HELLENIC INSTITUTE OF MARINE TECHNOLOGY
TECHNISCHE
UNIVERSITEff
Laboratorium voor
ScheepehYdrornechanlca
.Archlef
Mekelweg 2,2628
CD Oeft
TeL: O15786873
Fax 015. 781838
IFTH INTERNATIONAL CONGRESS
ON MM'1NE TECHNOLOGY
ATHENS '90
L
MAY 1990
q
HULL FLARE
INFLUENCE ON SHIP MOTIONS
IN WAVES
-R. Klshev, D. Radev
jgarial' Ship
HydrOflarnics Cerflre, Varna, BULGARIA
Y. Netzvetaev. Y. Kaitanou
lov &'ip Research Institute, Leningrad, USSR
In this
perce an atterpt ras been made to in-CII liane InÇ1uerCI.tritO practical skeepthQ withOut breattfl tee tradItiOnal motion
,yaluatiofl schemes. Renaming wLthiO the frame, o4 tee etrip theOry arid maU amplitude excitation,
the ccr,Site'S the waterline instanta
nØOUS ctaflfl' in the evaluatIon 04 the hydrostatic. inertia and O&mpifl forces. The added mass and
dar
ping terms, ottgiriClIY tiredeendant,are consice-railY simplifie0 by the ç.as-statiC (Io'. frequency) nçueptlO, whiCh converts tee dependence Ofl tine into dependence on instantaneCScraft, The approach
as brefl ver(:cO by lcrCeC oscillation tests of
floating cylindra «:th sh:rliie crosssections. as .11 as by sea) eerie; tests of ship models in steep nvas, the retu:td of which correlpte well with the calCulJtiDnG ettaifled by tnt ne'. technique.
NOr.EULATIJCO
-
instantaneous .e:titr.al creoa.. - sectional acre: mas,
- sectional Ca:ng :re4a:ieht d - instantaneo_5 graft
Diet - substantial 0CC
ivtve 000ratcr
F.
-
hydrcdyfla'nic fortes acttng en the Mull h - ocre hct;htk - wave number
1<. - coefficients of mOOed mass expansion on
instantaneous Craft - generali:ed mass values
- coefficients of damping expansion on Snstantaneous draft
- p?ocess el trie r.lative vertical motions
ge added resitnc..
-r
- perioc cf metbon
-- speed of advance
- process of ship notion at l-tC sode - sect:cnal otOth
- instantaneous wave elevation
- effective wave elevation accounting for
Smith effect
-- ave length
- nondimensienal ¿COtO resistance coeffiCient
Subscni ptai
O - fer equilib'ium position a - for amplituce
D - lar damping farces for inertia farce. R - for restoring fcrce5
I. INTRODUCTORY NOTES
- The
engineering
methods commonly used in shipmotion calculations, aro based an the assumptionS cf
smelt amplitudes and wallsided Niait fores. The mo-dern trends of development of iMp design.
lead to
unconventional
hull fare g tien with so-phisticated boo and stern geometry and well CevelO pod flare al-ong larQe portions of th. ship length. Another important issue Steins to be the raising ofthe operational demands, which farces the ship into more severe environment. The combination of these two factors mates the pplicatiOni cf standard linear motion theories doubtful and consequently imposes the involvement of
nonlinear
effects.On the other hanf, for pactical design
purpo-ses, simplified approaches are often preferable in vie.. of providing reasonable computing timeat nul-tirariarit calculations.
Thus, the ajo of the reportee investigation was the - development of a motion calculation procedure, idrich could account for the presenc. of flared hull sections remaining in the frames of the linear strip theory and it. subsequent realization as an option
to the mtandard seakeeping computer program.
2. SASIC FOPJtULATIONS
The motion of a slender ship with flared bow and stern sections,
advancing
in head regular steep waves, is considered.Folle.iing the assiin'ptien for aCditiVefless el
the forces acting on the ship hull, trim longitudinal motion equations are composed, as follows:
M.d. (t) - F.(tl F (tI F..(t) ill
i 3,2
It Is assumed further that the ship reactIons
remain linear and th. strip tr.eory is still aopli-Cable (2, thus the total forces on the hull can be
Obtained by integration cf corresponding sectional forces along the ship length. He , the fare. cur-vature. and the large amplitude relativo vertical motions at the ends require
consideration
of thein-stantaneous
waterline position in the farces evalua-tion. RccO.ding to 123, (43 and 123 tee forcecon-pa-nent.
in eq. Cl) ere expressed, as follows: F..it) - pg- -fD
[aesa,t
Drx(x,t) dt dt- Sasmie.tid6t5mit)_2m1t)'
(2) -(e,t)3s"'°de
-dt -F.oCtI da e -i 3,2.here, tP,e relative motion i. substitutCd by trie folioi.ing expression:
TECHNISCHE UNIVERSITEIT
Laboratorium ',00r
ScheepshydromecMa,ij
239
rchIef
Mekelweg 2, 28 cD Deift
TL O15-78N73.F
015.78183S
xtf
eleCt)
ç(e,t)
(3)
sectional
added esses
anddanping
are
jg-nalIy considered to be time-dependent.
_pUAS1STAT!C AFPROXIMATION ADDED MASSES ANDØADlP1
At lo
frequency assumption the .ectional added
and damping dependence oritime
cari be
re-ced to S0fli
quasi5t.tic function of instntafleous
sraft
afl(x,t)
-- bawls.d, U)
(4)-
a.0 *
mu
of this function was
investigated
in
(4 bytoo
series
of
4erce
oscillation
tests,
naul y!
small
anpltude
osciIlations
at
different
drafts C - (0.5
l.Z)d.;
large
anpltude oscillations with respect to
a0
processed
bynonhineal
identificatIon
technique.
--The
tests
were carried out on a nurber
edcy-lindrical bodies with flared cross sections
resenD-ling th bow bnd stern seattons of a 20 000 Ct fast
caritaiflerChip
sh..n
in Fig.!. The results Obtaiflel
in Fiç..2 and 3 she.. good
coincidence
betweenthe
-
e0perimental and tire theoretical quasistatic
estima-tians end the nonlinear identification., which allow
the
adaption
f an apprcaimate relationship of the
following type:
-K...Ca,u)
co.
- I(o(s,)[
The
form
of
ti-e
eoperirentally
obtained
'coefficient,
in
the
above qucraic erpansion Is
dunrcn,trate
in Figs. 4 and Z.
Qn tire basis of physical consideraticn,
it i.
a5!um,d
further on that the prjncial hydroc.?nanic
forces cOuld be eopressed. afollcws:
co,
- bo.,Cv,t)X..t)
-
f
a(e,tld
(7)
- !.
J
b(u,tgt
Sobstituti
of eq. CD) finally leads tos
- siOs)
IC(.,u)
(5)
- ho(is)
PJo(e,u)where, a. and b's are hydrodynamic added mass and
damping coefficients for the equilibrium draft.
Th, verification of the
aqoveespression.
is
demonstrated
in
Fiq.6,
wherethe
hatched
area
cover, the lOX fluctuations of the eeperimefltal data
around ihm
meansquared
value,
the
dotted
line
represent. a, and b5 calculations by the estended
Lewis form technique C13
andthe
dcircle,
give
the
correction,
to te calculated
value.
according to eq.(B). It
is clear that th, suggested
corretlon brings
the
calculations
in conformity
with
the averaged esiperimental values. Meanwhile, a
comparative analysis in Cf) proved
the
coincIdence
of the hydrodynamic coefficients prediction effected
by
the
different
techniques
(close
fit
andconformal mapping).
The
restoring
forces
could
becorrected
analogously,
considerIng
then
poportional
to
acertain sectional
idth y, which corresponds to the
ge increment of the cress section arpa for
oneperiod
of
motion
dueto the curvilinear section
shape.
4, PRACTICAL APPLICATION
The
main consequence of the above
ratiocinati-ons is that the standard linear ship notion theories
could be used for seaireepinq calculations in case of
complicate hull section forms atso, simply
bysub-stituting
the
a,a, b.. equilibrium values by
rele-vant corrected ones.
Practically, the procedure has been imple...ented
as an
option irtorporated in the standard seakee;ing
prediction program based on the l;near strIp
tnen-y
nethod
C3. The calculation :r:ces. is crçani:ed by
successive apprcnimations.
Initially, the
hydrodynan:c
coefficient,
andmotion
amplitudes
are
attained
by astandard
procedure
without
taking
consideration
of
the
eventual
section flare. Then, the amplitudes of the
relative vertical motion
are
evaluated
for
every
section
and for those with well developed flare the
espansion coefficients K, and N.
are
estimated
bylinear reçression of the corresponding values in the
region (do t r,_).
Thecorrected
added mass anddamping
coefficients
andthe
relevant
effettive
section
widths are suppli.d bacb in the calculation
scheme. The newly
obtained
notion
characteristic.
are
compared to the previous onus and if necessary,
the
procedure
is
rerun
until
saneprestribed
accuracy is reached.
(n C43
the announced engineering .pproa:h has
beenapplied
¿or
evaluation
of
the
seakeedlng
qualIties of a 20000 Cot fast containership .ho.v. in
Fig.!.
To- validate the procedure, ectended Ccberi
cents ..ere rarrted out in regular ..aves at different
wave steepness. The principal results have been
com-pared in t..o aspects
as linear frequency
response
(unction. (in Fig..B + lI) and as a direct
response-eocitetion
relationship
¡t
constant
f reouer.cy- (Fig.. 12 + ID).
In principle the
eepericental
result,
fellow
the
commontendency
al
response
decreasing
at
resonant area
arid- of
slight
increasing
at
high
frequencies.
Thesystematic
calculation.
clearly
-ha.. that
the
flare
accounting
leads
te better
fitting
of
tire
theoretical
andthe espertmental
predictions, though fo. tire
ship
investigated
the
- NwCo,u)
C (e, t) (Z)du
P4.(C,u)t
72.arsl0ß fra.
standard
nall-sid.d' pr.diCtlo.as
- are relat1&Y
5,.all.
me mcst
significant deviation 04 the
esperi-ntai pOittt5 from thu Un.ar response
secitation
is
observed
¿t Nigh 4reencies (short
o.t the absolute amplitude values
are
small
and
their
influent,
in forming the g.neral
thet'
ship b.h.Vi0" is minor. For
.t L. the linearity
e4,cton is retained for all reanenable values e:f nave
steepActS afld
the
samecan be stated for aver.;.
adr4 renistante dependence on squared wve
h.i;.'tt.
0, the5
grounds the application. of the tinear nt-ip
mith t,.aSlstLtital COrr,CtiO,ra 4cr predicting
5teePi1
qualities
of
flared
ship
hulls
is
juntifim
..u.
,.,u.U.
-Fag. 2 S.ctima.l added ..ss and CalnQ dependenc, ma instantaneous draft
(quasiatatital ape:achl
f 1Hz
SPip theery
X 0X7 s i
X00.io. JCXP(OIaiUII
Fag. 1 Pody-plan of to. 20000t. Centatnerahip
I. LSd. tfld.
tSj.
t.
/
/
Strip (hr,,y'
tall,
tra.. S.C.. REFERENCESFig. 3 Sectional added aus. and diede; dependence en instantSdteoul
draft
(dyfrealcil approachfinit. aeglittadel
t. 1.111. 1.211. tjW.
241
Athanassaulis G., Loukakis X., An
Estended Lutais
Fore Family of Snip Sections and Applications
to
Seakeeping Calculations - NTIJA, Athens, 0993.
9R., Elisgard F., Time History Simulation
of Vertical Motion and Loads on Ship
in
Regular
Head Waves of Lar;, Amplitude, NFR. No.2, 19go.
Boroday.!., Netzvetaev Y., Ship MotiOns In Waves,
Sudostroenie PubI. House, 1969.
Kishev R., Ra.v D., Hull Flare Influence on
Len-gitudinal
Motions in Engineering Seakeeping
Cal-culations, Final Project Report, BSHC, 1999.
S. Vuoramoto Yet al.,
Nonlinear
Ef4.ct
for
Ship
flç.
I
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S Co.ff.ci.nte in lb. quadratic annson of da.oing - Fig. 7 Flare influence onadded naos ¡077oa.ping
r
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R.pwc, - p.aito. 4 ba,. r.Iatj, ottOn
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liyeir theory
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linear theo.-y