VALTION TEKNILLINEN TUTKIMUSKESKUS TIEDOTTEITA STATENS TEKNISK FORSKNINGSCENTRL MEDDELANDEN TECHNICAL RESEARCH CENTRE OF FINLAND,RESEARCH NOTES
LAIVATEKNIIKAN LABORATORiO- SKEPPSTEKMS) LABORATORIET -SHIP LABORATORY
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VALTION TEKNILLINEN TUTKIMUSKESKUS TIEDOTTEITA STATENS TEKNISKA FORSKNINGSCENTRAL MEDDELANDEN TECHNICAL RESEARCH CENTRE OF FINLAN RESEARCH NOTES
ECHNISCHE
UNIVERJTFJT
Laboratorium
or
SCheepshydmecn
Arch let
Mekelweg 2,
2628 CD Deift
Tel' 015-78
Thomo Karppinen, Heikki Helasharju
& 5Ï'imo
MfF015.le183e
r
Irr
Seakeeping performance prediction
program SKP
Program manual
ESPOO 1988
1
rrniwY.
J.j A
tic3ci CD
tA
Valtion teknillinen tutkimuskeSkus, Tiedotteita
Statens tekniska
forskningscefltral, Meddelanden
Technical Research Centre
of Finland, Research Notes
Sakeepiflg performance
prediction
program
SKP
Program
ranua1
l'uomo Karppiflefl
Heikki Helasharju
Timo Aitta
Ship Laboratory
Espoo, February 1988
837
CONTENTS
F
APPENDICES Page
1. Method of curve fitting for frequency response
ABSTRACT and phase angle data
PREFACE 2. Wave spectral formulae
INTRODUCTION 8 3.. Default sea areas
9 4. Input/output example
2 BACKGROUND .
s. weibull probability function 2.1 Seakeeping performance indices.
6. List f primary variables
2.2 Percentage operability ...,.1
7. Input data card description
3 METHOD OF COMPUTATIONS 15
3.1 Ship responses to regular and irregular waves 15
3.2 Operability 18 4 SEAXEEPING CRITERIA
. ...22
4.1 General 22 4.2 Vertical acceleration 26 4.3 Lateral acceleration 27 4.4 Roll 29 4.5 S1mining 2946 Deck wetness
304.7 Operability limiting criteria - human factors 31
5 PROGRAM ORGANIZATION 35 6 INPUT DESCRIPTION 42 7 OUTPUT DESCRIPTION 44 8 PROGRAM VERIFICATION 46 9 CONCLUDING REMARKS 52 REFERENCES 54
i INTRODUCTION
In a seaway ship performance deteriorates as compared with the performance in calm water. This degradation of performance due to weather and wave induced motions may appear as an involuntary speed loss, -a voluntary speed reduction or as a lowered working effectiveness of ship
personnel. Violent motions may prevent essential work onboard thus causing lost working days.
The Nordic co-operative project '!SEAKEEPING PERFOR1(ANCE
OF SHIPS" dealt with various aspects of seakeeping
problems. The task of the
VTT Ship Laboratory in theproject was to find a general ranking system for
seakeeping performance of ships and to define limits to
acceptable wave induced motions. The operability limiting
criteria with regard to ship responses are used in the
procedure for predicting a numerical value for a seakeeping performance index. This index is in the
present work defined as the operability percentage and it
is used as an overall measure of merit or ranking for
seakeeping performance of ships.
The program manual consists of a description
of the
general background of seakeeping ranking systems and
especially the seakeeping performance index selected to be used in the project.
An outline of the
method ofcomputations
is given together with the
principles of selecting the operability limiting criteria ofthe various responses.
The structure of the program and the input data fleeded
are explained. The manual also gives a complete run as an example.
Finally the verification of the program is discussed and remarks concerning the present status of the program and
further modifications are dealt with.
2 BACKGROUND
2.1 Seakeepina performance indices
The practical evaluation of-, ship
seakeeping performance
requires a numerical index by
which to measure
theseakeeping performance. The index
should measure the
ability of the ship to fulfil its function in the environmental conditions the ship is
likely to encounter
in its lifetime or over a long-term
interval. Since the
effect
of the
seaway and weatheris- to degrade the
mission performance of the ship in
relation to the calm
sea performance, it seems natural
to formulate the
seakeeping performance index so that
it measures the performance degradation. 'The mission
performance in still
water is taken as a standard of reference.
It is important that a numerical
value for the index may
equally well be computed on the basis-of basic
seakeeping
model test data and theoretically
predicted ship responses. In seakeeping model
tests the number of speeds, headings and recorded responses
'is always limited
compared with, for example, theoretical
predictions-by a
computer. Thus the. measure of merit should
be such that a
numerical value -can 'be determined on the bas-is.of minimum
amount of data on the elemental motion components
of the
vessel. When more information
on the seakeepi-ng
characteristics of the vessel -accumalates, it should be
possible to update the value
of the seakeeping
performance index.
it has often been suggested that seakeeping
performance
of merchant ships cou-id
simply be measured
by theirability to maintain speed in heavy weather.
If the
measure of
merit is based on
the abilityto maintain
speed, the operational
ability may be
defined as the
ratio of the maximum speed in the'
r
condition to the maximum calm water speed, V. The
seakeeping performance index then becomes the ratio ôf the long-term speed ma seaway - the sustained sea speed - to V. The sustained sea speed reflects the ability of a merchant ship to fulfil its function, i.e. to deliver cargo and passengers safely and precisely from port to
port, regardless of sea conditions.
Procedures for predicting the sustained sea speed have
been presented by Chryssostomjdjs (1972), St. Denis
(1976), Journee & Meijers (1980) and amamoto (1984).
Kitazawa et al. (1975) consider the speed loss due to
voluntary speed reductions and Naito et al. (1980)
present a simple method to estimate the required speed reduction to keep the ship motions within the maximum
acceptable limits.
10
-In predicting the sustained sea speed both the involuntary speed loss due to added resistance and loss of propulsive efficiency caused by wind, waves and ship
motions and the voluntary speed reduction due to
excessive ship motions at the discretion of the ship's master should be considered. However, it is not usual in seakeeping model tests to measure all
the basic data
required for a prediction of the sustained sea speed.
Hosoda et al. (1983, 1984 and 1985) apply methods of
reliability engineering and define the operational
ability as the mission effectiveness. In rough seas the
mission effectiveness measures the rate at which the
mission of the ship can be accomplished in relation to
calm sea. In calm sea the mission effectiveness is
assumed equal to 100%. The mission.effectjveness concept is well suited for assessing the seakeeping performance when the efficiency of the personnel and equipment of the vessel are of primary importance in carrying out the task of the vessel. How to define the mission effectiveness of
a ship hull is not so clear.
ships. By naval
Hosoda et al. consider salvage missions by patrol boats and Lloyd & Hanson (1985) apply the misston effectiveness concept to the assessment of operational effectiveness of
shipborne naval helicopters.
2.2 Percentage onerability
in the present work the percentage of the time of
Operation has been taken as the measúrè of seakeeping performance. This meàsure of merit has often been applied to assessing Of the seakeeping performance of naval ships (e.g. Johnson et ai., (1979), Chilò & Sartori, (1979),
Bales, (1981.), McCreight & Stahl, (1:985), and Chilò et
al., (1986)), but as a comparative measure of seakeeping
performance it is equally well applicable to merchant ships this seakeeping performance index
expresses the percent of time the ship is capable
ofcertain operations according to its mission on a given
sea area over a long-term interval. The operational
capability of the vessel
is defined in terms of ship
motion limits. When ship responses exceed the limiting criteria, the operations cease. Thus,the index value expresses the percent of time the ship motions are smaller than the operability-limiting criteria.
By ordinary merchant ships the value of the seakeeping performance index at a particular speed and heading may be defined as the percent of time the ship is capable of
maintaining the speed and heading on a specific sea area. If only voluntary speed. reductions due to excessive ship motions are considered, this operation index can be computed for all ships on the basis of frequency response
functions and the phases of the various responses. If the
frequency response functions are known at several speeds and headings, all speed and heading combinations can be weighted according to their importance and the index value
is obtained as
a weighted mean.. If the added resistance and the propulsion efficiency in waves are12
-known, too, the effect of involuntary speed reduction -can be taken into account in the index value When the
percentage of operatIon is determined or several speeds up to the maximum calm water speed, it is possible to derive the average annual or seasonal speed, as shown by
Chilò- & Sartori (1979).
The basic steps in the procedure for predicting the
percentage of tine of operation at a particular speed and
heading are (Figure 2.1):
Transformation of -the experimental or
computed discrete frequency response data to continuous functions over the whoÏe relevant
frequency range.
computation of-the roôt mean square response amplitudes of the various responses in -wave
spectra with nodal wave periods over the
entire -period range.Selection of limiting response criteria and computation of the limiting significant wave
heights in each wave period group.
Computation of operability time in each wave
period group and in the whole sea area.
The numerical value -of the seakeeping performance index,
or the percentage operability in the specified
environ-ment at a given speed and heading is determined by:
P0(v,,i)=rP(T1;V:p) Q(T1) (2.1)
where P is the probability of significant wave -height not exceeding the operabi-lity-limit-ing value and Q is the
percentage of wave observations in the period range with
central period T1.
A more detailed desription of the
procedure is- presented in the next chapters.
- The final result, the percentage Operability Po,
should -not be considered as a -deterministic figure defining
exactly the. number of operational days in a year. The sea
13
-onditionB the ship encounters on a specific sea area
vary statistically from year to
year. statistical
uncertainty of the prediction is - furthér
increased for
instance by the human differences in the
characters of
ship masters.
The seakeeping performance index is best
suited for evaluating the seakeeping performance of alternative designs on a comparative basis, and for
revealing
possible problems in the seakeeping qualities of the vessel in the design phase.
14
-WAVE FREQUENCY WAVE FREQUENCY RESPONSE SPECTRA. S,.RS RMSft(.)dw WAVE FREQUENCY RMS, XX X-X LX LX WAVE SPECTRA H,lm T, = 3 ... 30 s CRITERION KAXIItJK ALLOWABIO PIlS VAlLE CRITERION RMS, PERCENTAGE OF OPERABILITY MODAL WAVE PERIODFigure 2.1. Principles f the prediction of the
percentage of operability time at a particular speed and
heading.
SIGNIFICANT SEA AREAY OPERABILITY LIMITING
WAVE HEIGHT Il, DUE TO RESPONSE X.
I
-
15-3 METHOD OF COMPDTATXON8
33. Ship responses to reqular and irreaular waves
in deriving the formulae for predicting the seakeeping performance index it has been assumed that the linear superposition principle and the Rayleigh distribution can
be used.
in spite of these, assumptions also the roll motïon was
included in the predictions.. 'Although the roll response
of most ships is non-linear,, at least at resonance, the operability limiting boundaries with regard to roll to be so low that the effeòt of
extrem ily important.
Applying the linear superposition principle and assuming the irregular waves to be unidirectional, the spectral
density of the ship response to waves can be found from:
'f
S,=IR(w)J. S(w)
(3.1)
where
w
is the wave or absolute frequency 5(w) is the wave spectral density andR(w) is the frequency response function i.e the
amplitude of the ship response. X in regular
wave of unit amplitude.
Here the ship response can be any of the linear responses
of the
ship to waves
such as heave, pitch, relativevertical motion, vertical velocity or acceleration.
When, the ship response is expressed as:
x=x0cos(w,+)
(3.2)'the frequency response function is obtained by:
R,(w)=x0/A(w)
(3.3)
non-linearities is
RES. AMPI. TRANSFER FUNCTIOII R
WAVE AMPI. RESPONSE X SPEED V kn
HEING: p deg.
seem not
AP
16
- I O.g.o. Co..oponds Io Hood Waoo
p - 90 O.goos Co'oopond. Io
i. - O D.g,.ss Co..000.'dI to Fcltow4ng Wr.00
PP
17
-Different frequency respòflse functions are obtained for
different ship speeds and headings. This cañ be indicated by writing the frequency response function in the form
R. (w;V.p)
The mean square value of the response. in irregular seas
is obtained as the area under the response spectrum function:
o-m0,=
f
S(w)dw
(3.5)
where
cia,
Is
the standard deviation, or root mean squareresponse.
The wave spectrum is here defined by an analytical
spectral density function such as the ISSC- or
JONSWAP-spectra:
S(w)=(A/w)eXp(-B/W)
(3.6)where the significant wave height, Hs can be factored out.
and the spectrum may be written in the form:
S(w). H
f(ùi;T)
(3.7)
The significant wave height is defined by
H,=4J
(3.8)
When the expressions (3.7) and (3.1) are combined for
g is the acceleration of gravity
(3.5), the mean square response can be written in the
p is the ship heading to waves (Figüre 3.1) following form:
V is the forward speed of the ship. .
02112f(R(w))2/(w;T)dw
H(g(T;V.P)2)
(3.9.)
I, - SURGE - HEAVE - PITCH- SWAY - OtL - YAW
Figure 3. l Definition of ship heading and notion components.
In 3.2 and 3.3
A is the àmplitude of the incident regular wave
w, is the frequency of encounter.
The frequency of encounter is related to the wave frequency by:
w,w_(w2/g)vcosp
(3.4)
where
g,(T;v,p) is the the root mean square response for unit significant wave height as a fúnction of wave
period: with ship speed and heading as
parameters
3.2 Operability
If the g functions have been determined,
the operability limiting significant wave heights for different types of
criteria with regard to linear ship responses can be
asily found.
For a criterion defined as the, maximum allowable root mean square valúe, as for instance for accelerations and angular motions, the Iimiting significant
wave height,
hx, is given by:
h,,(T;V,p.)= d,,,/g,,(T;V,p)
(3.10)
An alternative way to express the limiting criterion with
regard to response x is to define a maximum allowable probability for exceeding a critical value Xcr.
B' the Rayleigh distribution the probability of exceeding is
given by
P(x>
X,j= exp(-x,/2m0j<
P (3.1 I.)where P is, the prespecified maximum allowab)e exceedance
probability and inOx has been defined in (3.5). When (3.9)
is substituted for
Inox in (311), the limiting
significant wàve height can be' solved from the resulting
expression., and is thus obtained by:
X,,
h,,(T: V ;p)
(3.12)
g,,(T;V;p),J-2Inp,,
Equation (3.12) is equivalent to setting the maximum
permissible root mean square value to:
= x,,/j(-21npj
(3.13)
The criterion wjtI regard to deck wetness j5 most
conveniently expressed' in' terms of the maximum
permissi-ble probability,
dw :'---
-P(deck welness)- exp(_F2/2m0,) <'ed.,,
(3.14)
where 'F is the effective freeboard' at the section
considered and mor is the mean square relative vertical
motion. By (3.12) the limiting significant wave height
with 'regard to deck wetness can be expressed in the form:
hd,,(T;'1' ji)
F
g(T: V ,p),[-2ln
Pd,,(3.1i5)
where gr is the root mean square value of' relative
vertical motion' for unit signIficant wave height as a function of wave period with ship speed and heading as
parameters.
The slammIng criterion 'is conveniently defined in the same form as' the criterion for deck wetness.
By the Rayleigh d'isri'bution the' probability of slamming becomes (Ochi 1964)
P(slam)= ex'p(-d2/2m0,
+ V,/2m,,,) <P,,
(3.16)
where d
is local draft, Vcr Is the' critical re-entryvelocity and mor and rn0 are the mean square relative
motion and' relátive vel'oôity, respectively. tt follows
from (3.16) for, the limiting significant wave height with 'regard to slamming
hs(T;1/.P).j
2InP.{gg,)
(3.17)
where P5, is the maximum, permissible slamming probability
and g and g are the root mean square relative motion
and relative velocity for a unit significant wave' height, respectively.
f
fh(T)- H0\
P(T;V,M)P(He<h(T))
iH,-H0 ¡
where, 20
-When limiting significant wave heights have been
determined with regard to all critical responses as a
function of wave period, the hx(T) curves at a particular speed and. heading can be plotted on a wave scatter
diagram (Figure 2.1) expressing the joint probabilities of occurenCe for H5 and T in the operation area of the
ship. The operational boundary of the ship on the Hs - T
plane is obtained by taking the lowest of the limiting
significant wave heights at each wave period. In mathematical terms
h(T ;V ,p) m.in{h,(T;V p)) (3.1.8)
The probability of the significant wave height not
exceeding the operability limiting value h in each wave
period class can either be determined by counting directly from the wave scatter diagram or from the
Weibuli distribution fitted to the wave data in. each wave period class. When the Weibuil distribution is used, the probability of the significant wave
height
not. exceedingthe. operational iiiniting
height
in a particU1r wave
period range is given by
(3.19)
H0 is the lower limit of observed, significant
wave height for a specific period range are parameters to be determined by the fit
The percentage operability in the specified enviroinent at and heading speed the particular determined by: P.0(V,p)=).' P(T1;V.p) Q(T1) (3.20) can finally . be
where Q is the percentage of wave
observations in the
period range with central period Tj..
The foregoing procedure can ba repeated for
several
headingS .at .each speed jf
only the
0espondthg
frequency response fuflctiOfl5 are known.
The
percent-age operabiÏltY becomes
the weighted mear1 over all
eadiflg5 and speed&
p0(Oceafl area)'
(ii) j(v1 v)
P.O(1'kP')Here
is the conditional
frequency distribution of
hading at a given ship speed and'
j,, is the frequency
distribution of speed',
Both frequencY ,djstribution5
are to be defined' in
accordance with the mission
profile of the
ship. Theprocedure can easilY be extended to
include several ocean
areas with different wave, climates.
4 8EAKEEp
CRITE1IA
Criteria for acceptable levels of ship
motions, Which are used in the
procedure of predicting
the percentage of
operability, have been defined on the basis of full-scale data and
criteria proposed in the literature. The
information available has been
supplemented with our own
.bservatjons during
full-scale tests with small naval
vessels
In generai,
speed is reduced,
operations are discontinued if personnel is in danger, the
personnel has remarkably
dropped
is
signifjcantiy reduced. The captaj are:
a)
excessive. vertical and lateral
b,) slamming
deck wetness
rolling.
screw racing.
All ship responses are not
equally important from the
point of view of different ship
subsystems as shown in
Table 4.1.
For instance,
vertica'i velocity is important only from
the point of
view of helicopterrecovery and lifting operations while
vertical acceleration has an effect on almost all activities
onboard. In the operability
predjctjo procedure
criteria have been defined with
regard to all
responses marked with # in Table 4.1.
A
criterion with regard to pitch has
not been considered necessary since ofl
merchant ships large pitch angles as such are
Usually not a problem.
The effects of pitch that course is changed, or
the ship, cargo or
effectivenéss of the or habitability onboard main concerns of the
accelerations
may be experienced
onboard. are accounted for by thecriteria with regard to slamming, deck wetness and vertical acceleration;
No limiting level has been
set for the frequency ofpropeller emergence. There is little information
available on screw racing in full scale and lt is not
quite evident how propeller emergence or racing should bedefined in the prediction.
The basic set of criteria used in
theoperablity
prediction procedure are given in Table 4.2.
The slamming and deck wetness criteria have been defined in terms of critical probability (events per hundred wave encounters) while all other criteria are root mean square
values. The different points ôf view considered in
estimating the limiting magnitudes of ship motions given
in Table 4.2 are presented in Table 4.3.
Thus, in defining the critical level of vertical
acceleratioñ at the forward perpendicular (FI) safety of ship hull and cargo, in general, have been considered.
The acceptable level of vertical acceleration on the, bridge has been defined from the point of view of crew safety and performance. The roil and lateral acceleration criteria take into account the working conditions of the
ship personnel and the safety of the cargo.
From thepoint of view of equipment operation the critical
magnitudes of notion could probably
in most cases be
somewhat higher than in Table 4.2.
As can be seen in Table 4.2., a particular set of criteria has been defined for fast small craft.
24
-Table 4.1. Limiting criteria versus ship' subsystems.
Spècial' operations:
helicopter sonar
lifting
'1). 'For equipment on foredeck
2') For' deck .cargo
3)'For opératïons'on open lower decks
This has been done mainly to point out the different nature of the motions of small vessels at very high speeds. The linear methods used in determining the operabi1tY are not particularly well suited for seakeeping predictions of fast
small' craft.
-Table 4.2. Genera'l
operabilitY jmitiflg
criteria for ships.
Vert. aCC. riuS, FP
()
Vert. acC. riuS, bridge (g)Lat. ac. rius,
bridge (g)
Roll rius (deg-)
5lammiug, cri.t. probab.
peck wetn., cnt. prob.
0.275 0.2 0.1 4,. 0. 0.03 0.05 0.65 0.27 5 o.. 3. 4.0 0.03 0.05
Table 4.3. points of view
considered in the criteria.
Criterion
Vert. acceler. , FP Vert. acc., bridge
Lateral acC., bnidt5 Roll aiumiflg Deck wetness Ilul I safetY Equip. operat. Cargo safetY perSOflfl-safety and efficiency slam deck wetn. 01 vert. accl. lat. acci. roIl
I
pitch o o o o vert. mot. vert. veic. rel. mot. 0 SHIP SUBSYSTEM Ship hull Propulsion machinery Ship equip-ment Cargo Personnel effect. Passenger comfort o o o o o o o26
-In the case of fast craft also the numerical
values of the operability limiting criteria
are only directive. When a fast craft operates at a low speed the
criteria set for naval vessels should be used.
4.2 Vertical acceleratIon
Though ships do not
usually reduce speed or change course
as a result of high
vertical accelerations at the forward perpendicular criteria have been
defined also with regard to this motion parameter.
Criteria at the FP shoüld
be considered rather as criteria for comparing
seakeeping perforuance of' alternative designs than as limitIng criteria for
reducing speed or
changing course in actual' service., The
Vertical acceleration criterion at the FP
refïects the overall level of
vertical motion of the ship in weather conditions where slamming or deck wetness,
the primary reasons for a manoeuvre to reduce ship motions,
may be
critical. On the basis of the
published information it may be assumed that
the vertical acceleration criteria are more reliable than the
slamming and deck wetness criteria. As shown in Figure 4..l
for merchant ships the
operability limiting
ras vertical acceleration at the 'FP decreases with increasing ship length.
The critical acceleration boundary i's in close agreement with
Aertssen's (1968) proposal and correlates well
with later
full-scale observations as shown by Karppjnen
'& Aitta
(1986)
A spedial criterion' of O.;17g ras vertical
acceleration at
the FP has been
defined 'for vessels carrying ro/ro-cargo.
This limiting
magnitude of acceleration is based on the full-scale 'data 'by FerdinandO & De
Lembre '(1970) and Lindemann et ai. (1977).
27
-The criterion of 0.275g rus at the FP has c'
in comparisons of naval ship 'operabil4 (1981') and Walden & Grundsan (1985);
The high acceptable vertical acceìerationN small craft are due to the different frequency vertical accelerations on this type of vessels. 'o craft the acceleration spectrum is much wider and loca at higher frequencies than on displacement type vessejrk:
Hwnan bei'ngs tolerate high frequency vibrations much "better than low frequency motions as shown in Figure 4.3.
Usually also the mission of a fast, small craft is such that operations 'at high speed are only required for a short period of time making the high accelerations more
acceptable.
The criteria with regard to vertical acceleration on the bridge are intended only for basic work on the, bridge such as steering, observation and navigation. Criteria
for other types of work. onboard are proposed. later in
section 4.7.
4.3 Lateral acceieratior
The lateral acceleration criterion of 0;lg rus on the
bridge is equal to the U.S. Navy surface ship criterion estimated on the basis' of crew safety and' perforaance. This' motion limit, applies to such operations as transit and combat in general and underway replenishment. On thebasis of some
full-scale observations (Aertssen & vanSluys, 1972, and 'Hoffman, 1976) it seems that masters on merchant ships permit slightly higher lateral
004 I--J 0,03 002 -J V) -J t_j 001 I-t_J
-
28 -loo 200 LEÑGTh BTW PP Im)Figure 4.1; Criteria with regard to vertical acceleration
at the FP.
29
-The roll criterion for merchant ships
is mainly based on
full-scale data recorded on the same vessels as the data
used for estimating the limiting magnitude of vertical
acceleration at the FP. On the basis of safe footing, for
which the critical roll angle appears
to be about
14
degrees (St. 'Denis, 1976), and the fast
degradation of
human performance with increasing roll motion as summarized by Cox & Lloyd (1977), the operability
limiting ms roll angle could not be much higher than 6
degrees. Already at a degrees rms roll the probability
of
roll angle exceeding 14 degrees is more
than one
exceedanCe in five oscillations. A roll criterion around
4
degrees ms has often
been referred to as
an upperlimit to ensure maximum crew effectiveness onboard naval
vessels.
4.5 Slammiflq
The critical slamming probability, or the critical number
of slams per 100 wave encounters for merchant ships
is
shown in Figure 4.2 against length between
perpendicu-lars. The limit has been defined partly on the basis
of
published full-scale data and partly so that the
operability limiting wave heights obtained by applying the slamming criterion are sensible compared with the operational limits due to vertical acceleration at the
FP. In the operability predictions Ochi'S (1964)
definition of a slam is used. ccording to Ochi a bottom
impact is called a slam if the foreship
(approximately at
0.l5L abaft of the FP) emerges
from water
and the vertical velocity relative to watersurface at the station exceeds the critical valUe
V,,O.O93[7p
(4.1).Figure 4.2. critical slamming probability for merchant
ships.
300
loo - 200
30
-where g is acceleration due. to gravity and L is the
length-between perpendiculars in metric unIts.
On the average Ochj's formula for the critical re-entry
velocity is sound, but more precise definition of, the critical re-entry velocity would take into account at least the suspectibility
of the
forebody shape to slamming and the speed of the vessel. In fast small craft the slamming criterion should be applied with care.For passenger vessels the operability limiting wave height obtained by applying the bottom slamming criterion
may be
too high. The- comfort of the passengers mayrequire a speed, reduction or a course alteration already
on the
basis of whipping vibration induced by
flareslamming. Unfortunately the available data are too scarce for reliable defininjtjon of a criterion.wjth regard to
flare slamming.
4.6 Deck wetness
Like the slamming criterion also the deck wetness
criterion must be sed with deliberation for small craft.
On fast. vessels already thick spray may be an incentive
for a slow-down. In the operability predictions deck
wetness is defined to take place when at a particular station the amplitude of vertical relative motion exceeds
the freeboard. This definition does not distinguish
different degrees of deck wetness from spray to green
water.
It is also worth considering the effects of static and dynamic swell-up to the freeboard. Depending s-lightly on speed and forebody section shape they may considerably
affect the freeboard. No empirical formulae for
31
-corrections have been included in the present program. A survey of. the available methods has, been presented by Karppinen & Aittà (1986). -
-4.7 Oerabilitv limitino criteria - human factors
Depending on the mission of the ship the ability of the personnel to carry out a particular job may be critical from the, point of view of the' operability of the ship. Limiting criteria from the point of view of safety and working efficiency of' ship personnel and comfort of the passengers have been defined with regard to vertical and lateral acceleration and roll. Wheñ ship motion exceeds the limiting magnitúde at the work site, it is assumed that work is discontinued. Respectively, when the same takes place in the passenger spaces, it is assumed that
the operational boundary of the ship has beân reached.
The criteria with regard to ms vertical acceleration and
a short description of the corresponding working and .living 'conditions are given in Table 4.4. Sorne references
on the basis of whiòh the limiting magnitudes have been estimated. are also given ïn the same table'. Additional references can be found in Karppinen & Aitta (1986).
Table 4.4. Limiting criteria with regard to vertical acceleration.
Table 4.5 repeats the vertical
acceleration criteria and
shows the 0orrespofldiflg criteria
with regard to roll and
lateral acceleration which may
not be as reliable as the
vertical acceleration criteria.
Vertical ac-celerat ion 0. 20g o.isg o. log o.. 05g 0. 02g Lateral ac-céleration Roll (deg) 6.0 4.0 3.0 2.5 2.0 Description
Light manual work Heavy manual work Intellectu work Transit passengers
cruise liner
(performance) In terms of human effectiveness
critical motion levels for light
correspond approximatelY to an effectiveness
the scales of Hosoda & Kunitake
(1985) and
(1977). According to Lloyd
k Hanson
(1985)effectiveness may be related to
the time
complete a task in relation to the
time required
áondltiOns. Thus 50 % effectiveness
would imply that
task takes twice as long as in calm weather.
and heavy of 70 Cox '& the taken in human to calm the Vertical acc. rms Description
0.275g Simple light work. Most of the àttention must be devoted to keeping balance. Tolerable only for short periods on high speed craft.
Conolly (19.74),, Bakenhus(1980).
0.2g Light manual work to be carried out by people adapted to ship mottons. Not tolerable 'for longer periods. Causes quickly fatique. Mackay & Schmitke (1978), Applebee & Baitis
(1984)
0.15g 'Heavy manual work, for instance on fishing vessels and supply ships.
0.Ïg intellectual work by people not so well 'adapted to ship notions. For instance
scientific personnel on ocean research
vessels (Hutchison & Laibie, 1987). Work of a more demanding nature. Long-term tolerable for the crew according to Payne. (1976). The International Standard ISO 2631/3 (1985)' for half an hour exposure period for people unused to ship motions (Figure 4.3). 0.05g Passengers on a ferry. The International
Standard for two hours exposure period for people unused to ship motions. Causes symptoms of motion sickness (vomiting) in approximately 10 % of unacclimatized adults. Coto (1983), Lawther & Griffin (1986). 0.02g Passengers on a crüise liher. Older people.
Close to the lower treshold below which vomiting is unlikely to take place. Lawther & Griffin (1986)
32 - 33
-Criteria with regard to accelerations
and Table 4.5. roll. the work % on Lloyd
2,0 .! 1.6 1 . 1,25 1.0' 0,63 0.5 0,4 0,315 0,25 O,? 0.16 0,125 0.1 0,1 0,1a,16 4.3V
The sere
dlscosfort boÛndaryCCordi
to iflternati stndard ISO2631/3985
Withega
to acce1eraton as a functi0 of freq14for
POsUre times, of O minUto5 2 hOursand, tentativ
8The figure 4sa
Got0,5
(1983) Prop05 for a and of Iaboratoexpej
by
MccaUley
et al(976)
coresPondjflg tolo
iCkfle incide/ce ratjo (VOThltiflg) amongUad,t
health men. S PROGRAM.OROARIZATION-The Seakeeping Performance Prediction Program - program SKP -, begins the calculations with the basic data source of ship motions, i.e. the frequency response functions of
the different responses The final result is the
percentage operability time in the specified sea area at
one forward speed and heading angle.
The program has .a rather straightforward structure.- The main program serves as a control for -the job processing
calling the various subroutiñes as required. At present one run of the program involves computations in only one
unique condition defined by ship's load condition, speed-, heading to-waves and so forth.
The f-low chart of the main program is shown in Figure
5.1. in the f-low-chart the five - key positioned
subroutines are found:- INPUT, PAO, RNS, CRIT and OPERA. Various subroutines with more limited tasks are ca-lied by
these. The mutual order of the- main program and a-l--1 of
the subroutines is shown in Figure 5.-2.
The input data file is
read and
a-iso printed by thesubroutine INPUT. The input data may be categorized to-:
basic data such as -ship dimensions, F-roUde
number etc
frequency responsés of the different
measured (-or computed) responses in
discrete form as a fUnction
of circularfrequency
optional criteria for accelerations and -roll in addition to default criteria
wave data (scatter diagrams) of additional
sea areas.
-Figure 5.1. Flow chart of the main program. subroutine names are given in parantheses
and names of the
external files inside circles.
36
-fit a curve through frequency response
and phase angle data
(P.Ao)
compute wave spectral
densities and stOre
results, (WAVES)
compute rius responses (BNS)
set. criteria and cotn
pute limiting signif
icant wave heights (,CRIT) INFILE ma
0aUs
2 o . 5. . .- ---an8
Jo
-Table 5. 1,. Selection of
the responses included in the program.
Response
Heave
frequency response and phase angles Pitch
frequency response and phase angles
Vertical accéièration stations i -RoIl Reltjve motion i 2 3 Vertical accl. FP Vertical acceleration bridge Lateral acceleration bridge Vertical acci. St 1. Lateral acci. St i. Vertical accl. St 5. Lateral accl. St 5. Default criteria input criteria + + + + Note
no. crïterj set;
used to compute
ver-tical accelerations
computed vertical ac-celerations
for slamming for deck wetness
accelerations with frequency response as input
39
-Table 5.1 shows the scope of responses from which the
user may select the responses to be used in the operability calculations according to ship type and
frequency résponse data available. Note that instead of pitch and heave phase angles it is sufficient to know the phase difference betwéen pitch and heave in order to
compute the vertical accelerations at arbitrary cross
sectIons of the hull.
Discrete frequency response data are smopthed and nade continuous by.a polynomial fitting procedure. Subroutine RAO controls the procedure and calls subroutines .RAOFIT and RAOCOM, in which the actual fitting and a comparison between polynomial transfer functions and the
correspond-ing; input data are carried out.
-The evaluation of polynomial results is performed in
subroutine RAOVAL.
Súbroutine RAO' consist of successive loops.. Each loop
deals with data of an identical type of responses.
Subroutine RAOFÌT calls two. subroutines LIMFIT and REGR.
LIMFIT performes a least squares polynomial fit of third
order... ThIs prodedure is adapted to the first and last
piece of the curve to be fitted. SubroutIne REGR performes a linear least multiple variable general
regression analysis, which is used for fitting a fifth order polynom in
the mid section of the curve to be
fitted. Subroutines MINV and GMPRD are called by REGR for
matrix multiplications and inversions, respectively
The method of curve fitting is in detail described in
Appendix 1.
After the polynomial fit and checking of the results the
run proceeds with computations of root mean square
response amplitudes. The computations are performed in subroutine RMS, which calls subroutine RAOVAI to compute.
the frequency responses at the appropriate circular
40
-RuS also calls subroutine WAVES which
computes the wave
spectral densities with both issc and JONSWAP wave
spectral formulae for 15 seaways with unit Bignificant
wave height. The modal wave periods range from 3 to
30
seconds. Each seaway is defined by 50 spectral density values which are computed at frequencies with a fixed
relation to the modal wave frequency.
Descriptions of the wave spectra formulae are given in
Appendix 2.
Since the wave spectral densities, are a constant data
source for 'rifle computations, it is necessary
to use
subroutine WAVES only once in a specific computer
enviroment. The wave spectral density values are stored in a data file (WAVSCP). The data file is then utilized
during subsequent runs of the program SKP.
The next subroutine, CRIT, computes the limiting
significant wave heights as a
function of modal waveperiod. Criteria may partly be from data
sentences of the
program and partly determined by the user in the input data file. The structure of the subroutine CRIT is again
that of successIve loops organized according to the similarity of the character and units of the responses.
Finally the operability calculations are performed
by
subroutine OPERA. In the program there are wave data of
six sea 'areas as default data. The operability
calculations are automatically carried out at these six
locations. A suitable reference area for ships of various
size and type can be found from these six wave climâtes.
They also
form a rather continuous set from milder(Almagrundat) to heavier (North Atlantic/winter.) Wave
conditions. Appendix 3 deals wïth the default sea areas
more thoroughly.
The modal wave periods used in the différent
wave climate
data vary and do not match the modal wave
periods used in
the calculation of limiting
significant wave heights.
Therefore, first in the operability
calculétions an
interpolation is made
to make these
two data sources
coincide. A simple parapolic type interpolation
procedure
is adapted to the limiting
significant' wave height data
in subroutine ThYRA. Subroutines
TTOO1, TTOD2 and TT003
are called by KAYRA in order to perform the job.
After the interpolation the
lowest limiting significant
wave height at each modal wave period
(mid period of each
period rénge) is searched in subroutine AALTOM.
Once the limiting 'significant
wave heights are' found the
operability percentage within
each period group is
calculated by using the Weibüll coefficients stored
in
the data sentences of the program.
Subroutine KERTYM
performs the calculations.
The final results of the operability
calculations are
printed in subroutine TULOS.
The operability calculations are
repeated for new
seaareas if additional data in form of
scatter diagrams are
included in the input data file. The Weibull
fit is first
performed by subräutine WEIBULL.
A linear least squares
fit provided by subroutine
LINFIT (called by WEIBULL) is
used for the determination of the Weibul]. coefficients
of
each wave period group in each sea area.
Appendix 6 gives a list of the primary variables
used in
subroutines and also repeats a short
description of the
6 INPUT DESCRIPTION
42
-The first five data
cards specify the tit]e and transfer general information for running the program and' selecting the appropriate set of limiting criteria
with regard 'to
ship responses Most of the' rest used for defining the frequency
phase angles, which âre given
non-dimensional frequency :,
UJWJL/g (6.!)
The fitting procedure
requires at least il data points to work properly and up to 50 points can be used.
In the i'nput the
frequency response functions are defined in a non-dimensional
form according to table 6.1.
of the data cards are response functions and
as a' function of a
In the table
Z heave amplitude
O pitch amplitude
roll amplitude
p wave heading angle
-w circular frequency of encounter
A wave amplitude
4_3
-k wave number
r relative motion amplitude and
a acceleration, amplitude.
Asymptotic values of the responses for low and high frequencies are also shown i-n the table. Outside the frequency range covered by the input válues these asymptotic va-lues are used as òonstant frequency response
function valües in order to enable the computation of ras responses at all relevant frequencies. Asymptotic values
must be given in the input as the first and the last
value of the frequency response function. The X -' co-ordinates of the asymptotic valües must be selected by the user.
The phase angles of pitch and heave with respect to wave elevation must be given in degrees. Constant values at the beginning and end of the frequency range are used, and the va-lue of them is -to be selécted by the user. It
is a-iso possible- to leave the heave phases undefined and
instead give the phase difference of pitch with respect
to heave as an input.
All
frequency response and phase angle input must be
given in a rising order from l'ow to high frequencies. Note- alsO that thé fitting- procedure does not work if the
highest absolute value of Y input is found in the third
section 'of thé curve to 'be f itted 'In practice this may
take place only in case of phase angle -input. The data
should then be modified according to trigonometrical rules.
A detailed description of the input data file is given at
the end -of the manual in Appendix 7. Table 6.1 Input form definitions.
Response Form Low
freq. High 'freq. Heave Pitch Roll Relative mot. Accelerations Z / A,
O/kA
r, A
a/(wA)
1.0 Jcos/i J Sin (L o 1.0 o o o 2 o44
-7 OUTPUT DEBCRXPTXON
The output begins with the repeated input of general ship
datae frequency responses and phase angles.
After the polynomial fit a comparison is made
betweeninput and results computed with the polynomial expres-sions. A numerical goodness of fit is computed as the standard deviation:
2)1/2
(7.1)
where .Yi is the input and Yci the calculated frequency response value at frequency xj and N is the number of
X
-y pairs.Any negative values of frequency response results âfter the fit are shown in the comparative print-out. Later in the program, when computing the frequency response values for ms calculations, negative values are set equal to
zero.
The root mean square response amplitudes are printed out
as a function of modal wave period in the 15 wave spectra. Displacements are given in metres, angular
motions in degrees, and accelerations in fractions of the
acceleration of gravity, g.
The next sections of. output consist of limiting criteria and operability limiting significant wave heights for all responses, again as a functÌon of modal wave period.
The final rèsults give for each sea area the modal wave
periods (central periods of each period range), the
probäbility of occurrence of each period group Q(T), the ultimate limiting significant wave heights at each period
and the probabilitY of H9 > h in
period group Tj..
A limit for physiCallY
unrealistic wave height - period
combinations is used in the form
H9 = 0.1
Finally the weight of each group
considering the total
time and the total operabilitY
in the
sea area
arecomputed:
p(T,)*Q(T,) - p(V.) (7.2)
The results from Weibull fit for
additional sea areas are
printed also as part of the output. First the computed
cumulative probabilities P(x <
I1) in each period group
are compared with the source
distribution and then the
Weibull coefficients and the
correlation coefficient of
the least square fit (see
Appendix 5) are printed.
A complete example of output
After the approved to "Seakeeping program was laboratories difficulties ships and with' p heading 46 -8 PROGRp.j VERIFICATION
initial testing phase the
program SKP was
be used in the Nordjc co-operative
project
performance of ships". In the project the extensively used In
the four Nordic ship
which participated in the project. No major appeared during computations of
several raètica].iy taken all possible response, speed combinations.
The fitting of
frequency response datais of primary importance when considering the quality of
the final results, it was found that
the procedure developed for program SKP is quite
sufficient, for accuracy requirethents
in the rus response computations.
However, it should be
pointed out that the procedure is not very efficient
in
smoothing if the original data poInts have
considerable scatter. The user should
therefore drop out obviously
anomalous data Points.
At least 11 data points are needed for the
fitting
procedure to work, but usually 15 to
20 data points is
required for reasonab;e
representation of a complete frequency response curve.
Figure 8.,i shows a typical result of
a basic type of
curve to be fitted. The awkward changes, which are
typical to phase
angle curves, are not always very well
reproduced, but if the resulting computed vertical accelerations are compared with the ones directly measured the accuracy proves, to be quite
satisfying, Figure. 8.2 shows
representative results of this.
47
-Program SKP is able to produce rina response results quite
comparable with those measured directly in irregular
waves as illustrated in figures 8.2 - 8.4.
For obvioús reasons the f thai results can not be verified in the same way as the intermediate results above. None of the participating laboratories were able to represent any comparative data as far as operability results were. concerneth The results of the project are thus a first attemp to gather a data base of this type especially for
merchant ships.
The results of the NordiC co-operative project are
published by NORDFORSK in 1988. Some results of the
project were also featured in NSTM -87 A few examples of the information the latter part of the calculations give.
-
48 -1.0 2.0 3.0 NON-DIMENSIOÑAL FRED. 2 o 4Figure 8.1. An example of fitted results for relative
motion frequency response function. Original data
points s results of the polynomiai fit -o.
.15 O Io IO
-
49 -- COIPUIED BY 5KP FR04 FREQUENCY RESPONSE OVIA- - - CQUPUIED BY SOP FRQUPIICH
AND HEAVE DATA
5 MODEL TEST RESULT IN
IRREGULAR WAVES
IO 20
PEDAL WAVE PERIOD (S)
Figure 8.3. RMS response of relative motion.
-20 PDA). WAVE PERIOD (S)
Figure 8.4. RMS response of pitch..
.15
.10
.05
I 0.00
0.00 20 30
° DAL WAVE PERIOD (S)
FigUre 8.2. P14S response of vertical
acceleration!
-cc.IpUTED9V SOP FR04
FREQUENCY RESPONSE DATA
W MODEL TEST RESULT IN
IRREGULAR WAVES
0.0
30
- - - CCPIPUIED BY SOP FR04
FREQUENCY RESPONSE DATA
W MODEL TESI RESULTS IN
IRREGULAR WAVES .20 .10 0.00
j
e m,'D
3w
lì
3 ('Tz
o
0. u)j
ew
e\
Io 20 30 1.0 2.0 3.0 4 a>-o
z
o
w
LI./
/
50
-I
DECK WETNESS SLAMMING -- VERTICAL ACCL. AT FP ARTIFICIAL LIMIT FROMBREAKING WAVES 10 20MODAL WAVE PERIOD
(S)
Figure 8.5.
Operability limiting. signifjca wave heights
as a fUflctj of modal wave period
30
Froide m O.18 - O.t7
ioo.oc
80.00.
80
C
vwt ecc #'ite 0.1 gras et 0.0e.
-
.flcI - - -SWTHEAII ATU0
I1H ATUIITIC Iø!flI AT MaWon.m a
00
-. 80.00 -- 70 00 80.00 80 00 100.00 110.00 - LENGI4 (1Figure 8.6. Percentage of operability vs. ship length.
o 10 20 30 I, 1'O 70.00. 80 B0.00. 4000 80 00., 2000 10.00
9 CONCLUDING REHARK8
52
-The seakeeping performance prediction program - SKP - and the results gained in the project "Seakeeping performance of ships" form a good base for studying the quality of the seakeeping behaviour of new desings. The work should be carried on for even wider data base for ships of all
types.
The program was originally intended to perform
operabili-ty calculations of ordinary merchant ships,. There is also
a special branch of ships - such as dredgers, pipe
layers, crane ships, diving support vessels and so fourth - for which the operability limiting criteria are, often
defined differently. However, the structure of. the program SKP is such that the modification of the program in order to include new responses or to exchange oid to
new ones Is not a tedious work,
The program can thuseasily be adapted to even wider handling of operability
calculations of ships as well as other floating structures.
The program could further be developed by defining more specific operability limiting criteria to certain groups of special vessels such as passenger vessels, research
vessels,, supply ships, fishing vessels, patrol vessels
etc. To simplify the comparison of seakeeping performance of alternative ship designs even the stations where the criteria are applied could be, prespecified. This would also promote the formation of a data base against which
the seakeeping performanôe of new designs could be judged.
A deficiency of the program is that an operability limiting criterion with regard to fleur slamming is
missing. This should be added to the selection of the
criteria in the program as soon as
the level of flowiedge
of the phenomenon is sufficient.
The definition of a
conventi0n- bottom slamming should be
refined, to take
into account the
suspectthitY of the
forebOdY section
shape to 5amming. prediCtiofl9
of crew effectiveness in a
seaway, as defined by
beoda,
could easily be incorporated in the program.
intereSti aspect not considered
in, the akeepiflg
performance prediction procedure
is the probabil15t
nature of the seakeeping criteria
in reality. The
decision to slow down or
change course in rough
enviromental conditiOflS always depends
on the subjective
judgetnent of the captain, and
there always
are many
onflictiflg factors affecting
this decision. Further
study is required before the
5akeeping criteria may be
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LaborIng of Ships in
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Aertssen G. & van Sluys, ti.
F. 1972. Service
Performance and Seakeeping Trials on a Large
Container Ship.
Transactions RINA, Vol. 114. Pp. 429 - 447.
Applebee, T. R. &
Baitis, A. E. 1984.
Seakeeping Investigation of the U.S. Coast Guard 270-ft
Medium Endurance Class
Cutters: Sea Trials Aboard the USGC BEAR (WMEC 901). DTNSRDC Report No. SPD-1120.01. 67 p. Bakenhus, J. 1980. Ergebnisse von See-Erprobungen mit konventionellen und unkonventionel'len Schiffen.
Jahrbuch der SIG, 74'. Band. Pp. 23
-, 49.
Bales, N. K. 1981.
Optimum Freeboard:
A Critical Reassessment of the 'Balanced_Ship Concept.
Marine Technology 18, 3, pp. 264 - 275.
Chilò, B. & Sartorj,
G. 1979. Seakeeping
Merit Rating
Criteria Applied to Ship Design. mt. Shipbuilding.
Progress 26, 302,
pp. 29g - 313. Chilò, B.,, Sartori,
G. & Santos,, R.
1986. A New Methodolo9 Developed by CETENA to Assess the
Seakeeping Behaviour of Marine Vessels. Ocean Engineering 13, 3,
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Chryssostomidis, C. 1972..
Seakeeping Considerations
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Conolly, J. E. 1974.
Standards of Good
Seakeeping for Destroyers
and Frigates in Head Seas.
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Vehicles and Structured fri Waves, London, April,
Inst. of Mech. 'Eng. Pp. 59 - 67.
Cox, G. G.,, & Lloyd, A. R. 1977.
Hydrodynamfc Design Basis
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55
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r
Johnson, R. A., Caracostas, N. P. & Comstock, E. N. 1979. Ship System
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Journal of the Soc. of Naval Architects of
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Consequent Motion Sickness amongst Passengers. Ergonomics 29, 4, pp.
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À1
-Àppendix 1
Method of. curve fitting for frequency response and phase
angÏe data
Fitting a continuous curve through the discrete input values of frequency response or phase angle is performed
in three parts.
The first. part is a third oder least squares polynomial
fit with
avalue of the
first, input value and zeroderivative at the starting. point.
The number of data
points in the first fit is chosen as n1
2/3 * ïnaxrounded to the closest integer less than or equal to n1, where 1max is the index of the maximum y - value of the
data points. However, at least the first f iye data points are included in the first fit. In practice it is advisable .that especially in case of prominent resonance peaks in the frequency response data points should be
selected so that 1max is more than five.
The second pa.rt is a fifth order least squares polynomial
fit. The range is from' n1 -
1 to i3 + 2, where i3 is
selected so that 'at least 40 per cent of data points are between max and N, where N is the total number of data points'.The last part is again a third order polynomial fit wi'th a terminal value equal to the last input value and zero
derivative 'at the terminal point.
The computation of frequency response function values in order: to further compute the rms values is performed in
AÏ2
-Each of the three polynoms cover the appropriate non-dimensional frequency ranges, but in addition a
simpte matching procedure between them is adapted. The
width of matching
regions is taken as 20 % betweenX(imax) añd X1 and X(N) and X(inax) for joining the
first and second or second and third polynomial results,
respectively. The distance between two successive
original x data points is set as default values for the
minimüm of the width of the matching regions. The matching is performed with simple Ïinear interpolation
between Y values gained with the two successive polynomsl.
Figure Al.l illustrates the method of curve fitting.
-Wave spectra formulae
The computation of root mean square response amplitudes is performed iñ altogether l5 seaways using both the ISSC
and JOÑSWAP wave spectral density formulae:
1SSC:.
S(w)=(A/w)exp(-BIw4)
(A 2.1
whereA= 173H/T
B 691 /T
JONSWAP:S(w)' 1554
5exp{TW4}
(í42.2)
where y = exp A21 -[o.19.iwT-l\2
JG
f
anda=O.O7forw <5.24/T1,
='O.09/orw>.5.24/T1.
(A 2.3)
Appendix 2.in the formulae N5 is significant wave height and
T
2,rm0/m
where rna, is the n'th moment of the spectrum.
Each wave spectrum is defined with 50 ordinate values at the following frequencies with respect to modal cirçular
16, 18, 20, 25 and
A31
-AppendiX 3
Default sea areas
The program has six wave
where the operability
autoltiatiCal1Y. Table A3. i
climates as default sea areas
gives a summary of these sea
calculations are performed
areas.
The scatter diagrams of these sIx wave climates
are given
in the following tables. The
scatter diagrams represent
the joint probability of occurrence
for significant wave
heights and either modal wave periods,
Tm, or mean zero
up_crossing wave periods, Tz. The data are given in parts per thousand.
The Weibull coefficients of the
default sea areas are fed
into the program in data sentences
in subroutine OPERA.
Table A3.l. Default wave climates.
mv FN4ITA, winters 69-76 Lloyd &HansOn (1985) hindcasted - A2- -w/w,=. 0.6, 0.84, l.O0, 1.20, 1.50, 1.80, 2.10, 2.45, 3 00 0.65, 0.87,, 1.03, 1.25, 1.55, 1.85., 2.15, 2.50, 0.70, 0.90, 1.06, 1.30, 1.60,, 1.90, 2.20, 2.60, 0.75 e 0.80, 0.92, 0.94, I. OB,. 1.10, 1.35, 1. 40, 1.65, 1.70, 1.95, 2.00, 2.25, 2.30., 2.70, 2.80., 0.82, 0.97, 1.15, 1.45, 1.75, 2.05, 2.35, 2.90,
The me response amplitudes and limiting significant wave heights are presented as a function of modal wave periods
for the following 15 periods:
T5 = 3, 4, 5, 6, 7, 8, 9, 10, 12, 14,,
30 seconds
The well-known relations between nodal wave period T5 and
characteristic wave peiod T1 are used
T = 0.834 T5 JONS WAP