comments on the report:
ON ESTIMATION OF LONG TERM
DISTRIBUTIONS OF WAVE INDUCED MIDSHIP
BENDING MOMENTS IN SHIPS
with applications of proposed methods
by
NILS NORDENSTROM
Repon from the Division of Ship Design Chalmers University of Technology The measurements have been made ih cooperation with. the Swedish Shipbuilding
Research Foundation
The analysis is supported by a grant from the Swedish Technical Research Council
Gothenburg May 1964 Anders Svennerud
Preface
These comments tO my earlier report "On stimatiOn of Long Term Distributions of Wave Induóed Midship Bending
Moments in Ships" have two purposes.
Firstly I want to point out to those less familiar with statistics, the central role of statistIcs ii all
na-tural science research, I do not expect that my very short introductIon, will make the statistical concepts clear, but
I hope to awaken an interest in these important fundamentals. Secondly I want to give a more useful and understand-able description of the methods presented iii the earlier
report. Some views and conclusions regarding methods and results are given.
I especially thank Professor Anders Svemienid whose understanding and interest in the subject has made this work
possible and Mr. Ru-bger Bennet for our interest±aag and st1mulating discussions.
Gothenburg, May 1964
Appendix I, TIathema±ica1 treatment of the
còmection between error of measurement and
transformation function
0e0.0...0. ....ó...,.e.0.
49c
Appendix II A note on the choise of
"representative r value"
000,00 0000OflØ0fl.o5.00.. o,.
5j-Appendix III, Sorne simple ways to estimate the parameters of the Weibull distribution
55, Appendix IV, Statistical anaiysis of the
data presented by Göransson and Olofsson in
reference
/6/
. co,: 000000000,o 900000C- 58
IntroductjÓn
i
Summary of reference /13/
0000000e..oe.00
Other methods cáo OSI 00.0. o
.10
A practical application 11
The type of the long term peak
value distribution 0 . 0 0 0 0 i o e o o o e. t 15. Thê importance of accuracy of the
method used to estimate r values 00 00 00 00 00 00 00.4,002 17.
"The lagest possible value'! C 0 0 3
'.0 -Moient factors 27. Summary
00100.500 0000000000*01St 00000 006 0.0.00
r O 43 Reference s 0 2 0 0 0 o e n i o o o o o o e o e o a o s o i o o s o o o s o o I I * O 0.0 0 0 j 07 r IÏntxoduction.
Two probiem concerning wave bending thoments aro discussed in the report /13/.
Estimation of wave loads from full scale rneäsremen-ts at sea.
2. Predict5ion bf long téith t.butions oí wave loads
for the entire life of ä ship.
The results can be used. f o.r the analysis of other
vari-ables e.g. the motions of a ship izia seaway.
A shit :j subjected to a very Jarge number (about 108)
of stress cycles during the.lifetime. The amplitude of the loads vary at random and. statistical distrihutiòn functions are tie only means of analysis of this variation.
Let us bgin with a brief diseuCsion of some important
fundamentals for all scientific work, Carnap /3 4/ and.
Nagel /12/have treated this subject in considérable d.tai10
There are two kinds of reasoning and. conclus±ons,
Analytic or d.eductive.0
This way of reasoning cannot increase ou imowledge of
other facts than those which are contain od. in the pre-mises. E.g. mathematicai proofs are ana1ytic
Synthetic or inductie«,
This way o± reasoning is the only way to increase our
lmowledge of facts that are nQt:»ontain.ed. in the pro-mises. Then you Imow some events that already have
taken place, and want to predic.b the outcome of the same kind of events in the future you have to use
ductivereasoniiig. The best way to handle thiC prolem
is to use statistical method.
All statements that can be made about facts
must be
based on statistics, and the introduction of statistical
rnethod does not lead to a provisory solution, which
s
actu-ally said sometimes, but is on the contrary the only sien.
tif±c approach.
The terra Drobability is used under many different
cir--cumsta.ces an.d has many different meanings.
Asexarpie
probability is used in colloquial language when we want to
express a vague beliéf in something we cannot verify
This
is probably oie of the reasöns why the term often is
mis-understood when it appears with a quite different meaning in
scientific language.
Here we use probability defined in the following two
ways.
See Carnap /4/.
1
"Probability is the degree of cofiratio. of a hypo-.
thesis h with resDect to an eidence statement e egc
an observational reporte
This is a logical, semantical
concept.
A sentence about this cOncept is based, not on obser-..
vation of facts but on logical.
analysis.---(änalytic)"
2
"Probability is the relative frequency (in the long run)
of one property of eènts or things with respect to
another,
A sentence about this concept is factual
empiricaL"
(synthetic)
One usually speaks about the probability of an event
This makes it easy to misunderstand the öoncepts
Probabil-ity is not a property of events or things
ut of 3entonoe
about events or ±hiigs.
One sentence must be either false
or true.
A sentence can, however, be probable with respect
to other sentencies because one sentence can be true more
Often than another sentence in the long run,
If for instance you say "The probability to ge six in
this bast with this dice is 1/6", you can not verify or falsi-fy the statement by casting the dice. once. Therefore the
stateent is meaningless. If on the other hand you say "It
will be six" you can immediatelyprove if the statement is
false or true by casting the dice once and therefore the i.at-ter statement lias a meaning. Theh you say "The probability to get six Is 1/6" aid more or less unconsciously think of
some kind of Ititherentu probability you should think "The statement 'it i1 be si±' is true with the relative
fre-quency 1/6 in thé lOng rt.u"ò
If you accept a cëtain hypothesis aftr a statitical
test of say 5 percents significance level, this will mean
nothing (inherent) but making a decision in a way that 95
percents of all similar decisions will be correct in. the long run if the hypothesis is true.
A statistical distribution function is a tool deter-mining the probability that a variable takes on values smal-1er than or equal to a certain given value.
The distribution function gives a clear and useful
de-scription of events that already have taken place. Prom
such an estimated (measured) distribution ftmction we can predict how a variable under unchanged conditions with a
certain calculable. degree of confidence will behave in the
future. The distribution function thus gives us a rational
expectation about the future behaviour of a variable. The mentioned degree of confidence cannot of course
become solid )mowledge as analytical deduction is not possible. We cannot be completely sure that the sun will rise to-morrow but it is rational to act .as ifit would do so. This is self-evident for most people. It is therefore remarkable that
these. very persons often. are suspicious of statistics.
Summary of reference /13/.
A large number of full scale measurements during the
past thirty years have shòwii that the short term (about half
an hour) distribution of peak stresses can be welL described by a certain kind of distribution function Which is called
the Rayleigh distribution0 This distribution holds for the
discrete peak values and not for the entire continous
vari-ation of the amplitude. The latter variable is approximately normally distributed, The Rayleigh distribution is of a
simple mathematical form and it is fully charachterized by
on single parameter which we denote r. This parameter is
estimated from a record and can be interpreted as a measure
of the severity of the load situa-tian. The parameter r is
the root mean square of the peak values. Piire 1 illustrates
th cÓrnection be-ween a record9 corresponding Rayleigh
distri--bu-tian and the predicted future behaviour of the variable0 óertain Rayleigh d±strïbu-tion, correporidiìig to
certain value of r, cives the distrbution of peak values which you expect Lf yóu cöntinüé a rëóord under.tuadhanged
eiterna conditions (wêather speed, öburse etöo) ò
on the whole if you take a recOrd under eondit±ons whiöh cn be
chatäcterjzed by ±he same value ö,f r Thëlàttercan oCcur
in an infini-te numbor o± combina-±ons of óxtornal cönditions0
The entire "load life" of a ship is imagined to consist
of a sum of a very large number of short term distributions
The lifetime al' a ship is thus divided into short periods
where the loads in. each period is expected to follow a Ray-leigh distribution which is charaCterized by a certain value
of r. Itis then iìediately obvious that if you lmow the
long ter distribution of the r values9 you can predict an
expected long term distribution of peak values by summing contributions from each short term distribution of peak
alues. The total probability for the stress to exceed a
certain stres level is obtained as a. sum of the
robabii-ties to exceed the saIne level within each short term distri-bution. By repeating this procedure at
some different stress
of peak values.
If we accept the above mentioned procedure of suation we can make the following statement of the probleme
To get a representative sample öf r values,
To estima-te long term distributions of r values. To transform a. long term distribution of r values to a long term, distribution of peic values.
To estimate the confidence oÍ' the resulting long term distribution of peak values.
i Then we. make a nwnber of measurements on boárd a ship
e.g. during one vOyage across the North Atlantic we get a
sample of' r values. Such a sample is seriously affected by
the fact that consecutive measurements are made under similar
conditions. This is due to the slow change in external
con-ditions. One voyage may contain measurements only in heavy
weather and head seas. Even if we ma1e rneasurements during the entire life of a ship we may get a sarnple that is not at
all representative för the trad in question or on the whole
for the type of ship.
In order to get a r distribution which is more
repre-sentative than the one we happen to get in a limited time, we use a weighting procedure. - We choose one Or more
vari-ables (weather, wave direction etO.) that strongly affect
the wave loads and estimate an expected long term distri-buton of these variables by using Weather statistics, We then put larger (smaller) weight to measurements made under conditions that have occurred more seldom (often) than we
expect them to do. Note that there isno need. to Imow
the loads are affected by the chosei variable. it is,
how-evêr, desirable that the loads are affected by the chosen
Variable.
The data used in this report are Weighted with respect
to the sea state defined by-the Beaufort scale. In this way
we elim.nate a great deal of uncertainty and it becomes
possible to compare different ships as if they. were sub-jected to the saine weather conditions.
Two earlier proposed types of long term distributions of r, viz, the normal one and the log-normal one are
ana-lysed in the report /13/. The transformed variable log
(r + e) is found to be approximately normally distributed,'
This new distribution describes thê long term r
value.distri-bution much better than does the above mentioned ones, It
lies in between the normal one and the log-normal one, The
latter distributions are obtained as extreme cases when the
constant c approaches eternity and zero. A comparison of
the different r distributions is given in the next chapter.
Results from the above mentioned 'summätion of short
term distributions are presented in /13/. The three above
mentioned long term distributions of r are used0 The sum is obtained by numerical integration of the corresponding
func-tions in an electronic computer1' The result is presented in
dimensionless graphs which directly give the resulting long term distributions of peak values as function of the
para-meters of the long -term distributions of r, The graphs give sufficient accuracy for practical use.
Analysis of the integration shows that the upper part of the resulting long term distribution of peak values is
almost solely dependent on extremely large r values which are exceeded with very small probability. It is shown that it is necessary -to carry on the integration up to five times
the standard deviation of r above the mean of r, ±n order to
'ge± reliable inforrnation about the in-eresting largest loads
that occur only a ±ew times during the lifetime of a ship0 You cn object that such a high level in the r value
distribution is not realistic because, it corresponds to a
larer number of r values than a ship is ever subjected to
during the lifetime. This objection is, however, insignifi-cant because even i you are interested in the commonly
largest r values, you have to consider the risk of obtaining
i) This work was made at Faci-t lectronics AB i-n othenburg.
7. even larger values, The distribution of r values does of
course 'not stop at the expected largest value0 The largest
value takes on different values in every sample and is in itself a statistical variable with a distribution of its own.
The largest value (second largest etc.) will thus be both larger and smaller than the expected largest value (second largest etc,) and the distribution above the expected largest
value is of great importance. It cannot be insisted 'upon
too strongly that you must not let the most important part of the distïbution slip out of your hands when you carry out the integration0
4 A sample of r values cannot for natural reasons cover
the entire life of a ship. An available long term
distri-bution of r values will therefore be a random sample from
the total number of r values a ship is subjected to during the lifetime0 If you take a number of such samples from the
same ship and estimate a number of long term peak value
distributions with aid of the graphs mentioned above (3),
you will get the same number of different results. The
weighting procedure mentioned above (1) does not exclude this random variation but only reduces the number of measutements necessary to get a representative sampled
To be able to draw any conclusions from such a random result it is necessary to know the magnitude of the expected
deviation from the "truth" The "truth" here means the
re-sult you would obtain in the 'ong run, on the same ship using
the same method of measurement0 his kind of reasonable
truth must not be mixed up with any kind of metaphysic abso-lute truth that has nothing to do with natural science0
The report /13/ presents methods to compute the
devi-ations as confidence limits0 These are fuictions of the
total number of measrements, the number f r values within different groups9 e.g. weather groups and the values of the
pa'ameters of the r distributions0 The confidence limits
gives an interval on both sides of a computed value. This interval contains the "truc" value With, a óertain
pröba-bility. 1Tote that the confidence limits contain the "tri.ie"
value with a certain probability, and that the estimated
value is distfibuted around. the !ttfl.jeTf value, not vice vérsa..
The confidence limits give a
easue
Of the reliabilityöf a result, and conversely they give the number of measure-ments necessary to get a certain desired accuracy. t is
also possible to estimate how to distribute measurements among different groups (e.g. weather groups) ±n order to get
optimum accuracy, and thus get as much informtion as possible out of a ertain number of measurements.
Other methods0
The methods described in the report /13/ presupposes that you use the Rayleigh distribution to describe the short term distrIbutions, and then use estimated parameters for
.further calculations. One could ask why it is not better tO use strain cycle counters and thus directly obtain an 'Texact
distribution. Some aspects to this question is of öurrent
interest.
The factual wave loads do of ourse not change if you
change the recording method so the analysis will be based on the same random sample of wave loads whichever method
you may use..
Knowledge of the types of distribution functions, which by experience have well described a great many measurements
from many ships makes it possible to use parameters to de-scribe results from measurements. Such parameter values
give more exhaustive and accessible information about a
result, than does a detailed desciption of a random sample in an individual case0 This applies for instance to long term distributions from strain cycle counters. In order to use such distributions you have -to fi-t hypothetical distri-bution functions to the data and -test the goodness of fit0
In other case there is no possibility to judge the relïa-bility of a result, and draw any conclusions of general
applicability.
Consequently, values from strain cycle counters can
give reliable results if they are handled according to the
same principles as used when evaluating our records with
the aid of r values. The d±fference being that in the former
case we do not make use of the knowledge about the type of
the short terni distribution. This can be considered as an
advantage only if we do not rely on thirty years experie.ee of short term distributions. There is, however, a need for
control.
The estimated long term distributions that are obtained from any method can be controlled by comparing the largest
(second largest etc.) value recorded with the largest (second largest etc.) value predicted for the sarne period.
Conse-quently the same possibility of control applies to results from strain cycle counters as well as results from r values
Short term distributions characterized by r values form at present the most simple and effective basis for a weigh-ting procedure. They are also the best basis for a detailed
analysis of the influence of different variables (weather,
wave direction, speed, loading conditions etc.) on the wave
loads. Weighting of values from strain cycle coünters is
practicable only if you use comparatively expensive and
complicated measuring equipment on board, e.g. tape punch or tape recorder, or if you read off the counters at short
intervals and punch the data on cards or tape for use in a
computer.
It has been said that it would be less expensive and
better to measure only the extreme values during rather long
periods with a simple device and use the data for
extreme-value analysis. That is certainly of considerable value,
but in that case you have to give up all interesting in-formation about other values than the extreme ones, and the
advantage of that method lies in the possibility of
mea-suring inexpensively only the extreme values on many ships. The external conditions vary cQnsiderably during these long periods. This makes weighting ineffective and you have to
carry on the measurements for a very long time in order to
get sufficient accuracy.
All different methods that can be used for the analysis
of distributions of wave loads are, however, of great in-terest as they make possible comparisons between results
from different methods, especially now when we have rather little experience in this complicated field.
At present we cbisider r values to be the best basis
k practical application.
Pigure 2 shows a comparison between different methods to analyse a total number of 1577 short term recörds of
mid-ship bending stresses in 7 shïps. The distribution of r
values for each of these ships is shown in the report /13/. Some relevant characteristics of the ships are given in table
II.
The following three methods have been used for the
estimation of the long term peak stress distributions.
The sample of r values from each ship is divided into groups defined by the weather at the period of
measure-ment. The Beaufort scale is used, the groups thus being 0-3, 4-5, 6-7, 8-9 and 10-12, We assume that the r
values are normally distributed within each group and. compute the parameters of the normal r distributions from the corresponding values of r. The parameters are
used to estimate the long term peak stress distribution
within each group. The total long term peak stress
distribution is obtained as a weighted sum of the distri-butions within the groups.
This method was proposed in reference /1/.
The entire long -term distribution of r values from each ship is assumed -to be normal. The parameters of this
distribution is obtained by plotting weighted r values
on normal probability paper aaad fit the straight line to the data. The fit to the upper part of the
distri-bution should be considered most important. This is of course not in order to pay special consideration to any
random scatter of the largest r values, but depends on
the fact that the data when plotted in this way will
get a curvature in its lower part. The lower values
have very little influence on the result and should not have any influence on a line which fits to the most
im-portant upper part of the distribution. The parameters obtained from the normal probability, paper are used to
estimate the long term peak value distribution from the graphs in report /13/.
The variable log (r + e) is assumed to be normal. See
further method 2. It is shown in the report /13/ that we can use e = 2 kg/mm2.
The comparison of methods refers to the point of peak stress distributions corresponding to the lifetime of a ship.,
i.e. the maximum stress we expeöt the ship to be subjected to
only once in its iifetime As we see in figure 2 methods 2 and 3 give similar results, the difference being that method
3 gives a little larger values. This depends on the fact that
the distribution fanction for r that we use in method 3 gives greater probability tò get large r values than does the normal r distribution in method 2. It is shown in the report /13/ that method 2 gives an underestimation and method 3 possibly
an overestimation o± the stress. It is therefore probable
that these two methods give a lower and an upper limit för
the stresse
The r distribution proposed in method 3 fits the data much better than does the normal distribution of method 2 so
the former method is to be preferred. Method 2, however,
sometimes gives a rather similar result fitting the data of measurements fairly weil so this simpler methòd can be used
in some cases. These cases are determined by plotting the
data on normal probability paper.
Method 3 gives a result that in three cases diverges
from the result of the other two methods. The shortest and the two longest ships have got the largest divergencies.
This is probably due to the fact that we have got very few
records in heavy weather from these ships. This is of great
importance when we use method 1,but is relatively unimportant
for the other two methods. Methods 1 and 3 give good agree-ment for the remaining ships.
Tue confidence limits (see table I) explain to a. great
13. methods. Tie result from method 1 is, however, even more
dislocated because the two longest ships have got no records at all in Beaufôrt 10-12. This points out a serious weabiess of methöd. 1, for the. result should not be affected by such a
random eent Method i also gives considerably widei
confi-dence imits than the other methöds, especially in thos cases where the upper Beaufort groups contain fe
measure-ments. Phe confidence limits also varies with the total
num-ber of measurements but it is shown in the report /13/ that
the confidence of method 1 solel de.ends on the u.'er Beau-fort groups. It is possible to increase the reliability of method 1 by uziiîying at least 3 of the upper Beaufort groups, but then it is necessary to do an internal weighting in tuis
larger group and thus wo approach methods 2 and 3.
As a matter of fact it is self-evident that the most
important upper Beaufort groups should not have least reli-ability. Comparing method 1 with the other two methods we
find the most striking difference being that method 1 handles a number of separate groups but the other two methods so to
say connect the groups so that they cELn help each other to tell what the. distribution looks like in its most important but troublesome upper part. If one happens to get very un-expected reóords or no ecords at all in heavy weather,
methods 2 and 3 do not lead to any catastophe. This is, however, the óase if we use method 1. It is easy to sâtisfy oneself about this fact by adding a large r value in heavy weather and observe the jump of the predicted values. This
is the fact shown by the colifidence limits.
The free choice of weighting procedure is another ad-vantage of ethods 2 and 3. Using these methods it is
easy
to extend the weighting to more variables (e.g. weather, wave direction, speed) because then the weighting is made
first and does not make the integration more laborious. Use of method 1, however, makes extended weighting very laborious, or at least expensive in a computer, because each group is
integrated separately and the number of groups incréases
It is also possible to make a l?ss laborious weighting
accor-ding to method 1 by first weighting wit}-iin groups and. then
flake the final weighting afte' -the integration of eabh groupc This method is, however, less efficient.
Method i was the best one as long as we did no-t have any good. approximation for the entire long term r
distribu-tiön, but it does no longer give the bèst reliability when
we ow such a long term r distribution. However, method. i
is still of great interest because it visualizes the
influ-ence of the weather.
-Reliability and. simplicity is of vital importance in
choice o-f method. There is no doubt thatmethod 2 änd
The type of the long terni peak value distribution.
Figure 3 shows a graph that directly gives the para-meters of a long term peak value distribution as functions
of the parameters of a long term normal r distribution. The
long term peak value distribution is described by the Weibull
distribution (see Appendix III and figure 2). This
distri-bution fits well to the result from the integration that is
presented in the report /13/.
It is interesting to note that the parameter k, that
solely determines the curvature of the WeibUll distribution,
directly can be estimated from the parameters of a normal r
distribution. This is interesting because the value of k has a great influence on the risk of fatigue failure as
com-pared to the risk of failure at one single large load. n-creasing k values increases the risk of fatigue failure be-cause then the maguitude of loads occurring òften increase as compared to loads occurring seldom, and conversely de-creasing k values do increase the risk of failure at one
single large load as compared to the risk of fatigue failure.
Figure 2 shows k values for our ships as a function of
ship length. The k values were estimated. from figure 3 (method 2) and Appendix III (method 3). The figure shows
that k has a minimum at a ship length of about 170 meters. The bloók coefficient seems to hava little influence on k be-cause ships No. 2 and 3 have quite different bloòk coeffi-cients but similar k values and about the same length. If
k varies in this manner with the length of ship then hips
of the given length are. subjected to one single comparatively
large load with larger probability than longer aid shorter
ships.
Extended measurements can give a better estimate of k
as a function of variables of current interest. This is of
great importance as k undoubtedly is a very suitable
para-meter in the analysis of wave loads. It should be noted that a large k value does not necessarily give more fatigue failures because those ships may well be of a typethat usually is better constructed in this respect.
It is not surprising that k increases with a large length of ship because of the smaller probability for a ve long ship to meet waves f a Oharacter Ìiecessary to cause a load. öorresponding to the greatest load, experienced by a
shorter ship j This depends on the fact that the wave steep-nss decreases as the wave length increases. Very long waves
are also less freq,uent than sOmewhat shorter ones. See Roll /14/. It should. alCo be noted that k does not tell aiything
about the absqlute values of wave loads but oily characterizes the relation between latge and. smil wave loads on the ae
ship.
Wave statistics and model experiments in 'aes can give many interesting Contributions to the solution of these
17.
The importance of accuracy of the method used to estimate r
values.
The uncertainty of the methOd of measurement has two
main influences on the estimated long term peak stress
distri-bution.
Larger standard error of measurement leads to wider
confidence limits around the predicted stress and it also
leads to a larger overestimation of the stress.
We begin to investigate how the uncertainty of the
method of measurement influences the long term r distribution.
We later use the uncertainty of the r distribution to estimate
the uncertainty of the peak stress distribution.
The methods used to estimate r introduces a standard
error of the method of measurement that is proportionì to
the r value.
This gives larger absolute errors to the larger
r values than to the smaller ones.
Therefore an estimated
distribution of r v1ues always has larger skewness i.e.
longer "right tail" than te distribution we intend to
esti-mate.
If for example r is exactly normally distributed, an
estimated distrilution of r values would not be iiormal, but
the largest estimated r values would be larger than the
corresponding normal. values.
Larger uncertainty gives larger skewness.
If the
stan-dard deviation of the error of measurement is great as
com-pared to the standard deviation of r, then the upper part of
the estimated r distribution becomes lognormal independent
of the type of the "true" distribulion of r.
This depends on
the fact that the staildard error of measurement is
a linear
function of the r value.
See Appendix I.
This is one
expla-nation to the fact that the lognormal distribution has been
successfully fitted to r value data, in spite of the fact
that a lognormal r distribution leads to a preposterous peak
stress distribution (see /13/).
It also points out what
erroneous results it is possible to get if one does not take
great care of the error of measurement.
Consequently, uncertainty of the method of measurement
leads to the use of r distribution functions with too large
skewness, and thus to overestimation of the risk of getting
large r values. -- .
Overestimation of the standard deviation of r is an
other conequenbe. of the introduced error of measurement.
This depends on the fact that the estimated standard
devi-ation of r is composed of two components.. One compoflent
being the spread of r values depending ori varying external
conditions (weather etc.), and the other component being the inescapable error of measurement. The ferner component can only be estimated from data, but the latter component can be estimated analytically and. is dependent on the method
ofmea-surement. It is therefore possible to estimate th influence
of the error of measurement on the estimated standard
devi-ation of r. Figure 4 shows ti4s influence..
The. influence of the error of measurement increases as
the r value increases. Thereföre a grouped sample of r values
wi];l get larger estmated standard deviation of the groups
with larger r values, even if the t?teIt variable would have the same standard deviation of all groups independent of the
size of the r values. . This is connected With the above
men-tioned skewness. See Appendix I.
In this cOnnection we remind of the properties of the
distribution functions mentioned on page 11. The normal distribution is symmetrical. The normally distr-ibuted
vari-able log (r + c) gives little skewness of the r istribution when e is large. The skewness increases when c dçcreases.
The skewness is largest in the log-normal distribution when
c equals zero. The skewness is,however, not solely depen-dent on C, but is also dependent on the other parameters of
the distribution..
Persons unaccustomed to statistical .thinkin, too often feel strongly attempted to accept the disastrous
rnisuder-standing that a little systematic error can be jt.ggled away in a magic maimer by making a lat'ge number of measurements. This is of course wrong. In our case it is not possible to
measure-19.
ment on the r distribution by increasing the number of
mea-surements. An increased number of mèasurements can reduce the scatter of the predictions but this is of little or no interest if the points are scattering around the wrong value.
It is necessary to do a very complicated analysis o the problem if we want to lmow the exact magnitude of the
discussed deviations from the distributions we intend to
esti-mate. We will here only.point out some tendencies and do a simple estimate of the magnitude of the deviation caused by
a certain error of measurement. We know from the report /13/ that a peak value distribution estimated from a normal r
distribution is an approximately linear function of the stan-dard deviation of the r distribution, and that the width of the confidence interval is proportional to this standard
devi-ation. Let us assumO that the standard deviation of r is
small as compared to the mean of r. This is the case in a Beaufort grouped sample We can then disregard the skewness
within a group and directly read off in figure 4 the influeflce
of the error Of measurement on an estimated stress value and
the corresponding confidence interval. If for instance you set the upper limit of the allowed systematic deviation to 5 % you can read off in. figure 4 the corresponding desired accuracy f the measurements. It is also possible to use figure 4 to correct far the error of measurement.
It is evident from figure 4 that the error of measure-ment has great influence on groups with large r values but
has little influence on groups with small r values. If you unite all groups to one single long term r
distribution you will find that this will get a considerably larger standard deviation and therefore becomes less sensitive
to the error of measurement, especially as compared to those
groups containing the largest r values. From this point of
view one single r distrihütion is to be preferred, but the skewness can become important when we use one single r
distri-bution and the skewness also introduces an overestimation. The influence of the error of measurement on the confidence limits is, however, always favourable for the single
diCtri-but ion.
Prom the above it is evident that it is important to handle evex sIngle measurement in the same careful maimet in order not.to introduce any unimowi ui.certaintiésinthe
caidulatiöns. It is also evident that one single long term r distribution is less sensitive to the error of measurement
"The largest possible value'1.
Many authors have discussed a concept that is denominated. in a.y different ways, and which we cali "the largest posihle
value". It has been said that a physical upper limit'exists
and that statistical distribution funct±ons w! thout upper lim:Lt for this reason cannot be valid above this magic point. It ha
for instance been proposed that we should determine an "upper limit for wave bending thoments" and that we should use distri-bution functions which stop at this limit0 Trials have also
been made to compute "the largest possible wave load' in Waves of unrealistic steepness in order to fix an uupper limit" and concepts as "largest r value" and "most severe sea state" have
been discussed.
This is only a sample of a great number of snailar
íoru-lations. It is evident that these terms sometimes really are interpreted literally and that an absOlutely largest value is
considered to exist. We start with a discussion of this intor-pretation,
The basis for reasoning about "largest possible values" is probably the fact that a sea wave for instance cannot be
higher than the diameter of our planets PrOm this one has drawn the conclusion that there must be a certain limit to
natures own achievements, It seems like "the largest possible
value" is treated as a physical constant.
Probably nobody would believe that "the largest possible value" is common, but on the contrary very uncommon0 "The
largest possible value" is also usually said to be much larger than common values. By so to speak pushing the problem suffi-ciently for away in this manner it is easy to maintain coníused.
conceptions because one would not usually experience any value
that is larger than "the largest possible value",
As the term "the largest possible value" in many cases
is based on misinterpretations of basic concepts there seems
to be a need for an analysis of these concepts even. ifas a matter of fact it is self-evident that any absolutely largest
value doe not exist.
To be of any interest "the largest possible value" will
have to comply with at least the following two demands.
The hypothesis "the largest possible value exists" must
have a meaning.
A hypothesis has a meaning scientifically, if any one logical consequence of the hypothesis leads tö sentencies
that can be.empirically verified.
"The largest possible value" must be applicable.
This demand is in fact covered by demand No. i. Here we
only mean that the concept should be useful for
construc-tion purposes.
"The largest possible value" does not comply with any
of these demands and. is therefore of no interest. Let us
ex-plain this statement. We refer to the introduction of this
report.
If "the largest possible value" exists it is a factual
empirical thing. The magnitude of this valu e cannot be deter-mined analytically. Thus any sentence about the magnitude of
this value will have to be empirically verified. Then we have
to use inductive reasoning that cannot give full certainty. It is therefore evident in this case that it does not make
sense to define a value that can be reaóhed but (with probabil-ity i) cannot be exceeded. However large a value observed
there is always a probability (larger than zero) to exceed
that value. It is therefore impossible to verify a statethent about the magnitude of "the largest possible value.".
Consequently demand No. i cannot be complied with.
Assume for a moment that "the largest possible value"
does exist and that we biow its magnitude. What use could we
make of this lmowledge?
It would certainly not be wise to determine the dimen-sions of the ship structure to sustain "the largst possible
23. load", vthieh seems to be very unlikely to occur, if at the
same time we did not know its probability of occurrence or,
correctly seaking, did not Imow the probability to exceed a
value, close below "the largest possible value". It is obvIous that this probability is not. constant under all circumstances,
so the interesting thing would not be the magnitude of "the largest possible value" but the probability to exceed values
below "the largest possible value".
Consequently demand. No. 2 cannot be complied with.
We can thus state that "the largest possible value" is of no sense and of no interest if it is not defined as a value
that is exceeded with a certain small probability.
Pormula-tions similar to "the largest possible value"
e.g. "most severe sea state" havé not always meant values defined in our manner, but seem tO result from the difficulty
to accept.. statistical thinking.
The whole problem of strength of structures is basïcally h statistical problem.
This has to be accepted.
"Thé largest possible value" interpreted as absolutely largest is a metaphysical concept - a late remembrance of the
"Ideas" of Plato - and has nothing to do in natural science.
Summing up we recapitulate the following points of the
reasoning.
Wave loads are facts.
Sentencies about facts have no meaning if they cannot be
empirically verified.
Predictions regarding the magnitude 'of wave loads cannot be solid knowledge.
Wave loads are not interesting unless they are associnted
with probabilities.
Let us finally accept that any absolutely larget load
does not exist. Then below we speak about the larges-t value we mean a value that is exceeded with a certain small proba.-bility. This is obviously the only interpretation of the ter
tithe largest possible value" that does make sense.
Our discussion has showed that it makes no sense to look
for any upper limit for wave loads. We now proceed to discuss
the following question. Is it possible to use "the largest r value" or "the most severe sea state" that is exceeded with a
small probability for any conclusions about dimensioning?
It is not possible to draw any such conclusions. This will be evident in the discuss-ion below. As each sea state
corresponds to a certain r value it is sufficient to. discuss r.
The conclusions in question are usually drawn by using
a "'epresentative large r value". The stress (load) is com-puted from the corresponding Rayleigh distribution One
usual-ly states that the probability to exceed the computed stress equals the product of the probability to exceed r in the r
distribution and the probability to exceed the stress in
question in the Rayleigh distributiOn. This conclusion is completely wrong and very misleading. It is therefore easy to understand that it leads to the senséless consequencies
that have been pointed out iii. several cases. The fact that a ship has to be subjected to a "representative large r value" during an absurd length of time to reach a stress value
predic-ted by the methods handled in the report /13/ does not tell
anything about the reliability of those methods.
The total probability to exceed a certain stress is a sum of probabilities from each of all r values a ship is
sub-jected to during the lifetime. If you choose one "represen-tative r value" (sea state) you do not consider the larger or smaller probability to exceed a certain stress level at every
other r value. TIiis is the reason why a ship cs to live
through one r value during a very long time before the largest
stress computed from the "reDresentative large r value" eauals
the correctly estimated largest stresse, Even if you choose a very large r value the time necessary may well be longer than
the ordinary lifetime 0±' a ship, because the most important part of the r distribution lies at a very high level. Canse-quently even a very large r value can give a sc !Laafl
contribu-tion to the total probability of exceeding the expected lar
gest stress value, that the ship can live through th:Ls r value
for a practically unlimited time without considerable risk of
exceeding the expected largest stress value0 See Appendix IL
See also pages ami 7 in ai reporte
Finally we can state that it is not interesting to look
for "the largest r value", "the most severe sea state", "the
most severe wave- or response-spectrum" or any similar concept even if it is defined as a large quantity which is exceeded
with little probability0 The only way to u r vaJ.ues (or
similar) is to use the entire distribution
of r
values that we expect during the lifetime of aship0
One may
ask wh
we do not simply investigate an examplewhere wo calculate a "true'1 long term peak stress distrihation
by integration of
a r
dllstribution We could then choose ar
value"
in such amanner
that the stresscom-puted from the corresponding
Rayleigh distibution
equals the"true" stress0 This can 'e obt-ai:aecl. by ohoàsing suitable
values for the probability to exceed "the representative r. value" and the probability to exceed the stress in question
in the Rayleigh distribution, We then get two fictive
proba-bilities that in certain case give ihe amo result as a
cor-rect öalculationc,
This "practical method io howeve:c, not useful because the fictive prObabilities vary from one case another0
Short and long term distributions can not be described by the same function with the exception of -the completely uiirealistic case when r is constant throughout the 11f etime Therefore the proposed "practical"
method will
give a comp1etelr wrongslope to the long te stress distributioi which obviously is not Rarleigh distributed. Moreover the siöpe of the r distrI-bution varies from one case to another Por this reason two
r distributions can give completely differing
bug
term stressdistributions even if the r distributions happen to coincide
in one "representative" point. Consequently "the most severe
sea state" is not interesting because it means quite different
things on different ships r
We are thus again baôk to the. demand of using the entire long term distribution of r values, sea states, spectra etc. tö get the possibility of using these concepts in. the solution of the wave load problem.
Moment factors.
The variable we primarily measure on board the ships is
the extension in. fore and aft direction between two points in deck ör side close, to the stringer corner nrnidships. From
this extension we simply compute the stress with Hookes law.
Athwartships stresses that may occur are not taken into
con-sideration. Estimated r values are stresses in kg/mm2.
The stresses are computed as half the sum of the hogging
and sagging stresses. These parts are later determined as
percentage parts of the sum. This method is chosen because it
gives better statistical accuracy of the estimate of both the sum and the parts as compared to estimates of each part
sepa-rately. Here we first discuss the sum.
In order to compare data from different ships and be able to draw general conclusions we have to use nondimensional
mornent factors. Different types of moment factors wilJ. be discussed in this chapter. The problem of estimating wave
loads is divided into an "internal" and an "external" part.
The "internal" problem is constituted by-the fact that the section modulus of the transverse section amidships varies
considerably between different ships even if they have similar principal dimensions. Therefore we compute t midship bending moment from -the stress recorded and the cornputed section modu-lus of the measuring point. It has been
said,
by other authorsthat a certain inaccuracy is introduced in the estimate of the
section modulus because the elements of a transverse section do not have the same effectiveness in different types of
trans-verse sections. This inaócuracy is, however, certainly much smaller than the error introduced by neglecting the difference between ships and determine the stress as function of the
principal dimensions as some authors propose. It has been shom experimentally that the difference between the "tnie"
and the estimated section modulus is much smaller than.. the
di±'ferencjes between section moduli of different ships. A
misestimate of -the section modulus will be of little importance
if the section modulus is computed in the same manner at
surement and at design. This holds, however, only for ships of traditional design.
When choosing the required section modulus we meet
another side of the "internal" problem. This depends on the
different ability of different designs to withstand a certain
load without failures. This problem will not be discussçd in
detail here.
The "external" problem is to pay proper consideration,
to varying external dimensions (including the distribution of weight in fore and aft direction) as well as other external
conditions (weather etc.) -that varies from one case to another
and have influence on the wave loads This problem wille
discussed here0
The problem of determining the requiréd section modulus
has been discussed for a considerable length of -time and many
ways of approach have been proposed However, it seems im-possible to find any general methods because in each way of approach we haxe to consider the very special pro-requisite
conditions and take into consideration which way we want to use a result. It is evident that if e try to determine the required section modulus from the result of full scale tests,
we cannot use the same methods as used when determining the
section modulus 'from model tests in waves, taking standard
series of model tests in waves into consideration (analogous
to ordinary tank tests).
Therefore, it seems better to accept the d.ifferencies in pro-requisite conditions and define those quanti'bies best
suited to each way of approach. There is, however, one wa to compare results from different ways of approach by
com-paring long term distributioiis of wave loads.
Here we define a moment factor as a function of ship parameters that has constant value at the same probability level in long term distributions from full scale measurements
on different ships. It is evident that a function of this
kind, gives the best description of the connection between
- 'computations or model tests - have to be compared with re-sults from full scale measurements.
The entire pròblem is thus divided into two comptely
separate parts. On one hand the "internal" ability of the
ship to Withstand. certain loads, on the other hand the in-fluence of principal dimensions and. other "external" quanti-ties on the wave loads. This division is the basis of the rules of the classification societies where the problems, however, have been coupled together and, the permitted stress
is not only dependent on the "internal" ability of the ship to sustain a certain load but is also dependent on variations
in "external" conditions. This is due to the fäct that earlier
it was ot possible to observe anything but the total result
i.e. the failures, and there were. no possibilities to separa'e the causes. The mentioned. division is necessary for an ana-lysis of the causes of failures. Wave load statistics is necessary for the division.
It is also necessary in this connection to d,vide the
total wave bending moment into one still water part and one
wave part as we here only discuss the part that varies in
waves. Here below wave bending moment only means the varying
part of the moment.
In order to compare our results from full scale measure-ments on different ships we.first form a moment factor m0 in
traditional manner (Murray). Then we discuss different types of moment factors and we determine a moment factor that
ac-cording to our above mentioned definition gives the best fit
to the data.
Nowadays it is commonly accepted that the magnitude of the wave bending moment is better described by ship length and breadth than by length and displacement formerly used. This depends on the fact that the draught has little influence
on the wave bending moment which primarily is affected by the hull form in the vicinity of the water linee See Swaan /16/ and Vossers /17/. We use the largest stress X8 we expect a
M8 = S
M8
y B L
In the first trial to determine a moment factor fitting the
data we also use section modulus at measi.ring point S, speci
fic weight of sea water , mouldêd breadth B and length bet-ween perpendiculars L. For the present we put tIe fictivel) wave height H.proportional to and later we discuss H as a functiOn of L. Particulars of the ships are given in table
II. In the following we use meter and toi = 1000kg.
Figure 5 shows m as a function of L. The same figure also shows the water plane area coefficient and the pris-matic coefficient OP as functions of, L. The curves describing
m0, O and. O shows a striking resemblance and the fullness of the ship is no doubt one variable that is strongly connec-ted to the difference between the two groups of ships separa-ted in the figure.
The moment factor m1 was proposed in reference /1/.
M na
-1
yBL3C
Reference was then given to Swaan /16/. 11e shows that
a statical calculation (without Smith's efeet) for ships
with vertical sides gives approximately. a linear relation
between M and Det Norske Ventas applies a dependence of the fullness that is similar to the dependence in m1 (the basis being a statically calculated sagging moment giving a
coiservativè prediction for fine ships). See equatiOn (2). ccórding to Swaan, however, M is not prOportional to but the relation is of the type
M = const. - a) (i)
where a 0.4 when 08 < < 0.9 arid when the wave length
Consequently, reference to Swaan /16/ gives the following
moment factor.
31.
is similar to the ship length. Waves of this length give the largest wave loads, It is therefore explicable that m1 (see figu.re .5) can not describe the influence of the fullness on the recorded wave loads.
II' the statically calculated moment varies in a certain
way with certain parameters this is of course no reason to
believe that the dynamical moment has to vary in the same way. The hydrody-namic moment is different from the hydrostatic one
and aòceleration forces from the weight of ship and surrounding
water are added in the dynathical case. The relation, if any,
betweènCtatical and dynamical moments has to be empirically
verified. Statical moments are, however, interesting because they can lead us to try reasonable functions. Model
experi-ments (see Vossers /17/) show that the influence of fullness on wave bendìng moment in some cases are similar to relations
statically calculateda However, one has to be very cautious
about conclusions from statical calculations.
Prom reference /6/ we get (see Appendix IV) the following
relation between C andC,.
0WL = 0.68 (C + 048) (2)
Vossers /17/ gives the formula
3 0 = 2 + i
which also can be written
0.67 (C + 0.50)
The latter formula is very similar to (2). This gives
an indication that the data of reference /6/, which we will
use below, are representative for a large number of ships. We put a = 0.4 and get from (i) and (2)
M8
yBL C
This moment factor has approximately the same.dependence
of fullness as the formula used by Lloyd's Register0 They assume the wave bending moment to be proportional to aBel)
In this connection the fore and aft distribution of
weight and buoyancy is of particular interest and C is
there-fore more adequate than CBO The latter is affected by irrele--vant factors as bilge radious and rise o the bottom0 If we
hold desplacement, length9 breadth and draught constant and
increase the bilge radious we increase the wave bending moment0
At the same time C increases but C remains constant6 We therefore propose C to be used in this connectioli.
It is evident froh figure 5 that m2 is better than m but that m2 still does not.describe the influence of the
full-ness in a way that fits our data. The wave bending moment recorded. thus shows a stron dependence of the fulJ,.ness than
is given by m1 and m2.
Many other investigations support this conclusion0 Johnson /9/ presents results from the very extensive
full scale measurements carried out by the British Ship
Research Association (B S R A). Pigure 15. in /9/ gives
ap-proximately the following relation which refers to the rnoent
a ship is expected to meet 1 time in 100 days This is
ap-proximately equivalent to the probability level io_6 M = const. (CB - 0.5)
It should be noted that the influence of CB this
great in spite of the fact that the ine ships as an average have met more heavy weather aiid have spent longer time on the
North Atlantic than have the full ones
i) C denotes block coefficient.
Bermet /2/ has analysed B S R A's measurements and he
gives effective wave height in Beaufort 8-9 asa function of'
CB. Figure 5 in /2/ gives approximately the following rda.
tion.
M = const. (CB - 0.16)
It should be noted that this holds only for Beaufort
8-9.
Zubaly /18/ presents results from calculations based on
model exeriments and wave statistics. The moment factor
is given for two ships (L = 137 in; 0B = 0.60, C =
071 and
0B = 0.80, C = 0.87) as a function of wind, speed W in knots The following relations are derived from /18/.M = const. 0WL (CB - 0.11)
M = const. C, (C - 0.21)
By inserting equation (2) we get
M = const. (CB - 0.33) IV = const. (CD - 0.38) W 60 W = 35 W = 60 W = 35
Göransson änd Olofeson /6/ present statically
calcu-lated wave bending moments of 30 ships having 0.63
Op
0.82. They g±ve the moment factors
h (hogging) and (sagging). M M s 2 9 1k = 2
BL H0
yBL
HH0 is the wave height. H0 L/20 is used in /6/.
Statistical analysis shows (see Appendix IV) that the
three moment factors
1h' and h + = 1kh + are very
strongly correlated to C ,O and OBI No one of the latter
parameters is significantly superior to the others. Prom
Appendix IV we get
+ = conet. (c - 0.13).
Neither 0B' a nor O can be expected to give a complete
description of the influence of the fullness on the statically calculated moment. One reason being that the wave bending moment varies with
0E
(c) when
0WL (cr) is constant. Thisis due to the fact that the wave bending moment is dependent on the slope of the cross sections in the vicinity of the
water linea Vertical sides give the smallest momeat (u shape).
Increasing angles to the vertical plane increases the moment
(y shape) The degree of u shape can for a bonstant value of
or C be described by C.
C/C. This is
a kind ofvertical prismatic doefficient. Statical calculations for 4 fine ships (C = 0.686, reference /6/) and 3 full ships (C =
0804, Ivarseon at the Swedish Shipbuilding Research Fornida-tion) show that the moment is approximately a linear decreasing function (not proportional) of CV when the shape of the sec-tians vary from y shape to u shapes The moment of the fine ship is more sensitive to changes of than is the moment of the full ship. This depends on the fact that a smaller part of the full ship is affected by a change of shapes The stati-cally calculated moment of the fine ship is about 15 larger
at y shape (Cv. = 0.855) than at u shape (C = 0.928).
According to Swaan /16/ C is the parameter best suited to describe the influence of the fullness on the wave bending
moment. He considers the influence of the shape of the
sec-tions to be negligible as compared to the great degree of
ap-proximation introduced by the statical approach. However,
Appendix IV, based on reference /6/, shows that in statical
calculations for realistic hull forms C is not superior to
C.
C and C are slightly superior to 0B which, for above mentioned reasons can be expected. Concerning the shape ofthe sections it is pointed out above that y shape gives
con-siderably higher moments than gives u shape and one can no
doubt assume that differencies in statically calculated moments correspond to differencies in dynamical moments although the absolute values of neither the moments nor the differencjes
35.
Thereforé it seems reasonable to expect the shape o± the sec-tions to become of increased importance when our mowledge
about wave loads increases.
The longitudinal moment of inertia is another variable having influence on the wave loads, and even if we hold the
lQflgitudinal moment of inertia òonstant changes in the
lOngi-tudinal weight distribution will change the wave bonding mo-ments. Unfortunately wedo not have the longitudinal weight
distribution at each period of measurement easily accessible,
but does to a great extent give a measure of the average
longitudinal weight distribution. The hydrodynaimical part of the moment is closely related to Ci,.
For simplicity here we consider to give a usefil
de-scription of the longitudinal distribution of weight and
buoy-ancy. C is at any rate one single parameter giving a good
description of the influence of these quantities. The next
step will be to introduce additional parameters describing the influenóe of the shape of the sections and the longitudinal weight distribution.
The data presented in referencies /2, 6, 9, 18/, refer-red to above, gives reason to expect the following moment fac-tors m3 and in4 to fit our data better than do m1 and
M3 M8
BL3(C-O.2)
in432
const. (c - 0.35)
It is evident from figure 6 that Is better than in1
and m2, but that m3 still is not satisfactory, On the
con-trary m4 gives a good. fit to our data. Note that in4 closely resembles the mentioned, result from Ïnodel tests presented by Zubaly /18/. In the future we will possibly get a function of the type (c - a)2 + b. This is indicated by model tests
and by statical calculations.
We now try to fit a function to the results from methods 2 and 3 (see page ii) that is obtained by using m4 (figure 6),
In4 = a e
The result from method 1 seems to be. doibtful because the
right
part of the curve obviously has got to large steepness0The moment factor m is proportional to H/LI Here it is not necessary to make any distinction between H and He
be-cause these two quantities are related to L in the same way0 It is well Imown from statical calculations (Swaan /16/) and. from model tests (Dalzell
/5/,
Ivarsson /8/, Vosers /17/)that waves of' about the same length as the ship give th lar-gest moments, and
that
the momentis
approximately proportionalto the wave height. Consequently we expect the mOment factor
(at a certain probability level) as a function of ship length
to be proportional to the wave steepness (at a certain
proba-bili-ty level) as a function of wave length. The wave steepness
has a finite maximum for small wave lengths, it decreases as
the wave length increases and it approaches zero when the wave length approaches eternity (see Roll /14/). This sim le
rela-tion between wave steepness and moment factor is no doubt fundamental for the understanding of the wave load
problem.
Many model tests (e.g. Zubaly /18/) supportsthis
statement.We therefore try the function
which has a finite maximum for L = O aid approaches zero when L approaches eternity. Figure 6 shOws that the following
fuñe-tions give a good fit to the results of methods 2 and 3
L 2m4 = 0.00270 e 250
L 100 L 240
3 = 0.00275 e
270
The largest moment we expect a ship to meet during the
lifetime
isthus probably contained
withinthe limits (see
page 12) given by the following formulas.
= const. L e
100 L 240
270
It
is interestin.g to compare the following three ways of describing fictive wave height.L.
i. H1 = const. L 260
(3)
const. L°'5 Lloyd's Register
113 const. L°'3 Dot Norske Ventas
Figure 7 shows
a qualitative comparison between the three functions. The constants are given values so that the functions coincide at the ship length 200 meters. It isevident from
figure
7 that the function H. is of a quite different type than 112 and H3 The functionHi reaches a
maximum, in this case at 260 meters,
and
it decreases for larger L.Puidàmentally the same type of function has been ob-tained from model tests (Dalell /5/, Lewis /10/9 Ivarssoi
at the Swedish Shipbuilding Research Foundatiön).
Murray /.11/ has presented statistics of failures from a very large number of ships. It shows that
within the region
(medium size ships) where H1 is relatively larger than 112 a
37.
L0.00270
y B L3 e - 250 100 L 240 (4) 3 =0.00275
y B L3 e 270 C 0.65 0p 0.85Prom these
formulas
we get fictive wave height as afunction of
ship
length.L