certain
itwould be blowing, Southern Cross
would be the boat to take to Newport.
In conclusion, we would like to say
that we do have a potentially fast West
Australian challenger. However, the
Figure 7: Construction of langent line to section area curve
used to predict apparent shortening of waterline length
Figure 8:
Speed made-good
curves showing the Australia superior to Southern Cross sai/in g to windward in true wind speeds
opto lOm/sec
(79.42 knots)
Dutch designer Johan Va/cnt/ja worked for Sparkman arid Stephens in New York before join/n g in partnership
with Australian designer Bob Miller.
The new West Australian 12-Meter
Australia is their first major
project-Ed. 145
L
waor Smooth'ï!
, -Rough waler coss Australaopposition will also have worked hard to have a faster defender and mign make the final competitors similar n boat speed.
To win the Arrierica's Cup the next
step is to match sails, organisation.
crew work, etc., with the deten dens and
to out-perform them. The opposition should never be underestimated and especially in such a prestigious series
as the America's Cup.
V
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