RCH I EF
Technische Hogeschool
International Symposium on the Dynamics
°eIft
Marine Vehicles and Structures in Wavesr 'I ¶%7
PAPER 41
ENERGY CHARACTERISTICS OP STATIONARY RANDOM
OSCILLATIONS AND THEE USE. IN STATISTICAL
ENIA1IibIotheek van deLINEARIZATION
Ondeafdeing der Scheepsbouwku.nde
TechnischeHogeschool, Deft
DOCUMENTATIE
I: K
8 t 12 .. - .DATUM:
..
A.V. Gerassimov*Summary
The paper deals with a rather broad class of stationary random oscillations of linear and nonlinear oscillators. It
reveals that the probability densities of displacement and velocity of oscillations are functions of the instantaneouá values of the oscillator poteütial and kinetic
ener, while
the time-mean values of the same serve as parameters ofdistribution. At the same, time it appeax'a that for nonlinear
oscillations the varjance of displacament is not a parameter of distribution. In such a form the laws of distribution are identical
for
the whole range of linear and nonlinear
oscillations considered, which makes it
possible
to formulatethe concept of ener-equivalent random oscillations and to
show the consequences of it. Por the nonlinear oscillator the distribution laws of oscillations are found to be dependent on
their enérr levels. In particular the concept Of random .
*
Krylov Ship Research
Institute
M-158, Leningrad, USSRamplitudes so understood is shown to be the parameter of
distribution. For the linear oscillator the random amplitudes are distributed according to the
Rayleigh law.
ParameterS are
determined for a linear oscillator which is energy-equivalent to the given nonlinear oscillator in certain conditions of excitation. Hereinafter the term "energy-equivalent" is used to denote the equivalence of random' oscillations having equal energy levele. This linear oscillator is used as a model for calculating the energy level of the nonlinear oscillator, after which the distributions of oscillations of the same can be calculated with due regard for the features inherent in.them. To make a comparison between this energy-equivalent
method of statistical linearization and the so-calle4 equivalent statistical linearization method, two examples are considered0
Introduction
The evaluation of the effeOt of nonlinear factors on the ahip' s irregular motions and the accompanying phenomena attracts
more and' more attention. A comprehen8ive review of the group of problems in question was made by Grim at the 12 ITTC
[lJ.*
Among these is the problem of random Oscillations of a
rneôhanical system with a nonlinear resistance and restoring
force. In fact, this kind of. oscillations are characteristic,
to a. greater or lesser extent, for the rolling motion of a ship in seas.
*
Numbers in, brackets designate RefOrences at the end of the
been given due attention so.a'. Meanwhile, the versatility of such a concept as energy of an Oscillating system makes it possible to define the characteristic features of the energy-equivalent nonlinear and linear oscillations of the system. Owing to
this, one can
specify such a linear model of the non-linear system the oscillations of which (model), with thedisturbance
given, have
the same energy level as those of the nonlinear system. This level can easily be calculated on the basis of the spectral theory. On the other hand, the laws of distributions of nonlinear oscillations may be connected with their energy levels. This fact makes it possible to 4evelOp a method for the calculation of characteristics of random non-linear oscillations by which the energy, with the disturbance given, is calculated for the eñergy-equvalent linear system, while the distribution laws of nonlinear oscillations aredetermined according to the known level of energy, taking into account
the
featureswhich
are just inherent inthem
ratherthan
in their linear model0 This method will be termed as the energy-equivalent method of àtatisticallinearization.
Compared:with other known methoda of statistical linearization, this one offers the advantage of being more simple and accurate in
respect of evaluating the nonlinear oscillations.
The purpose of this paper is to substantiate the above conceptiOn.
ENERGY CHARACTERISTICS OF THE RANDOM
STATIONARY OSCILIATIONS
l. Let us consider the random stationary oscillations Of
a second order dynamic system (viz., an oscillator)
I
U (xl =
(1.1)
Where the viscous resistance force
4C)
andthe restoring
(quasi-elastic) forceU (.X)
devidOd by the mass unit are single-valued odd functions. For shortness Sake, when using such categorie8 as force,work, ener, etc., the
words"devided by the mass unit" will be omitted as a rule or replaced by the word "specific".
The random disturbance is supposed to be a
stationary centered Gaussian process with the spectral density given in the range of positive values Of circular
frequency Ct.' ;
hereinafter the
word "circular" willal8o
be omitted. Besides, the disturbance is supposed to be an ergodic
process, which means that the vibrations of the oscillator are
also ergodic.
Let us denote the potential energy of the oscillator as follows
Uo)
=0.
(1.2)
Due to the fact that the random vibrations of the
oscillator X(t) are
symmetrical, it is apriori knownthat
these vibrations have zero mathematical expectation and symmetrical distribution of both displacement and velocity.
!velocity
condition f atochastically Independent displacement and
velOcity of the sSmO. Hence, for the .proCesaea in question the joint probability density of displacement and velocity is
a
product of one-dimensional densities of probability (v-.ia)
The same. considerations of symmetry result in nonrandom
relations
L21
for the class of processes involved, Which are as follows:11 [x.ucx)j
-
=
M
[ZJ
(1.4)
where
Ii [
J
denotes the averaging over time within one realization of the process. The class of systems (1.1) also includes the linear system+ ix=
(r),
(1.3)
(.1.6)
the random oscillations of which have received the most careful:
study. So, let us first find
the
basic energy relations forthe
linear oscillations and then carry out generalizatiOn to the case of nonlinear oscillations.The one-dimensional and-the
joint
probability densities of displacement and velocity of linear ocillationS can. berepresented in the homogeneous form .
v)
2:A
Where
pfrlL'l-r21
Mf
1and i'ta time-mean value
+
p21?
.z Jf"
is the velocity variance of oscllationa, denotes the averaging
over
an ensemble ofrealizations,
fr/Djo
v-is tie: mean frequency of the process defined by the number of displacement up-crosses. These homogeneous representations are based on the assumption that the random process is a
two-dimensional function of the common argument, i.e.
time,
There-f ore, equal weights are attributed to the values oThere-f and2tT't)
at any moments of time and the mean-weighted values obtained with the use of the weight functions(i.7)-(l.9,)
are time-meanvalues.
The
instantaneous
value of kinetic ener of the linear oscillator(1.9).
(1.10)
4 ()
r
It is essential that the oscillator kinetic energy isunequivocally determined
only
by the instantaneous value of its velocity for both linear and nonlinear oscillators.This
is not the case for the potentialenergy
of oscillator; itsinstantaneous
value is determined not only by thenetantaneous value of displacement but also by the
form
offorce
function U(X). It
is alsoimportant
to note thatdisturbance influences the oscillator velocity,
and
its displace-ment is considered to be a kind of response to the velocity,the
magnitude
Of this response being determined by the transformation of kinetic energy into potential energy.Let us
term
(1.12.)
"the reduced potential energy" of the linear oscillations and
uc'x)=
2:t'
(1.13)"the reduced force.
function", respectively.
The dynamic state of the vibrating oscillator at
each
moment of time is determined by the totality of its displacement and velocity. It follows from (1.9) that the states of the
linear oscillator in which its total reduced energy
£
*(
2t)=
,T '"x)
Q(v)
remains the
sameare
consideredto be equally probable.
The time-meanvalue
of the totalreduced
energy ofthe oscillator
V
But,
as itfollows directly
from (1.12),so
Thus the velocity variance of oscillations determines the time-mean values nOt
only
for the kinetic energy but also for theLet us turn flow to the
expression (1.4).
Settingaside
the term for the time being,. we can say that this formula describes only the potential properties of the
oscillator:
here
the velocity variance of oscillationsis a measure of correlation between the displacement of the oscillator and its acceleration due to this displacement (i.e. the restoring fOrce). The correlatiOn moment between the
displacement of the oscillator and the di8turbance
determines the time-mean value of the work consumed for
synchronizing by disturbance. The random disturbance, which
i8 an oscillation by itself, must produce some work in
synchronism with
the
vibrations of the oscillator despite the tendency or the latter to vibrate with natural frequency.Using the spectral theory of the random processes, let write the spectral expansion of the correlation moment for the linear o8cillator between its displacement and disturbance:
argument for the complex transfer function of the oácillátor, respectively. The product
J
(d)j
changes the sign at
=
. Consequently, in certain instances the spectral distribution of disturbance may result in random stationary oscillationswhere
fk1x.qJ=
0,
(1.14)I
Ft
(d)1
E ()
3()
synchronizing. the oscillationS is equal to zero.
By analoj
with an ordinary resonance, the above condition can he called a "stochastic resonance". It is apriori obvious that the
condition described in (1.14) is applicable to both the linear and nonlinear oscillators excited by 'White noise"E2].
In all cases where condition (1.14) is satisfied, we shall deal with a noncorrelated disturbance, in the opposite case with a correlated one.
Let us denote the mean frequency of the process for a
noncorrelated disturbance by W. For the linear oscillator
= fl.
lxi
this ease, as is seen from (1.4),-= u
(1.15)
i.e. the time-mean value of the kinetic ener of random
oscillatIons is equal to the time-mean value of the
potential
ener of the Oscillator.Hence
f[I11fx
tCx)]_
Mt(xJ}
(1.16)
(l17)
The.latter expression makes it possible to represent the reducedpotential energy of the oscillator in the following form:
U?x) --
CJ(x),
(1.18)(l.19
Accordingly, the reduced force function of the oscillator has the form
U
UCx).
(1.20.)
Therefore, in carrying out the probability analysis, there, is reason to believe that the correlated disturbance changeC with time only the scale of the oscillator potential function, without changing its dependence on argument
7C. A
similar peculiarity is Observed for regular forced. oscillations.Now let us write the probability densities (1.7)-.(l.9)
:ifl
the fOrmL
(C'x))
=
(ir
&t/z)
ep
f
Uz)
7
(2.].)
?.tr(G.=: (s)
c(E)=
7g*/)4p[
E(x,zi')
(2.2)
(2.3)
Expressions (2.1) through (2.3) do not involve features which are specifically characteristic for a linear oscillator, while such. cathegories as potential, kinetic and total energy of a vibrating oscillator are similar for both linear and nonlinear cases. These expressionø are in the final analysis based on the moat general law of mechanics, viz, the law ofcoervatjon of mechanical
.ener,
The above considerátj(2.l)-(2,3) are common for the whoj.e class of the oscillators in question.
The suggested hypothesis is rigorously proved for the
nonlinear oscillator with a noncorre3.ated disturbance. In this
case ,
17(x)
,
and expression (2,3) is transformed as follows:
(::ç
it) =
+
--
(2.4)The similar problem where the noncorrelated disturbanóe is supposed to be a "white noise" is rigorously solved by using the
Fokker
-
Plank Ko]mogorov equation { 2J, and the result obtained is similar to thatshown
in (2.4).For nonlinear
oscillators
with Correlated disturbance, no common solutions are kiown, therefore in theSe cases .t isimpossible to giYe a .rgorouaiy theoretical cOnfirmation of the above hypothesis. However, sOme facts and analogies give
evidence in favour of the hypotheaja in the case of correlated disturbance too. In particular, let us consider the following. If the nonlinear oscillator is exposed to the action of
harmonic disturbance at a frequency of W , which induces.
regular oscillations with amplitude Z, the Work Of synchronizing the disturbance is proportional to
where CV(et) is the natural frequency of the oscillator for
amplitude a
Here we have a complete similarity with(1.16) as
a4)JiB
proportional to the average potentialthe
properties of the oscillator and therefore they are invariant
to the lawo resistance to oscillations.
The dissipation properties of the oscillator are taken into
account only
by relation (1.5) which implies that the average power dissipated by the oscillator is equal to theaverage power gained by the oscillator due to disturbance
Given the disturbance, its realization is subdivided into component which is collinear with the displacement
cJ,x(tJ-and the -component which is orthogonal to the same and always in-phase with the velocity of oScillations. This
subdivision is determined by a combination of conservative and dissipation Properties of the oscillator and in the general
case changes with the variation of both the level of disturbance and its spectral structure. Only when the oscillator Is excited by a "white noise", c
(i-)
0
,and hence HEx]
M. [±]
=
Without due regard for the above interrelation it is impossible to evaluate the energy level of the oscillator vibrations at given disturbance, which at present is practicable only in respect of the linear oscillator or 'the nonlinear oscillator
excited by a. "white noise".
However this is not at variance with the foregoing. In
this case consideration is given to oscillations whose kinetic energy mean value is determined by equation (1.5). In this expression 'the conservative properties of the oscillator
manifest themselves oiy indirectly through
,t)
sincetransformation of the oscillator kinetic energy into potential energy and vice versa (which
ith
described probabilistically by functions (2.l)-(2.3)) it is regulated by only thequasi-conservative properties of the oscillator (or by. quasi-conservative ones in the case of a noncorrelated disturbance). In particular, if the given law of resistance (e7(1Y) is. substituted by the law
provided that
M. {treLrJ
then for the oscillator with a linear restoring force in the case of an arbitrary spectrum of disturbance, or with a non-linear restoring force when excited by "white noae", it can be rigorously proved that the variance of velocity and the
correlation moment between the, oscillator displacement and
disturbance, will not change. It follows from these two
conditions that the laws of distribution of oscillations
(2.1)-(2.3). are invariable (in; this. particular problem).
Thus, the distribution laws for the class of random oscillations under review are invariant under'the viscous
resistance law of a dynamic system provided that the mean value of the power dissipated in the system is the same for various laws: of resistance and the given disturbance. In other words, if th dissipative force and the disturbance component
are simultaneously omitted from consideration, it will not influence the probability characteristics of stationary
oscillations..
The second genCral conclusion consists in that for the class of systems and disturbances in question the distribution law of the velocity of oscillations is the Gaussian law of
indivi4ual features of the systems0 Physically this concluSion is accounted for by the constancy of the mass of the system
(the added mass of the latter also inóluded for the case when the body oscillates in liquid) and also by the fact that the instantaneous values of its kinetic ener are independent of the past history of the movement.
j. Substituting the variable
we can write the distributiOn8 (2.1), (2.2) in the following
way :
_f
)
U?)
(3.2)
.'
J
It follows from these expressions that random oscillations of the class in question have similar distributions of
displacement an4 ve:ocity as functions of instantaneous values
of the reduced potential and kinetic ene, respectively. This
conclusion is drawn for the arbitrary law of viscous resistance and for the weak limitations in respect of the type of the
nonlinear restoring force. These limitations consist in that the dynamic system is in fact an oscillating system and its zero
position XOis stable equilibrium (the indifferent
equilibrium is also admissible). The averge circular frequency of the 'procesS is the scale of distribution of displacement.
Tr*
In the general case the expression 4'r 'J
/
e'- is theparameter of the distribution of displacement;. this eXpression can be interpreted as the square of the double 'amplitudes of regular linear bscillatiOns with frequency W , whose,
mean values of the kinetic and potential energy are equal to those inherent in irregular oscillatiOns. The magnitude of this double amplitude will be. called the energy-equivalent double amplitude of irregular oacllatiOflS. For the linear system
this i. However, for thö system with a
nonlinear restoring force there is nO such direct proportiouali
between
E
(i.e.
the mean potential energy of the system)and. the displacement variance , ao in the general case
is neither the parameter of distribution, nor the energy criterion of random Oscillations in contrast to the velocity variance
which
is always a cOmbination of both.The adequacy of quite a broad c).aaa of random oscillations (of the nonlinear oscillator) In respect of energy makes it possible to form rather a general idea of the ener..equiValeflt
processes. . . .
Irrespective of .the type of non1ineartY of the restoring
force (within the specified general limitations) the random stationary oscillations Of the class in question
whose
mean values of poweri4JV'(vfl
dissipated in the system and frequency of the process are equal (the level ofdisturbance given) will also have equal both the mean values of the specific (per unit of mass) potential and kinetic energy and the energy-equivalent amplitudes of oscillations; the foregoing holds true, in particular, for the comparison of nonlinear an4
linear systemS. ., . .
Energy equivalence of processes may be unconnected with the disturbance level and dissipation in the oscillator. It is
eat importance. If two processes of stationary random oscillations for the class under consideration have equal velocity variances and mean frequencies of oscilia.tons then
apriori both their time-mean values of the specific kinetic and potential energy and the energy-equivalent amplitudes of
oscillations are equal. too. Here the mean frequencies may be replaced with the energy-equivalent amplitudes of oscillations
and vice versa.
Now let the two oscillators, one lith nonlinear and the other with linear restoring force have equal laws of resistance0
Then, with the variancesof velocity
4
being equal, thedissipation of energy in both the oscillators will be the same.
Let us deteine the value of the linear restoring force for
which the oscillations óompared are energy-equivalent. Prom Eqs. (3.1) and (1.18) it follows that
C7'x) =
(3.4)and hence the distribution (362) can be transformed to the following form:
(u/z)
.Jq7r7Z)
frZ.-X,. we have Hence
c
(r/d;rJ:)
LA/)
But for the oscillator with a linear restoring force
C'?x)
-
I
,stx ;
X)
U-This. should be a Gaussian distribution, which is possible
(3.5)
if
tLai.
On the otherZr =
&z U/02.
side, we shall have and hence
E '
(3.7)
(3.8)
viz, the frequenciesV0
and C') should correspond to oneand the Barns value of the ener-equivalent amplitudes.
Thus 'under the above conditions
the ener-equivalent
linear system should have a restoring force equal tocx) = C:O
X, where
is the mean frequency ofoscillations in the given nonlinear system in the case of a' noncorrelated disturbance with the same value of the energy equivalent amplitude of oscillations0
In the distributions (3.2), (3.5) X is an argument, sà the averaging with the use of these distributions gives the displacement-mean values. Thus, at the same time one may come to a conclusion that with the given value 'of the
energy-equivalent amplitude of oscillations the displacement-mean value. of.the potential energy of the oscillating system is independent of the spectral structure of disturbance. The correlation
between the displacement of the system and the disturbance will change only the time-mean value of the potential energy. In other words, the dieturbance does not change the potential function of the system as it is, influencing the velocity of the process alone, i.e. the distribution of displacement with
time. It is precisely this fact that makes it possible to
represent the potential energy of random
oscillations 'of
thealone in the form
z)
The question
of. whether Eq.(1.18) is satisfied for each instantaneous value of X remains open.
However, from the point of view of ener this question is not of prime importance since the condition described in (1.19) makes it possible to assert that the difference
L1*(t.x)
(2/,)
TJ(x)'
is a function having a slight deviation from zero, with
a
zero mathematicalexpectation. Hence, the two-dimensional distribution of the state of oscillating system as obtained with the use of
approximation (1.18) will only slightly differ from the true
distribution,
Mention
should also be made of a wellkriown featurecharacteristic for the nonhinaer oscillations in caée of a correlated disturbance,
which
consists in "jumping" from one amplitude to another at a given frequency, that can beinterpreted as a discontinuity of amplitude, However, the discontinuity of amplitude in this case is taking place as long as we analyse the amplitude of stationary regular oscillations. as being a parameter of the process. In the process of
oscillations itself this "jump" is a transient process which
i8
oscillatory too0 The phase trajectory of this transientprocess, remaining continuous, passes from one limiting stationary cycle to another, any point of this trajectory characterizing one of the possible states of the system with a particular value of the total energy. There iè not much
difference between the whole phase trajectory of the realization
of random
Oscillationsin case of a correlated
disturbance and that part or parts of the same which correspond to relatively
quick (but far from being instantaneous) changes in the characteristics of cycles within the zones where "jwnps't of the amplitude are possible for regular induced oscillations. Consequently, this distinguishing feature. of nonlinear
o8cillations is taken into account by the energy conception presented above.
However, the simplicity of solution is due to the fact that no consideration was given to the evaluation of the kinetic energy of an. oscillating system for the given
disturbance. The possibility of existence of several modes of oscillation at certain frequencies of disturbance makes the complicated problem of evaluating the kinetic energy of oscillations still more difficult.
ENERGY INTERPRETATION OF THE LAWS FOR THE DISTRIBUTION OP OSCILLATIONS
4. Let the coordinate plane X be
the region of
possible values of .X
and V
so that each point of this plane characterizes one of the possible states of theoscillating system, thIs region being unbounded in principle.. Any realization of oscillations
x') is plotted by
a defInitephase trajectory x()
on this plane;
besides9 due to theergodicity of the process this trajectory entirely fills up the
plane X27 for a realization of infinite durations Por any random oscillations of second order dynamic systems theIr
realizations exhibit some properties which have much in common due to the fact that alongside with a stochastic independence
there is an absolute deterministic relationship between displacement and Velocity for each particular realization. Hence each zero value of velocity in the realization of the process always corresponds to the extremum of displacement.
Let us refer to the part of the process between the ajacent moments of
transition
of the zero level of displacement from the negative to the positive region as a "cycle of randomoscillations". Then each cycle will correspond to a loop of the phase trajectory between two adjacent points of intersection by it of the positive part of 1P-axis. Since within the cycle the zero level of displacement is crossed in the opposite direction too, the above lOop certainly covers the origin of coordinates. The phase trajectory always intersects, the .X-axis along the normal, the absciasa of the intersection point being the extreme value of displacement in the realization denoted
as a
X(Vzo.
The so called secondary extrema of realization .&,J take place(Pig.1) if three' consecutive points of intersection of the
-axis by the phase trajectory are on one side of the origin of coordinates. In other Words, the secondary extrema (1, 2, 4, 5 in. Fig.l) correspond to the secondary loops of the phase trajectory, which do not cover the origin of coordinates. The
rest of the extrema will be called the main extrema or the random amplitudes of the process arid designated as 'Using
such a terminolo, the random amplitude of the process is the maximum (in absolute magnitude) value of displacement within the random half-cycle between two adjacent zeros of displacement.
At points of intersection Of. 21-axis the phase trajectory is not, generally speaking, normal to the axis. The. ordinates of
the points Of intersection, i.e. values of the velocity of oscillations corresponding to zeros of displacement will be
called. the random quasiainplitudes of the velocity of
the
processand denoted it is essential that these values
of velocity correspond to zero values of the potential ener of
the oocl1ator.
The connection between the phase trajectory of the process realization
and
the joint probability density(x,V)
can
be explained as follows. Let us plotthe
corresponding elementary sections of the phase trajectory of the givenrealization over the phase plane for equally spaced moments of
time. Let us also select at point (j'
z)
a. surface element&c4)h. Then the relative number of the aboveelementary
sections of phase trajectory passing
through this
surface element is, in the limit, equal to probability elementLet us rewrite the joint prObability density of the displacement and velocity of nonlinear oscillations as follows:
p
f_[uitJ.
(53)
As noted above, the states of oscillator (viz, combination,
of
instantaneous values of displacementand
velocity) whichsatisfy the condition
E 7t)
U
3L(i)] +
it
z('t)
_
(5.2)
On the plane of variableB X1# the values of
E7t)
form a certain field, so that any 'duve on this plane is equivalent to the integration ofE7t,.)
over time. Let US substitute the variables in (5.1):*
'1
E, = C/
(x)+T7
(5.3).
The condition (5.3) is the equation of ener of the free nondamped vibrations of the oscillator with the reduced force function IL*(x). The period of these vibrations will be denoted
by.
('Therefore
the substitution of variables in (5.3)implies that a great number of all, possible states of the oscillator make up a totality of conditional regular cycles with periods Z("E*). At the same tUne thi substitution
repreaentB an integ'ation over time
(.5.4)
where the cu'vilinear integral is taken over contour
C
on the plane of variables XV- , satisfying the condition (5.3).The possible values of continuously fill 'up the
semi-infinite interval L -
0
, s is a continuous random value. .' At' the Same time, in contrast to random.valuea.xfr)
and tY't) , . is a countable randomvalue as arealization of random oscillations of any duration
T
contains a countable' number of1_va1uee.
The probability of the oscillator staying in the interval
of enr
levelsE± E+ CLE
will be equal to4
(&) o(
S,
where ci S is the area on the plane .Xit'between the contours C and corresponding to Slid.
As
()
5
.;.
V.p
(
;u';jc(E:)
p
jd
(5.5')
Integration of the left part over all possible values of gives the unity, hence
f(Ec)eLp(
LE=1.
(5.6)
F'om (5.6) we obtain ;the probability density for the time of the oscillator staying on the ener levels
?
(E:)
=
.2e
(
)
,C,
(5.7)
On the other hand, from (5.6) we have
(5.8)
.(5.,9)
(5.10)
probability calculated in terms of time. But
in
the variables£ ,. t the length of the contour ,' as it follows from (5.4),
j
21 S
)dEC
andthe, comparison between (5.8)
and (5.9)
leads to two conclusions. Firstly, we obtain the probability density of the enerlevels for random oscillations
7ç
(Ec*)Thus', irrespective of the individual eature.s of the oscillator,
the ener levels characterizing the equiprobable states under condition random oscillations of the class in question are
(cr
t)
-
L
?a()=
(
distributed according to the exponential law.
Secondly, considering, that the mean period of the
conditional cycles with the period. introduced above is equal to the mean period of the process Z , the amount
of
conditional
cycles in any realization of random oscillations of' T-duration as also the amount of random values of argumentis equal to the amOunt of random cycles in the same realization
We now tux'n to the discussion of the distribution law8 of the main characteristics of oscillations.
Supposing ?Y=O or .7C0 in Eq.(5.3), we obtain
E(eo).=
Q(0).
Here cZ° and are the amplitudes of conditional cycles, which will be considered as positive. The random values
a C
as a].so are continuous and countable at the same time, Substituting (6.1) in 5.1Ô), gives the probability
densities for the lével.s of' reduced potential 'and kinetic energy
of the oscillator
Tjw
0)
(6.1)
(6.2)
(6.3)
Al]. the possible values ofa°
belong to a set of positive extrema of displacement in a representative realization of' randomoscillations, but, generally speaking, they are not identical
*ith. this set.
The expression c7('a) is the maximum value of the reduced potential energy of the oscillator in the limits of the
conditional cycle. The mean (per cycle) value of this maiitude, as it follows from (6.2), is a parameter of the given process of rando oscillations. This parameter can be calculated in a
different way, i.e. as an arithmetic mean in the limits of the realization without recourse to the probability densIty..
On the other hand, in the limits of every random half-cycle of the realization in the positive domain of displacements, the maximum value of the reduced potential energy of the oscillator is determined by the main extremuni and is equal to
U('a0)
irreepective of the presence of secondary extrema in the limits of -the half-cycle (between the adjacent zero crossings).If the realization of oscillations is representative enough, the mean (per cycle) values CT*(a6) and must be equal in the probabilistic sense whatever the individual features of the oscillator and the duration of the realization, provided that this duration is long enough. However, the equation
:
UYa0)
=
(6.4)
where.
T
(6.5)
is the magnitude in the realization of both real (random) and conditional cycles, can be satisfied under the .circuinstanceaonly on condition that O It will be recalled that and
a°
are elements of one and. the same set of the positiveFor the noncorrelated disturbance
U(ci) .4$p f-
)
extreina of displacement. It follows from the above that a subset of a° is idetical with the subset of the random amplitudes Of process Q, , i.e. with the subset of the main extrerna
Similarly it is proved that the set of is identical with the set of quasi-amplitudes of velocity of process
The reverse of dependence
E:ca0)
is single-valued Ifu(x) ?
0
everywhere for()Q
Where for the zero position of the oscillator(x=c)
the restoring force has the peculiarities of the type U('O) ± U0 (the system with a set-up spring) or(x)= 0
if
j.xJ
(the system with a play) the single-valuedness will not be upset either. These conditions of single-valuedness will be considered as being fulfilled.Now according to the general rules the probability densities
(6.2,) and. (6.3). can be transformed respectively into the
probability densities of random amplitudes of displacement and the random quasi-amplitudes of velocity of oscillatiOns
I C
(6.7)
a-'O.
(6.8)
The distribution (6.8) was obtained by Crandall [2J earlier. As is seen, it holds for the' random amplitudes with any relative number of secondary extrema.Denoting
=
V(',). if
Q, ' andEc*
correspond' to One and the same conditional cycle (.5.3), we can
rewrite the probability density (5.7) as follows:
(a) = (4)
T
a.-O)
The distribution (6.9) referred to as the "probability density of the envelope" is obtained by Crandall in a different way for the noncorrelated disturbance [2]. The above
considerations make it possible to ascertain that. this distribution refers to the envelope of the main extrexna of
daplacement.
Prom this distribution, we obtain
-j.
f
[
It was probably Crandall r2] who was the first to use asiinilar expression in relation to the noncorrelated disturbance. Now we can state that this expression is exact and is not cozmeàted with limitations in respect of the form of Oycles in realization of random oscillations onwhjch Crandall's
reasonings are based. In particular this expression is not connected with a relative amount of secondary oscillations but it must be
applied to the random amplitudes of the process, i.e. to the main extreina.
Irrespective of the individual features of the oscillator, the oscillations of the class in question, along with the normal distribution of velocity, have, as it follows from (6.7), the Rayleigh distribution of quasi-amplitudes of ve.locity, i.e.
the
velocity values of oscillations for zero up-crosses of
displacement. This makes the quasiampljtudes. f velocity an
(6.9)
(6.11)
rimpotat
characteristic of oscillations. If it is aprióri known that the disturbance corresponds to initially introduced limitations, then you need just torecord. the momenta of
displacement zero up-crossings and the values of the system velocity at these moments and to use these as the empirical basis for the subsequent evaluation of parameters of
distribution in so far as the oscillations of the system with the biown force characteristics are concerned.
On the basis of (1.12), (1.13) and considering that for the
linear oscillator where the displacement
variance, we can rewrite (6.6) in the form
(6.12)
from which it follows that the random amplitudes (or the main extrerna.) of displacement are distributed according to the
Rayleigh law irrespective of the spectrum width of the process. This conclusion.is in agreement with the result earlier obtained by A.I. Voznessensky with respect. to the distribution of
displacement extrema for the "smoothed" realization.
At first sight it seems that the foregoing is at variance with the well known Rice law. As we are not in a position to
analyse this question in detail, we shall only note that the distribution (6.12) is in agreement with the Rice law.
For the nonlinear oscillator the condition
is of great importance; it shows that the mean level, of
oscillations corresponds to the natural state, of equilibrium of the oscillator, which implies that there is no. constant
limit is not essential since the restoring force is, an odd function, of displacement in re'lation to any origin of reading. Therefore, all the above formulae with relevant substitution of argument hold true for the linear oscillator also in cases when the disturbance does contain a constant component.
Now we shll try to show that the energy-equivalent double amplitude Q. Is, equal to the double mean value of the random amplitudes of displacement
Indeed, let us multiply both parts of this equation by the constants for the given process and write it in, the following
form:
f;fa) e)9.[
2j
(6.14).
ZJP
Ag. the quasi-amplitudes of velocity are diatribute4 according to the Rayleigh law, their mean value
Proceeding from the definition E , we. have the following
relation: or hence (6.13) (6.15)
(6,16)
(, 17)
(6.18.)
Assuming and making the substitution of variables,
we can rewrite (6.14) in the form
Hence We obtain Eq. (1.17)
Thus the assumption that
£?-
is proved. it should be emphasized once more that is the mean value of the mainSextrerna of displacement9 At the same time the ergodicity of the
processes in. question was confirmed.
The calculations using (6.11) are rather difficult since
the. period .*() for the nonlinear restoring force is
determined by an improper integral. The relations (6.13), (6.18) (6.15) result in the equivalent expresSion
1_
2
fZ1Yt)
?
AY2Jr4.-
(Ii
Which is free from the difficulty as mentioned above.
. (6.19)
(6.20)
may serve as the model of nonlinear system (1.1) else .
the
random oscil1atio .xj(-jof the
system (7.1), with a similar disturbance, will be equivalent accordingENERGY-EQUIVALENT STATISTIC LINEARIZATION OF NONLINEAR OSCILLATOR
iow. let us see on which condition the linear system
2.
.L
/21.
=
to some criteria with the nonlinear oscillations .X(&j'. of the
system (1.1).
Selecto4 of criteria for the statistic equivalence of
nonlinear and linearized random oscillations with particular reference to various applications or various engineering
problems may, generally speaking, be dIfferent. While studying the efficiency, strength, safety etc. of the mechanical systems which experience stationary Oscillations, the distribution of main extrema and average frequency of the process are of
paramount importance. Since the distributions of displacement
extrema of the nonhinearand linear oscillations differ in
principle, apart from the equality of average frequencies, only the equality Of averge random amplitudes of these processes may be required. As stated above the energy-equivalent
oscillations are determined by these two criteria.
It is seen from, par.3 that the restoring fOrce steepness of the energy-equivalent linear System must be
Hence .
(7.2)
where
Lt,
is the mean frequency of nonlinear osculationswith the given mean amplitude in the case of noncorrelated disturbance. The next analo is of interest. Let us compare the forced (regular) oscillations of a' nonl±near oscillator and "a linear one indüOed by the harmonic disturbance at a simIlar
amplitude and frequency. Then, if the natural frequency of the. linear oscillator is equal to. that of the nonlinear one at the
same amplitude, the moment of côrrelatiôn between the displace-ment of th'e system and disturbance will approximately be equal
r
in both cases.
and. potential
approximately The value
Therefore the: time-mean values of the kinetic energy of these oscillations are also
equal.
of is defined by equation (6.20) but for the system with noncorrelated disturbance
-f -
1
(
&7aj
?J)-'p--L
J
Let the value o be a parameter. Then in principle it is always possible to calcu.late approximately the integral and, as
a result to obtain numerical (or graphic) relation
('4).
We may proceed futher, however. In so far as the energy
characteristics are concerned there is no difference in principle between stationary irregular oscillations on the one hand and regular oscillations on
the
other hand, if the latter aredetermined by statistical values. As a matter of fact the mean frequency of stationary random oscillations is the frequency of reilar oscillations of the same dynamic system, whichina
statistical sense are energy-equivalent to random oscillations. The frequency W, is in accordance with the energy-equivalent
average cycle of free oscillatiOns of the system, that is a
cycle with an amplitude of a. Thus the average frequency of
the process in the case of noncorrelative disturbance
is equal to the natural frequency ca() of the System
provided that the amplitude is equal to the average amplitude
of the random process Q. This deduction is in particular agreement with some calculations carried out by Lyon
tJ
The velocity variance of random noncorrelated oscillations
i doterrnlned by the equation
Thus, knowing the function
-'v-el ocity variance
obtain the same relationship
The second parameter of the linear model should be determIned on the basis of the equal ener dissipation In both linear and nonlinear systems. The mean value of enerr dissipated in a
linear system is- equal to
2
and for the nonlinear system it is determined by the left part of-. equation (1.5). As thevelocity distribution of nonlinear oscillation is normal, it may be shown that
I
one can calculate the of random oscillations, that is
(7a5)
This equation is in line with the similar relatIonship derived by what is known as the equivalent linearization method. If the resistance la (v-jis expressed in terms of a polynorn,it can
be integrated to the final form.
The exact value of resistance law is
uown for the ship's
:i'olling as in many other cases. The most reliable data onresistance law can be obtained experimentally by the methods of
-free or forced oscillations
f5].
In both cases the empiricresui:ts are presented graphically as harmonically linearized
non-dirncn3ional coefficient of
rosictance (orwhere V
is the critical resistanóe) versus the oscillation;amplitude .X,. The employment of this relationship for the statistical linearization of resistance was described in Ref.f by the same author.
Using .the well-known methods of spectral theory the
velOcity variance ZvL
and the mean frequency of
linearized oscillationsai
can be calculated for the linear system (7.1) given the Spectral density of disturbance Since thesystem parameters, are functions of. the desired value it is
necessary that calculations be performed by using either the method of succesSive approximations or the method of 'aphic
interpolation. This problem
Will
be discussed later.In accordance with the present conception the obtained values of and should be considered as approximate values of the reSpective characteristics of nonlinear
oscillations
at
the same rate of disturbance,The value of will be used to determine
(4J
then by any of the methods the frequency of free oscillations of the nonlinear system can be calculated as a function of theiramplitude -"(. These data will be suff.cient to evaluate on
the basis of the above all the main distributions of nonlinear o8cillations.
In this case the linear model is used only for the calculation of the kinetic energy and the mean frequency of nonlinear oscillations, otherwise use is made of the
8. Now let us return to the calculation of velocity
variance of the linearized system (7.1) at given disturbance spectrum
S
(cv.i) and known relations and(i).
The analytic-and-graphical method involving graphic interpolatioxrequires
a
minimum of óalcuIation.Let us join interpolation planes and as shown in Pig.2, and. represent on them the curves and , respectively.
Then we take arbitrary values of fl (i = 1,2,3...) and (j = 1,2,3...); we shall' discuss rational se1ecton of these
]..ater. The velocity variane of oscillations,
4,.
is computedin terms of the standard
relationships
of spectral theory forevery couple of, values
(itt,
)
. After choosing the values of')
.,Dc'n,
etc. we plot the appropriate diagrams in the lower quadrant. The pointsa a
of their intersections With the curve /t(.) are transposed
into the upper quadrant (points
, , The curve' traced
through points , £...' is a function of
A?&z, ')/),
point
A at intersection of this function with curvewill determine the required value, of
M
(ne,
)?L),
nd hence the value Oftl(VL).
in fact small arcs of curves c4,..
(ne, Vj), oV.. (n
'1)are ãidently required in the neighbourhood of their
intersections with curves of and
respectively; these arcs 'can surely be plotted by three or four
points. Thus, it will b.e enough to carry out calculations just
for 3-4 values of at 3-4 values of frt for each of the
within.the selected range of variation and '. Experience
ghows the latter condition can easily be fulfilled.
§9. In some cases it may be desirable that instead of the method described in par.7 a less exact though more simple method
should be tided for the calculation of nj()
which willpermit integrating in closed form 'with the function of. U
()
given by, a p.olynom.
Under condition8 of noncorrelated' disturbance all possible
states of' nonlinear oscillator, aais seenfrom equation (5.3),
disintegrate the totality of its free nondamping cycles.
Substituting of for
U(x)
in (5.3), and using (6.1)le
obtain after inteatiOn by parts the equation
Ji
)
d
fx
u
(x) ,' (9.1')which is satisfied by any free cycle0
Let us replace each nonlinear 'cycle by a linear one with.
the same amplitude, and choose the restoring force steepness of the linear cycle on the assumption that the velocity riancea of both cycles are equal. In this case the cycles will be energy-equivalent. Since in the general case the
velocity variance of nonlinear cycle is not obtainable in closed form, we shall assume that the equality of the velocity
variances of the cycles compared will be satisfied provided' that the left-hand parts of equations (9].) forthese cycles are
equal. This assumption is the more exact the less the nonlinear
cycle form differs from the harmonic one (or is trajectory
fri
an ellipse). . Then the energy equivalence of the cycles comparedare, equal,
which
results inL i2(aj a3
-f U (Z)
dx.
3
"0
On the other
hand,
the velocity variance for the linear cycleI1fU2Jc
2('a)
a.'
(9.3)
'or
considerIng (9.2)/k/[UL]
94
Then let us average the equation (9.4) over the totality of linear oscillation cycles and. hence in the left-hand of the equation we shah. obtain the velocity variance of the process
f f
(9.5)wee
is the probability deflsity of the random amplitudes of the linear cycles, namely the Rayleigh, distribution. The velocity ariànce.'of the linearjzedoscillations should be equal the same for the nonlinear oscillations compared at the same level of exitátion. On the
other: hand, for the linearized oscillations in the case of
non-correlated disturbance
,where 4L is the
variance of their displacement.
'It should be emphasized once more that the variance is not equal 'to the variance of nonlinear oscillation displacement
To facilitate the comparison between 'the excitation levels of linear and nonlinear systems, it is desirable to have some reference for which purpose use can be made of the degenerate
nonlinear system with restoring force
a30x,
wherefor which (system)
4
The energy of levelexcitation will be the same in: the systems compared. if
=
/aL
0X4Then introducing the desiiation
u ()
-
ü
(x)/c&
(9.6)
(9.7)
and choosing the normalization factor in the. Rayleigh law asequal to. , We obtain the approximate calculation formula.
.3
. Cf
z2
r
:..JI__ -h?aI.xu0(x)dz,
(9.8)
(. 0Z
I
.J
which will obviously estimate at the same time the mean frequency fl of the nonlinear oscillations With
non-correlated disturbance.
This expression is inteated n closed
form if is given by a polynom.
The nonlinearity of the analytically expressed restoring force scharacterized by some parameter. If value is
taken a a scale unit.of this parameter then the identiàal dimensionless values of the nonlinearity parameter will have a corresponding comparable level of excitation in the systems
ôompared. Thö spocific conditions providing for the agreement between the disturbance levels are. dependent on the. function
u.j.
characteristics so when 'determining these conditions account must be taken of relation (9.6). SOme examples areCOMPARISON OP THE STATISTIC LINEARIZATION
IVIETHODS
The efficiency of the ener-equivalent method of linearizE tion of random oscillations can be estimated by comparing it with exact solutions. AU. known exact solutions relate to the case of excitation. by "white noise" namely to noncorrelated
disturbance.. Owing to this, only
formulae for W
can be verified. Equation (7,3) is exact,. so let us ilustrate theaccuracy of approximation (9.8) and the associated approximation of random oscillations for noncorrelated disturbance. At the same time we shall carry out a comparison wIth the data obtaied by the method which is knOwn aB the method Of equivalent
statistic linearization,
10. For the rnass-spring-setup system. excited by "white
noise" [7]
4=
where. spring, stiffness factor (per unit mass.).
In this instanàe Crandall obtained an exact analytic solution
[7:1;
Proni:equation (7,3)
?
z0)
(z0 £
F0This integral is tabular
f
8, integral 3.4633 that is the exact value of the mean frequency of the process involved(10.3)
The use of the exact equation (7.3) based on the
ener-.
equivalence conception made it possible to avoid complications resulting from the other approach to this problem [7j.
Now let us turn to approximate values denoting them by asterisk, Having performed the integration
ii (9.8) for the
case under discussion, we have
xc,
(].O.2.
(10.4)
with E0 to.be determined from (10.2)
as before.
Then we find a condition with the satisfying of which the non-dimensional value of nonlinearity parameter E0 will be of
the seine magnitude in..both lineai' and linearized systems. The
disturbance level is estimated by the statistics of the
degenerate (linear)system
4
and , with. the value ofexcitation level in the degenerate system to be corresponding to that in the linearized system, using both criteria. This
viill be the case if. the average work of disturbance per cycle
je the same in both yaterns. But the average number of cycles,
per unit time is different in these systems, hence the above-mentioned correspondence may be aóhieved only if spectral dénsitjea pf disturbance in them are different.
Let the spectral density of disturbance 'of the linearized sythtem in which the correspondence is observed be
where spectral density of disturbance of the degenerate
(and hence noitlinear) system. Then by Virtue of (9.6)
Simultaneously. we must have
'-,
(10.6)so that the correspondence in respect of displacement will be preserved. Eliminating ii from, these two equations, we find
av-(10.7)
This is the value of at which E0 is the same both i
nonlinear and linearized Systems.
It may seem at first sight that the enerr correspondence between the linearized, and degenerate systems will be upset in thjs case. However there iá no 'ound for such doubt.
om
(10.5) and (10.6) wehave
and velocity distribution of oscillations in the linearized System is
'1tT
But thiB is the normal
dtrjbutjon with variance
(w)
(v.*)=
.I
0 j7,O (4,('.1cA
(10.5)as it should be.
Prom equations (l0.4).an (1O.7)we derive approximate
energy-equivalent statistic values of the nonlinear oscillations
1(f+
Though is the displacement variance of the linearized system it should be equal, as it follows from the foregoing,. to
relation rather than. to the displacement variance of the nonlinear
system
On the contrary, if the displace-ment variance for the linear system is equal to that for the nonlinear one then the mean values of oscillation amplitudes ofthese tWo systems aredi'fferent.
Pig.3 and 4 give the following collations for the
appropriate statistics: the exact values, estimatjons obtaine4 with the
help of
what is kiowns equivalent linearization'method, estimations from the formulas (10.8), (10.9), the exact values of relation are shoWn in Pig,3 by points
(the Other
curves
are shown below).Then we find the appro.mate values of the probability
density for thenonliñear oscillation envelope..
Let us consider equation (9.2) as an approximate formula for natural frequency of the nonlinear
system
t()
,f
(x)d,
(10 10)O
whch for the given problem results in expression
=
(10.8)
a)0.
(I. .3
E0o
This expression should not be used at
c20 --
0.
Substituting (10.11) in (6.9) we get an approximate formuia for the required probability density
12 (Fc)
I +
(10.12)
x
Fig.5 shows for 1 the comparison between the exact
value of ( (no)
and the value o± obtained from formula (10.12) provided that)() is
estimated from formula (10.8), and also the envelope, distribution for the approximately energy-equivalent linearized system.The collation in Pig.3., 4 shows that even though
approximately realized the energy-equivalent linearization is preferable to the equivalent linearization, since even with a 8iiificant: nonlinearity of the system it allows making an adequate estimation for the most important statistics of the nonlinear oscillations, viz, the mean frequency. ' and the mean amplitude . It will be recalled that, the precom'ession of springs that is equal to almost one and a half standards of degenerate System'displacernent Jfr corresponds to the value
'of
E01.
The approximate estimation of the probability density of the nonlinear oscillation envelope (Pig.5) is also satisfactory.
Now using the same example we check the assertion
V
IC
(10.14)
Further let us caThulate the exact time-mean value of the square of displacement for the nonlinear cycle
-system at an amplitude of oscillations equal to the amplitude
of the enorgy.-equiva.ent cycre.
For a-aplitude free
oscillations the exact valuef 7]
ofthe system natural frequency is determined by expression
(= ,/a)
2Jc
e ,tza
6/,t
tüQ
,
-'-..
The equivalent cycle is linear
and
for itiç r2(t L
L
a
a
(10.13)
(10.17)
Denoting the relation, of the left-hand parts of (10.15) and (10.17) by 2.,
and
making some imple but somewhat unwieldy calculations we obtain . .J
(10.18)The enclosed, in braces in this.expression is a.radi.cálly
Infinitesimal diffrence, hence computation should' be perfo'med with 'eat precision (viz. 6-7 siificant digits in the minuend
is the relation beweenthe square root of
displace-ment variance of the nonlinear cycle and that of the energy-equivalent (linear) cycle, the amplitudes of these being equal.
Consequently if is expressed as then
=
(10.19)Taking into consideration equation (10.2) we obtain
=y
in passingfrom parameter E to , accepted earlier.
On choosing the values of e and carrying out calculations
fr
(10.13), (10.18) and (10.20) we obtain relations &()
and E0
(54
, i e. parametric form Of the dependenceof the natural frequency of the ener-equivalent cycle on parameter E0.
Pig.3 shows the values of It is seen that
is in agreement with the exact value of
0(E).
If we iiOrethe difference in the form of cycle between the nonlinear .oscillaiions and the linear ones (ellipse), i.e. if we assurnO
we shall obtain the results plotted on the graph of Pig.3 as points. In this case the effect of the form of cycle may practically be neglected. .
Similsi' calculations though not associated with the concept of the energy-equivalent cycle were carried out by Lyon f4Jfor. a nonlinear hard-spring oscillator described below (par.11).
These examples confirm the possibility of calculating, the frequency as the natural fre4uency of the energy
equivalent regular cycle in a nonlinear, system.
It follows from the above .that the accuracy of estimation with respect to the distribtition of elements of the nonlinear
oscillations is essentially dependent on the accuracy of
estimation of the mean frequency of the process in the case of the noncorrelated disturbances Therefore the ener-equivalent
method of estimating this mean frequency aà the natural
frequency of the oscillator at an amplitude equal to the
ener-equivalent amplitude of the process provides for an accuracy which is quite sufficient for the calculating of characteristics
of nonlinear random oscillations in case of normal disturbance.
ll. As a second example we shall take a hard-spring
oscillator (Duffing's problem) the random oscillations of which due to excitation by "white noise" were considered by Lyon [4],
[9]. In this case no general analytic solution is knownand
the exact values quoted below are obtained by numerical
inteatjon.
f9J.
The force function of this system can be presented as
.r?
k(x)
(x
)
(lll)
where is the nonlinearity parameter. Its dimensionless value is
(11.2)
where is again the variance of the degenerate system displacement for the given level of disturbance. The same dimensionless values of this parameter in both nonlneár and linearized systems will evidently be available if
in other words, if the systems have the same values of velocity variance.
Then, from equations (9.8) and (11.3)
may. be Written as
XQ0p
7
1/y
(1+
,.4)
(11.3) (11.4) (11.5) (11.7 )In.Pig.6 for the statistic of
'o/"4)
there are compared: the exact value, the ener-equiva1ent value defined from (11.4), and the one obtained by the method of equivalentlinearization,
Compared in Pig.? for the statiStic of
are; the exact value, the value from. (11.5), the value estimated by the method of equivalent linearization.; the exact value of
The free oscillation frequency
of the system (ai/p)
being estimated similarly to par..1O
11.6)
0
T/z
J-0
is shown by points.It can be stated that even for this case of a hard-spring oscillator the approximately realized energy-equivalent
linearization provides an appreciable decrease of errors in the estimation of main statistics of nonlinear oscillations viz. the mean frequency of the process and the mean value of
oscillation amplituth. 2 as compared with the method of
equivalent linearization without any complication of calculating
formulae. . At ,4,
I
the errors introduced by the equivalentlinearization method are O.l2&)4 and O.l2,t/ respectively while introduced by the energy linearization performed
approximately these will be O.04&o
and O,O4V. The latter
can in most cases be considered as reasonable for technical applications. At the given value of the rate of
npn-linearity of the system is appreciable, i.e. for a displacement equal 10
jfxo
the restoring force is twice the value of the linear part.The exact value of probability density Was not computed in this particular case. Therefore a comparison is given in Fig.8between the approximate distribution (11.7) and a similar (Rayleigh's) distribution of the energy-equivalent linear system in order to illustrate the difference.
The comparison between Pig. 5 and Pig.8 shows that the
difference of the envelope distribution of nonlinear oscillations from the Rayleigh distribution is largely dependent on the
References
1. Grim, 0. "Nonlinear Phenomena in the Behaviour of a
Ship in a Seaway", XII Intern. Qwing Tank Conf., Proceedings, Rome, 1969.
2, Crandall, S.H. "Random Vibration of the Nonlinear
Systems", Random Vibration, vol.2, editor S.H. Crandall, MIT Press, 1963.
Kauderer, H. Nichtlineare Mechanik, 1958.
LyOn,. R.H. "On the Vibration Statistics of a Randomly Excited Hard-Spring Oscillator", J. Acoust. Soc..Am., vol.32,
N6, 1960.
Blagoveshchensr, S.N. Spravochnik po teorii korablya
(Reference Book on Ship Theory), Sudpromgiz, 1950.
Gerassimov, A.V. "Statistic linearization of rësietancè to rolling motion" (in Russian), J. "Sudostroieniye", 4, 1971.
Crandall, S.H. "Random Vibration of the Nonlinear Systems with Set-up Springs", Tr. SNAME, S. E. Appl. Mech., vol.29, N 3, 1962.
Gradstein, IS., Rigik, I.M. Tablitsi 3.ntegralov, suzin,
ryadov . proizvedeniy (Tables of integrals, sums, series and product8), Izd. 5-e, Nauka, M., 1971.
9. Lyon, R.H. "Equivalent Linearization of the Hard-Spring
Pig.l. Agreement between a random cycle of v1bratonS and
its phase trajectory.
3,6 -. the main extrema of displacement; 1,2,4,5 - the
secondary extrema.
Pig.2. Scheme of graphic interpolation for determining the
parameters and of the linearized
system.
Pig.3. Values of 'the ratio as a "function of the
dimensionless nonlinearity parameter , for a system
with set-up springs.
1 - exact so].utioñ [7]; - calculated by the equivalent linearization methoaE7J3 - calculated from formula (10.8);
4 - exact value for a regular cycle; 5 - the same without taking into account the shape of the cycle.
Pig.4. Values of displacement statistics as a function Of the
dimensionless nonlinearity parameter for a system with set-up springS.
1 - exact value' 4/J0
r71;
2 - value.obtained, by the method of equivalent linearization
L71;
3 - value