IN WAVES OF TWO .WIGLEY HULL FORMS.
Prof. ir. J. Gerritsma Report No. 804
Motions,, wave loads and added res;istance in waves of two Wig.iey hull forms.
Prof. ir. J. Ge.rritsma
1.
Introduction
Model experiments with two mathematically defined hull forms
to determjne the motions, wave loads and added resistance in
regular head waves has been carri.ed out In addition forced oscillation experiments, in the heave and pitch mode have been performed to determine hydr'odynamic mass a.n4 damping. Th'eculations of the.dyn'ami.c. behaviour of such hul.l forms in waves.
2.. The models
The hull form of both models is givenby':'
= (i-c2).(l2).(l+o.2E2) + ç2(lç'8)(l2)4
Two length-beam ratio's have been considered: L/B = 5 a.n4 L/B 10
The main dimensions of both models are given in Table 1 and
a body plan is given in Figure 1 for the
L/B 10 model.3'.
Model experiments
3. 1 Model 241
.3."l.lMotjon 'characteristiCs and''addedres:js'tan'ce
The. 'mot'ionamplitudev and' phase characteristics have been measured -n r;eguia'r.h':ead waves.. In case of the
narrow .beam model nr..241 th.re.e model speeds have been considered..,: corresponding to Fn = 0.2, 0.3 and 0.4. The measured results for pitch.,, heave and added
resis-tance are given in Table 2.
As a reference fo.r the added r'ess.tance values the
still water, r'e,is'ta'nce is. given in table 3.
The amplitude and phase characteristics of heave and
pitch are given in the Figures 2 and 3.The measured added resistance is very small relative to the corresponding stil.1 water values and a few neg'atie values' a:re observed'. 'These are not included
in Figure 4, where the added resistance is plotted on a' base. of wave I ength ratio.
The accuracy of the added resistance measurements
with this iiärr'ow b'eam mo'de.l-i,s r-a'the r po.o r ,a:n.d these datash.o-u-1-d_be cansidered with care.
-height of aproximately a factor 2. The observed motion
amplitudes are almost linear with respect to
wave
height within this range, as shown in th.e Table 2.
3.1.2 Wave loads
In Tables 4,
5 and 6,
as well as in the Figures 5,
6,
and 7 the heave force and the pitch moment as measured
on the restrained model are given as a function of
wave length rat:io for three forward 'speeds.
Also the
phase lags of heave force and pitch moment
are
inclu-ded in these figures.
i.-l.-3Hydrodynamicuiass'anddampjng
Forced oscillation tests have -been, carried out to
det:er.min'e -added mass ;r
of
inertia -and:t'he co.upi'inig .co effi'c i ent's-i.n:theequat ions
of'motion of heave and pitch.
Also 'in, this 'case'"three
'have-been
con-s i.dered, acon-s well a'ria:n'geof frequenciecon-s.'
"-The equations of motion are given by:
+ bz + cz + d99 + eO + gO
F (heave)
a090 + b06
+ c990 + do,z + 'e9'.z + g9z
M (pitch)
The coefficients a, b,
d and e are tabulated in
dimen-:-sionless form jn the Tables 7 and 8 and the
corres
ponding Figures '8
-15.
The experiments have been carried out for
two
ampli-tudes of motion':
Za = 0.025 m.,
0.050 m and 0a = 0.026 rad, 0.052 rad.
A very, satisfactory iiñea-ri-ty.'.-in-:this--.ra'n'ge could be
ob se;ryed. The ,non
iinen:s.j,ona1. coé ffici'ént.s - ua're defined
as follows:
=.
a/pV
=* (L/g)½'/p:V
do/pVL
ee,z *
(L/g),½/pVL
ä99/pVL2
b90 * (L/g)½/pVL2
dz0/pVL
ezO * (L/g),½/pgL
= -- 2 -= =abo
=bbo
=d9
=e9
=3.2 Model 253.
A s,iinular set of experiments has been carried out for model 253, which has. the same form coefficients. as
model 241.
Model 253 has. a length-beam ratio. . L/B = 5.
However only one model speed, corresponding to F-n =. 0.2 has been considered in this case, because for
h.ighe,r Froude numbers t-he waves generated by th,e model
are. quit.e extreme.
The measured pitch and heave, as well
a:s addedregis-tance is given in.Table 9.
For Fn .= 0.2 the still, water resis-t'ance is 5.98 N, as
a reference f-or'. the -.e's'istan'ce values in waves. -The corresponding. figu-re.s are.:
Figure L6 'for -heave.-
-Figure 17 Lor pitch
Figure 1-8 .-for...adde-d resistance
Wave force and moment, as mea.sured on the -r'estrai.ne-.d model is given in Table 10 and Figure 19.
Finally the experimental values fo.r added mass., added.
mass- moment of inertia, damping- and c-ross. coupling coefficients are tabulated in Table 11 and 12.
The. corresponding figures give the values for. t-he coefficient1s of the equation's of motion Orfl a base' of frequency w'
.Figur.e 20:, added. mass atid damping coefficient. -for heave
Figure- .21-::--cro.ss .:coupli-ng'..-coef.fi.c.i.ents-. for heave
Figur-e .22 :-.'added. mass. moment of inertia a-nd dampi.ng-coeffi'cient.-for-pitc.h
.Figure .2-3: cross c-oupiing- coefficients .for p-itch
4.
Acknowledgement
The experiments and the data reduction- have been carried out
Main dimensions of models Modelnr. 241 253 L (ni) 3.00 3.00 B (in) 0.30 0.60 T (rn) 0.1875 H 0.1875 V (rn3) 0.09462 0.18920 (rn) 0.75 0.75 GK (rn) 0.1875 0.1875 CM 0.909 0.909 L/B 10 5
Table 2
Pitch and Wave Characteristics Added Resistance MOdel 241 Fn. A/L RAW (N) .za/ca
6zç
(de.gr)6eç
(de.gr) RAW*L, (cm) 21r.ca pgB2ç 0.2L00
0.62 1.17 - 41 L2'O -194 16.0 H 1.15:03
1.00 0.09 0.61 -116057
-228 2.2 1.18 0.4 1.00 1.25 -0.85 0.45 0.30 0.86 -149 ., -. 2 0.27 1.65 -248 -.124 -21.5 11.4 .1.16 1.1.6 0.3. 1.25 0:8.1238
- :58 H 1.34 -193 22.0 1.12 0.4 0.2 .1.25. 1.50 -0.83 H 0.2:0 1.57 0.96 H -119 - 6. : 0.79 1,.i3. 2i9 -:104 -.25.6, 4.0 1.05 1.30 0.3 H1..50 0.8:6 1.56 0: 2. oO: -137 .1.6.3 1.34 0.4 1.50 .: 0.4.1. 3.3L - 60 .' .1.28.. -179 8.3 1.30 0.2 1.75 0.0:2 0.97 1..:09 . -100 0.3 1.55 H 0.3 1.75 0.3.5 11.21 0 1.34 -110 . 5.6 : 1.46 0.4175
0.26 2.50 - 7 1.35 -161 3.7 1.54 0.2 0.75 . 0.00 0.13 6.8 0.23 H -224 0.0 1.20 0.3. .0.75 -0.14 0.09 - 5.4 0.11 -239- 35
1.17 0.4 0.75 0.90.006
- 0.07 23.2 1.15 0.2 1.1.0 1.0.0 1.21 - 6 1.68 . -16.5 25..7 1.15 0.3 1.10 0.35 . 1.24 - 99 0.83 -214 9.3 . 1.13 0.4 1.10 -0.20 0.65 -135 0.42 -223- - 5.8 1.0:8 0.2 1.40 0.19 0.89 - 6 1.24 . -.106 3.8 1.3.0 0.3 1.40 1.29 :2.14 - 12 1.94 -163 27.6 1.26 0.4 1.40062 .3.03
- .8,2 1.26 . -189 14.9 1.19 0.2 1.6.0 -0.43. 0.96 0 0.95 - 9:9 H 7.5 1.;40 0 3 1 60 0 31 1 27 0 1 58 -116 5 4 1 40 0..4 1.60 -0.03 .3.07 - 36 1.16 -171 H - 0.5 1.37 2.00 -0.03 .0.99 .0 0.68 - 95 0.4 1.54 0.3 2.0:0 0.08 .1.18 .0 '. 0.88 -101 1.2 1.52 0...4 .2.00 -0.65 1.53 + .2. . '-].14 -. .9.8 .1.50 0.2 1.0.5 2.09 .1.3.2 . - 27 . 1.44 -.18.2 26.1 1.65 '0.2 1.0'S .0.99 1.29 19 145 . -1.75 '25.5 .H .1.15 0.2 1.05 0.42 1.31 - 17 . 1.49 ;-.175 .. 31.8 0.67 0.3 1.25 , 1.74. 2.31 - .59 1.3:4 -19.3 2.3.1 1.60 0.3 0.4 1.25 1.50 0.14. 0.11 2.52 : 3.35 - '58 0 1.39. 1.20 I95 -.11.3 5.6 0.65' 0.82 0.4 1.50 -0.5.4 3.54 0 '1.2.8 - -2:0.4 0.95Still water resistance Model 241
Fn 0.2 0.3 0.4
RT (N) 3.79 9.80 25.96
Table 4
Wave force and moment Fn - 0.2 Model 241 Fn ca cm L/A Fa Ma 6(pç degr Mç degr
pgAc
pgIkç
* 1o3 * io3 0.2 2.80 1.00 140 282 38 -113 0.2 2.55 0.80 . 275 403 28 -106 0.2 2.45 0.50 540 .635 8 - 89 0.2 2.55 1.33 70 108 15.8 -122 0.2 4.60 1.00 149 272 40 -104 0.2 4.45 0.80 297 420 33 -107 0.2 4.30 0.67 402 504 22 -100 0!2 4.05057
506 611 18 81 0.2 3.90 0.50 545 660 14 - 70 0.2 4.70 1.3.3 71 103 160 -122 0.2 2.70 0.67 .397 512 2'2 . - 98 0.2 2.45 0.57 500 605 16 - 95Table 5
Wave force and moment Fn = 0.3 Model 241
Table 6
Wave force and moment Fn 0.4 Model 241
-7-Fn ca cm Fa Ma Fç degr degrpgAc
HpgIkc
*' io H*
0.3 2.75 1.00 163 296 43 -111 0.3 2.50 0.80 285 417 28 -119 0.3 2.55 0.57 480 576 17 - 90 0.3 2.40 0.50 572 665 10 - 86 0.3 2.5.0 1.33 98 126, 140 -112 0,3251
2.00 130 .30 177 119 O.3 4.70 1.0.0 1.72 '292. .48 -119 0.3 4.40 0.80 316 429 27 -.100 0.. 3. 4...27 0.67 415 537 25 -132 0.3 4.03 0.5.7 530 606 21 - 95 0.3 3.88 0.5.0 563 658 1.6 - 92 0.3 4.37 1.33 96 127 153 -130 0.3 1.81 0.67 415 46.4 21 , - 95 Fn a cm L/A Fa Ma '.. Fç de.gr . M,ç d'e.grpgAc
- pgi.kc. * io3 * 0.4 2.. 6.5 1.00 108 288 15 -120 0.4 2.60 0.80 327 395 21 -101 0.4 2.42 0.57 533 556 20 - 96 0.4 2.40 0.50 579 623 16 - 94 0.4 2.45 1.33 - 117 - -117 0.4 4.65 1.00 206 ' 284 30 . -12,0 0.4 4,40 0.80 363 412' , 27 -109 0.4 4.25 0.67 46i 489 ' 22 - 95 0.4 4.10 0.57 54.5 577 20 -100 0.4 3.95 0.50 608 636' 13 - 91 0.4 4.45 1.33 66 122 - -165 0,4 2.85 0.67 438 477 23 -111Added mass, damping- and cross coupling coefficients
Heave Model 241 Za '0.025 in Fnd9
e0
0.2 1.639 1.310 - .21,3 .311 1.659 0.3 .744 1.697 - .1.20 .110 1.659 0.4 .626 1.698 - .099 .125 1.659 0.2 .530 1.560 - .028 .048 2.21.203
.548 1.665 - 044 .088 2.21.2 0.4 .492 1.597 -.042 .115 2.21:2 0.2 .5.11 1.5.00 -.01.2 .048 2.765 0.3 .481 1.439 .-..016 .090 2.76.504
.464 .. 1.474 .. -.01.4 .1.1.6 .2.765 0.2 .450 1.2:89 . .002 .060 3.318 0.3 .465 1.262 .104 3.318 0.4 .454 ' 1.313 . .0:01 .125 .3.31.8 0.2 .452 . 1.0:54.07
.085 ' 3.871 0.3 .456 1.0c85 ..0,07 .128 3.871 0.4 .4.53 1.1.57 .01.0.44
3.871 0.2 .472 .824 . .0:07 .107 4.424 0.3 .472 .888 .009 .152 . 4.4.24 0.4 .462 .991 .01,3 ' .167 4.4.24 0.2 .548 .511 .005 .129 5.5.30 0.3 .536 .570 .007 .192 5.530 0.4 .508 .699 . .015 .212 ' 5.530 0.2' : .608 .389 .004 ' .136 '.' 6.636 0.3 .6C1 .446' .004 .204 .6.636 0.4 . 5.74 523 . .013 .246 6.636Table 7b
Added mass, damping- and cross coupling coefficients
Heave Model 241
Za = O05O
Fn a d,9 e.9 0.2 1.633. 1.35.2 - .21.6 .306 1.659 0.3 .798' 1.6.45 -'.118 .113 1.659 0.4 .675 1.726 - .105 .133 1.659 .0.2 .554 1.5.57 - .029 .050 .2.212 0.3 . .595 1.614 - .044 .093 2.212 0.4 .493 1.579 - .044 .118 . 2.21,2 0.2 .512 1.487. .- 013 .. 04.3 2.765 0.3 .4.89
1470
- .0'16 .089 . 2.765 0.4 .471 1.454 . -.015 ' .1.18 2.765 0.2 .454 .1. 302 :002 .059 . 3.318 0.3 .454 1.287.00l
102 ., 3.31:8 0.4 .446. 1.334 0 .126 3.31.8 0.2 .4.56 1.069 .007 .086 3.871 0.3 .460 1.C'94 .007 .127 3.871 0.4 .450 1.1,83 .009 .14.5 3.871 0.2 .471 .84,6 .007 .108 4..42403
.470 .904 .009 .158 4.424 0.4 .458 1,014 .013 .167 4.424 0.2 .568 . 54.8 003 . 179 5.530 0.3 . 561 ' . 595 .004 .196 5 5.30 0.4 .532 .728 .013 .220 5.530 0.2 .639 .437 , .0'Oi .188 6.636 0.3 .632 .483 .0.01 .207' 6.6.36 0.4 .597 .563 .010 .255 6.636.Added mass moment of inertia, damping- and
cross couplingcoefficient
Pitch model 241 0.026 rad
Fn a,9 b.9 0.2 ;0209 .047 - .003 - .087 3.866 0.3 .0235 .039 - .001 - .128 3.871 0.4 .0275 .031 .009. -.205 3.871 0.2 .0200 f 141 24O - .271 1.665 0. 3 .02 50 .068 . 136 - . 1.20 i.. 6 59 0.4 .0426 .044 .. 106 - .109 1.692 0.2 .0255 .056 .01.2 - 101 :2.21.2 0.3 .0236, .051 -' .0.53 - .076 2.212 0.4 .0333 .046 ...073 -.169 2.212 0,2 .O2i5 .051 .01:8 ..0:46. 2.765 0.3 .0233 .044 .024 -'.096 2.765 0.4. .0297 .037 .04.2 . -.164 2.760 0.2 .0214 .049 .00.1 -.062 3.324 0.3 .0236 .040 .007 - .103 3.32.4 0.4 .0:280 .032 . .020 - .181 3.324 0.2 .0206 .04.2 - .003 - .109 4.419
03
.0:234 .037 -0'03 -.154 4.424 0.4 .0271 .03.0 .0.04 - . 223' 4.424 0.2 .0217 .030 .000 - .126 5.530 0.3 .0;233 .03.2 - .001 - .188 5.530 0.4 .0364 .028 .005 - .263 5.536, 0.2. .0236 .024 0 - .131 . 6.647 0.3 .0246 .027 0 - .197 6.6:47 0.4 .0270 .025 .007 -.277 '6647Table. 8b
Adde,d mass moment of inertia, damping- and cross coupling
coefficient
Pitch Model 241. 0a = 0.052. rad
Fn
a9
b0
0.2 .0333 .147 .232 - .330 1.659 0.3 .0301 .0!66 .132 - .116 1.659 0.4 .0484 .0:60 .160 - .155 1.659 0.2 .0274 .056 .039 - .015 2.212 0.3 .0260 .050 .049 - .093 .2.212 0.4 .0356 .045 .073 - 16422l2
0.2 .0224 .050 018 -.046 2.771 0.3 .0244 .043 .025 - .09.3 2.765 0.4 .030.1 03.7 .038 - .162 2.771 0.2 .0220 .049 . ..O01 -.0:58 3.318 0.3 .024.1 .040 .00.6 - .104. 3.313 0.4 .0282 .03.3 . . .019 - .174 3.318 .0210 .046 - .003 - .088 3.876 0.3 .0239 .039. - .001 - .1.28 3.871 0.4 . .0278 .032 .009 - .1.93 3.866 0.2 .0209 .043 - .003 - .109 4.424 0.3 .0237 .038 -.003 -.152 4.430 0.4 .0273 .030 .006 - . 220 4,424 0.2 .022]. .032 0 - .126 5.536 0.3 .0239 .034 -.001 - .187 5.536 0.4 .0307 .005 .005 : -.259 5.536 0.2 . .0241 .026 .001 - . 130 6.636 0.3 . .0250 .028 .001 - .196 6,63604
. .0272 028 .006 - .274 6.631Pitch and Heave characteristics, Added Resistance
Model 253 Fn A/L Raw (N) za/ca z.ç degr OaL H degr RawL ca (cm)2ca
pg'B2c 0.2O75
0.90 0.12 -13 0.08 -183 2.1 1.91 0.2 0.90 1.06 0.30 -43 0.22 -165 2.5 1.9002
1.00 2.62 0.50 -49 0.35 -178 . 5.9 1.95 0.2 1.05 2.98 0.69 38 0.46 '-166 7.8 '1.80 0.2 1.15 3.55, 0.95 -26: 0.62 -154 9.6 1.77 .0.2, 1.20 3.02 1.03 -15 0.69 -147 .11.1 1.52 0.2, .1.25 4.15L06'
- '80.76-14.3
'9:8 .1.900.2.1.35
... :2.4.2.1.02 .0 .0.7.8. -1.25 7.6 1.65 0...2 1.5,0:: .1.79 .0.98: 6:..0,..71. -109 . .4.5 . 1.83 0'2H 1.75,, 1.0:2'. 0.93 '0.0.53
- 99 .2.2 1.97 0.2 2.00 0.6:8 0.98 ' . 9.0.43..- 93
.1.7 1.84 0.2 0.75 0.86 0.10 - 4 0.07 175. 1.1 . 2.54 0.2 0.90 2.06 0.28 -40. 0.21 -165 2.6 2.62 0.2 1.00 4.01 0.54 5'O 0.37 . 170 4.7 2.70 0.2 1.05. 5.34 0.71 -3.8 0.46 -160 5.8 2.80 0.2 1.15 6.59 0.96 -28 0.61 -15076
2.72 0.2 1.20759
1.05 -18 0.69 -145 ' 7.7 2.90 ' 0.2 1.2,5 7.18 1.09 -15 0.74 . -143 ' 7.6 2.83 0.2 1.35 5.67. 1.03 ' 0 0.77' -125 5.7 2.9'i 0.2 1.50 2.36. 0.97 '9 ' 0.70 -107 2.4 2.90 0.2 1.75 0.36 0.95 6 0.52 - 97 '0.4 2.8:3 0.2 2.00 -0.25 0.96 ' 4 0.45 ' -. 93. -0.3' .2.65Table 10
Wave. force and moment
Fn =0.2 Model 253 Fn ca cm L/A Fa Ma EFç H degr
Eç
.degrpgAc
p'gIkc H H * * 0.2 2.2:3 '0. 50 494 572 H 23 9.7 0.2 2.35 0.57 412 53:4 2.5 96 0.2 H 2.27 0.67 349 460 3.5 105 0.2 2.5.5 0.80 . 2.47 .347 '4.2 . 111 0.2 2.15 1.0O. 199. H '280 74 116 0.2 0.2, , 2.50 . 2,. 28. 1.3.3 2 .0.0 98' 79 H. .106 . '4.0 ., .155 .220 144 273:. 0.2 3.83' H 0.50 501 &09 .22 .96 0.2 4.12 ' 0.57 44.6 538 32 10.5 0.2 4.40067
3.55 4.56 38 10.8 0.2 4.50 . 0.80 . 263 365 50 113 0.,2 4.48 1.00 157 251 74 1.27 0...2 4.80 1.33 8'S 94 ' -184 -20.1 0.2 3.852O0
. 95 43 -101 -1.20Added mass, damping- and cross coupling coefficients
He ave Model 253 Fn d9.e9
Za 0.025 in 0.2 2.619 1.009 - .176 .619 1.646 0.2 1.041 2.820 - .032 .103 2.207 0.2 .989 2.256 - .019 .114 2.783 0.2 .907 1.949 .001 .137 3.341O2
.887 1.596 .010 .173 3.869 0.2: .939 1.237 .007 .201 .4.434 0.2 1.042 H .758 .00.5 H .229.' 5.492 .0.2 1i.73: .534 .002 .246 .6.636 Za = 0.050 m 0.. 2 2.791 1.261 - .213 .606 1.678 0.2 1.048 2.560 - .033 .107 2.22702
.996 2.264 - .020 .117 2.771 0.2 .912 1.986 0 .138 3.301 0.2 .908 1.588 .007 ,174 3.884 0.2 .949 1.237 .007 .206 4.445 0.2 1.08.2 .771 .004 .228 5.519Table 12
Added mass moment of Inertia, damping- and cross coupling
coeffic ien.ts Pitch Model 253 Fn
ag
b9
0a = 0.026 rad 0.2 .0.841 .192.190
- .631 1.658 0.2 .0305 .0.83 .042 . -.108 2.229 0.2 H .0194 :077 .027:-I24
.2766
0.2 .0160 .071 OO4 - .145 3:321 0.2 H. .0:1.36 .066 -.MO,3 -.179 3.86.9 0.2 .0122 .059 -.00.3 .209. 4.421 0.2 .0134 .0.42. -.00,1 -.239 . 5.56.3 0.. 2. . .0I48.. .029 .0 - .253 . 6.674 = 0.052..r'ad 0.2 .0:831 .1.93 .198 - .601i654
0 2 .0.331 . 080 .054 - 10;0 2 .2.11 0.2 .0.201 .077 .028 - .124 2.76.5 0.2 .0164 .071 .005 - .1.43 3.316 0.2 .0139 .066 - .003 - .179 3'.86502
.0.124 .059 - .004 - .208 4.428 0.2 .0129 .041 - .002 - .245 5.531 0.2. .016.4 .O27 .002. - .261 6.65.80.1 0.2 0.3 0.4 0.5 0.6 0.. 7 0.8 0.9 1.0
F,))
Figure 1. Body Plan of Wigley Model.with midship-area coefficient 0.909 and beam-length ratio 0.1.
-90 180 2.0 Za/1a
;$
.1.0 0 MODEL 241 HEAVE- OFn= 0.2
LFn = 0.3-
DFn=0.4
1.0Figure 2. Heave amplitude and phase model 241. 2.0 C, ec -180 AlL 1.0 1.5 MODEL 241 PITCH
.QFn.0.2
i?fl
0.3 OFti = 0.4 2.0Figure 3. Pitch amplitude and phase model 241.
0 1.0 1.5
AlL
2.0 0 1.0 1.5 2.0
0.5
1.0
1.5AlL
Figure 4. Added resistance model 241.
Fa/p gwCa Ma/p gI1kç
/
C.D w I I )0.5
1.0
1.5
Figure 5. Wave force and moment Fn = 0.2, model 241.
Figure 6. Wave force and moment Fn 0.3, model 241. 100
I
0.5100
Figure 7 Wave force and moment Fn = 0.4, model 241. 1.0 0.5
t
1.5 1.0 0.5 L/Azz 1.0 2.0 1.0 Fn = 0.3 .1 II 00 Fn = 0.2 OZa =0.025 m HEAVE MODEL 241 Za 0.050 m Fn = 0.3 Fn = 0.4
Figure 9. Heave damping coefficient.
Fn = 0.4
HEAVE MODEL 241 = 0.050 m
5 5 5
WI_____
Figure 8. Added mass.
0 5 0 5 0 5 U)' U)' WI Fn = 0.2 1 a' zz 0.5
d'
F
O. 5
-l..0
Fu = 0.2 = 0.3 Fn = 0.4
HEAVE MODEL 241 0 Za= 0.025 m
L Z=
0.050 m Figure 10. Mass cross coupling coefficient.0 Za= 0.025 in
HEAVE MODEL 241 L Za = 0.050 rn
Fn = 0.2 Fii = 0.3 Fn = 0.4
Figure 11. Damping cross coupling coefficient.
5 *10 -2.0 3.0 2.0 *10 1.0 ezO WI 0 5 5 0 5 5 0
* 100 6.0 4.0 '2. 0 Fn 0.2 J, 00 3
Figure .12. Addied mass moment o.f inertia..
Fn = 0.3 Pu = 0.4 PITCH MODEL 241 Oa 0.052 rad.
00
= 0.3
3
.5
Figure 11. PItch &ingeoefflcicnt.
= 0.4 L
IA)'
OOa = 0.026 rad.
PITCH MODEL 2.1 Oa =O.O52 .rad.
15 10 * 100 5 b' 0 0 0. 5
5.
0 5 0 5 0 0 5e'
Oz2.0
Oz -.0.5-1.0
-2.. 0-3.0
= 0.2
0Figure 14. Mass cross cOup1i.ng coefficient.
5;
OGa = 0.026 rad.
PITCH MODEL. 241 ,Oa 0.052 rad.
= 0.3
5
Figure 15. Damping cross coupling coeffIiWt.
= 0.4
5
w'I. 5
Fn 0.2. Fn = 0.3
PITCH MODEL 241. OGa = 0.026 rad., A'Oa = 0.052 rad. * 10
C Z 90 (degr) 180 20 0.5 1.0 0 0.5 A/L 1.5 2.0 Fn = 0.2
0a =
'i'0.018 m = '%O.028 in I - I -90 -180 (degr) OaL 20 10 0..5 0.5 1.0 1.5 I I -ILO
1.5 2.0 A/L 2.0 -FnO..2
OCa '10.018 I= 4.08
inFigure 16. Have amplitude and phase Figure 17. Pitch amplitude and phase
model 253. model 253.
1.0 1.5 2.0
Za" a 10
RAW. L
pgB2
Figure 18. Added resistance model 253.
100
I
0
Figure 19. Wave force and moment Fn = 0.2, model 253. 1.0 1.5 0.5 AlL 1.0 1.5 A/L
0.5 *10.
d0
-2.0 0 *10eO
Fn = 0.2, niodel 253. OZa = 0.025 m. Za = 0.050 m 2.0 P1.0 5 0 WIFigure 21.. Cross coupling coefficients Heave, Fn .0..2.,
Figure 22. Added mass moment of inertia .and damping coe.fficientPiitch, En 0.2, mode:1 253. 00a 0:.026 rad.
'Oa
'0052rad
*10 -1.0 -2.0Figure. 23. Cross àoup1ing coefficients. Pitch, En = 0.2, model 253.