NOTE ON
THE POSSIBLE USE
OF APERFORATED, VERTICAL-. WALL BREAKA TER
By
G. E. Jarlan
Hydraujj.cs 'Laboratory National Research
Council, Ottawa,
Canada
Introduction
with a solid, taking
Into account the viscàslty of the fluid than would be expeáted.
that In many cases sound penetrates
porous bodies more freely been the object of
exhistve
studies, particularly in acoustics. Stokes and Kirchoff
Investigated the, motion of air in contact
arid the effect due to heat.
They arrived at the conclusion
The problem of wave reflection at a porous wall has
If a continuous perforated but flat,
vertical wall Is placed perpendicular to the direction
of propagation of
acoustic waves, part of the wave energy will
be reflected wtiile
the remainder of the energy will be transmitted
or dissipated through viscous friction and heat. The perforation
may, for
Instance, consist of a series of uniform circular channels of a diameter much smaller
than the wave length of the vibrations
imposed. VIScosity and heat
losses may be neglected in a
simplified stucy of the
characteristics of the reflected wave.
If the origin of x
is taken at the face of the wall, the one
dimensional equation of the wave
propaga-.
L
tion may be written [ila =
eIoX
nt) + BeI(koX - nt) (1) >x / where a =ei(4x
+ nt) cos(k0x + nt)Is the incident wave with k0
e being the Sound velocity In air
and
n the frequency. The horizontal velocity componentIs given by
u = c(_e 0X +
BsiOX
nt)B
K(1)
- K0K(1+g) + K0
-2-The ratio of u and a near the wall is found as a first
approxImation by putting x O in (1) and (2) so that
- , B being the reflection coefficient.
For a thin wall, i.e. for a length of channel very small compared to the wave length of the perturbation, the mean
pressures are aproxiiately the sanie at both terminations of the tube. If
(u
denotes the area of the unperforated partof the wall and cI'p the area of the perforated part, one has:
n
6
c(B-1 (6u
+ p)which gives the relationship between the inside and tside motion
Using the continuity equation,
(1
(r
n a d 6 + K
J (
udr
= 0; 6=. cross section areaof the tube,
the expression for B, as derived by Rayleigh, may be obtained
with m-
-where K
le a ñmction of
n and c, of the channel radius r and of the speciflc heat of air. If one assumes K = K0 , thenni
2+m
for ni = 1, B = 1/3, and the reflection is small.
These results suggest that a similar phenomenon, as
far as the reflection is concerned, mIght occur when water
is
the fluid In oscIllatory motion,; Consider a chamber, one wall
of which has a serles of perforations equally dIstant from each other, placed In an infinite liquid.of depth equal to its width. When the wave impinges s;aint theperfcrated wail, part of the
energy Is transmitted through
the
circular holes, the rest being reflected or dissipated through friction at the solidboundary. The chamber will then aJternately fill and empty,
the oscillatory motion at the perforated wail being graduaJ.iy
transformed Into a mass transport through the holes which
forces the
lIq'Lidto arrIve in the chamber in
the
formof jets.
If
Hs the hydrostatic head rorrespondig
to the ma.lium of
the crest elevation at the
ai.l,
thevelocity of the jet will
bey =
\J2gHif H
Is coistant,
Thejet
pressure Po to a pressure Pi through an orifice of cross-section iill be accompanied by a change of momentum in the
direction of the velocity0 It is difficult to analyze the jet
problem 1f lt is to be studied as a manifold fibu with a
certain number of holes being submerged only part of the time and where pressure fluctuations follow a harmonic law.
Mass Oscillation in a Tube
The flow in a single tubé will now be examined, under the assumption that the motion Is laminar and the hole always submerged, using a simple device which will help to retain the physical principle Involved In such a casé. Two tanks filled
with water, open at the free surface, are connected by a tube, sufficiently long with respect toits diameter. A plunger,
subject to a harmonic motion, generates a forced wave in the
tube. The system being initially at rest, the motion In the conduit results
from the superposition of an oscilla-tion proper to the system and of the
I forced oscillation. Experience shows
I that the first type of oscillation
I disappears after a while and that it is I the forcéd oscillation which Is of
oL_J
Interest. The liquid oscillates In every point of the cross-section of thetube with .a period equal to the one
Imposed by the pistons. For a long and
narrow tube, one may observe that a phase difference tends to
occur in the motion of the liquid.
With O X representing the axis of the tube, the
Navier-Stokes equation is written as
Y:-!i'
J/Ò'V ,._/_V
òic
rer
t'SP'
where y is the velocity component along O X , is the pressure gradient such that '- = , r Is an
arbitrary distance on the radius of the tube and t) is the kinematic viscosity. V may be assumed independent of X if
the tube is very long. The boundary conditions are simply
y = O , r at the wall. exi(2) obtainéd for
V the folowing express1on
which shows that the velocity in the tubé involves two
terms of similar period and .amDlitude, out of phase by (R-r). A wave
amplitude0 For R very large and neglecting capillary zi
hysteresis, the relation gives V =
. Hence, an
axial symmétric mass oscillation tak
place in which the
velocity at the walls is greater than in the
core (Richardson annular effect)
When the motion in the tube is turbulent, a jet forms outside the tube. It is presumed that the
theory of wakes may be applicab]e to the case of. the jet, completely
self-preserving flow di pearing at a distance close
to 50 diameters from the orificeU'), The velocity distribution In the jet itself is importánt if one wants to study its subsequent
diffusion
within
the liquid0 Assuming the ratio of theReynolds shear stress
to the mean velocity gradient to be constant,
it Is possible to
use a velocity distribution similar to the
one observed -In a wake. This velocity
distribution may be represented by an error function with appropriate coefficients.
The study of flow establishment (se Tolimlen) shows that the
entrajnner1t o' the
surrounding fluid by the expanding turbulent region Is Inertially
balanced because of a continuou3 reduction of the velocity
with-in the jet Itself0 The shear exerted
longitudinally as the jet
occurs may be defined theorétically
using the Prandtl concept of mixing length. Practically, it Is
impossible to measure the
eddy viscosity coefficient within the jet.
If the circular
wall is not smooth, large eddy motion will take
place originating
from the artIon f forces normal to the
wall which In turn will
affect the edd- viscosity
and consequently the velocity gradient.
Across the surface of the hole, there exists an average pressure from the incident gravity wave.
This pressure acts as a driving force on the water in the hole,
thereby causing variation in the level Inì the chamber.
The flow In the tube being turbulent the resistance
coefficient to flow must be taken into acount.. Assuming the head loss
term to be of the form
r/2D(v/2
the differentialequation of the motion of the free surface in the chamber would be
tt
(i
2L.b
where f = frictIon term, F
driv±ng force. 2 7 /T,
-
= a distance,
yvertical notion. This equatloc is not easIly integrable because
of the nonlIner
errn bu an
approprIate solution cn be obtamne usir'
serles developmen
and Rieman Int-egríition methods.In order to fix the ideas, simplification may be made
whereby the above system may b,e represented by
a niase-spring-resistance mechanical system subject to a harmoç4ç driving
force F1 sin t. The equation of motion
is
,<*wX zF,Sc-w
);
,K=
'-t
A general expression for X is:
x
,j f4#. (w t cp)
W.
,
,,-2Kw
9
cút
4The term q
= 1/[:?
-1 #4Kc4/,3
w*)
-is the magnification factor. Plotting
q against W , one
obtains a.tuning curve which shows that the
high damping response
is fairly flat, After a calculation
of the appropriate coeffi-cienta, being a purely resistance impedance, it is possible to study the law of motion of the water level in
the chamber.
Breaater
A large amplitude gravity wave reflecting on a plain smooth vertical wall will create clapotis, the
amplitude of
which may reach 190 percent of the incident wave height, the accompanying wave set-up being of the order of 10
to 20 percent of the same wave, Thus,
the pressures and subsequent dynamic loads exerted on the wall ere important,
The stream lines of
the clapotis which
approximately represent the trajectories of the water particles are such that the horizontal
cponent of
the motion at the nose In the vicinity of
the structure are very important,
Consequently1 this horizontal force will tend to
exert in shallow water important shear stresses on the bottom, Erosion may then occur which could endanger the stability of
the vertical structure. Moreover, the breaking
of the
clapotis is inevitable in
shallow water and the subsequent
elaStic forces developing In the structure
end in the joints Is detrimental to good stability. A simple well-known
rule
may thus be Inferred whereby
a vertical structure must nevèr be placed In shallow water.
¿p,
-6-One must then have recourse to rubble-mound break-waters which dissipate the wave energy through
mechanical
friction in the porous medium, the amount of energy passing
through the breakwater being very small for short-period
waves
However, in areas where no stone is available (and
this occurs frequently In
Nova Scotia or Prince Edward Island) the construction of rubble mounds involves heavy
transportation costs having a noticeable bearing on final cost and maintenance budgets.
Consequently, it appears desirable to study the
feasibility of prefabricating a caisson which would offer the
same advantages as rubble-mound breakwaters but would not involve the disadvantages Inherent to the use of vertical structures in shallow water.
In view of the above theoretical considerations, it
was felt that a caisson with
a perforated sea-side wall could
be used as a breakwater, provided that lt would
not reflect
waves to a great extent and assuming that it could be
adequately
designed to resist the dynamic loads exerted by waves. Two-Dimensional Model Studies
To study the conditions
of the reflection of the wave
against a perforated wall a parallelepipedic chamber was built Involving a plain vertical wall made of concrete to the scale 1/30 (FIg. i and 2) Tests were made In a
wave flume, the equivalent prototype depth being 30 ft. The dimensions of te perforations were calculated In order to
obtain a ratio
m = 0J9, the
length
and diameter of the holes representing about 1/loo of the wave length of a deep-water wave of period 8 seconds. The impedance of the holes is thus
sufficIent to ensure a noticeable phaeè shift
between the wave
motion outside the chamber and the fluctuations
of the water level Inside, The reflection coefficient was first
investigated and it. was found that
this varied (for non-breaklng wave) as a
function of the wave camber, between 1G and. 20 percent.
It was also observed that the phase shift between the maximum water
elevation at the watt outside and inside the chamber varied from 50 for small camber
waves to 120° for high camber waves,
the amplitude of the fluctuations In the chamberbeing always smaller than the amplitude of the motiôn at the outside wall. These results are indicative of' the
effectiveness of the
Impedance for transforming
the oscillatory motion of the liquid into a mass transport. The horizontal
component of the velocity
being largely reduced through jet diffusion,
one maInly observes
in the chamber variation
of hy:rostatjc pressure somewhat similar to the one which would be observed in
a surge tank
although the damping conditions of the level fluctuations are
From this exploratry test enes lt can be inferred
that the width of the chamber does not
appear critical; in
-other words, the damping thaide the chamber was suffIcient
80
that no resonance, similar to the case of the Helmholtz
resonator, could develop. The selection of the width of the chamber would thus appear to depend merely ori the wave heights occurring at a given site.
From the fluid mechanics viewpoint, the
conditions
of dissipation of the et diffusing into a liquid niass subjectto an oscillatory motion la a challenging problem and lt is not
known how much the dissipated energy dampens
the energy of the incoming wave. Howeve lt could be observed that with suffi-ciently high wave camber,
the wave motion at the wall was
some-what reduced as compared to the incident wave height.
The
diffusion of energy Int the liquid mass creates an extra turbulence near the wall which is prone to exert a damping
effect on the wave front close to the perforated
wall. It was also observed that as jets penetrated Into the chamber,
bubbles of entrained aIr were carried down
into the water by
the jet. The presence of this
air should somewhat affect the amplitude of the vertical motion of the free surface In the
chamber (FIg, 3 to 9).
Bed Movement
Observations in a two-dimensional fltvne showed that,
as the chamber empties,
a fairly Intense current perpendicular to the wall Is
Induced
by the jets in the vicinity of the freesurface. Although all holes involve
a jet action, the latter is more important near the surface, which Is to
be expected.
Hence, according to the principle of continuity,
there exists
a circulation which takes place in a vertical plane.
Some exploratory tests were run in connection with the transport of material under the form of
a bed load. These tests showed that the material which penetrated
Inside the
chamber was evacuated In
the vicinity of the surface through the upper holes, The turbulence induced
In the chamber by the Jets appeared to be sufficient to permit the solid particles
to be lifted by vertical upward currents taking place In the
chamber, The material used in
these tests was a fine sand of
medIan diameter equivalent to 0.1 nni.
Remarks
The presence of this surface current would be an asset in areas where ice
floes occur during storms since the drift induced by the jets iould tend to damp the
momentüm acquired by the ice under the influence of combined wind and
Run-Up
Figures 10 to lL. show a two-dimensional impact of
a
wave against a plain vertical wall, the Incident wave height
being the same as the one imposed for Figures
3 to
5.
It maybe seen that the shape of the free surface is considerably
different from the one observed in the case of
a perforated
wall. The tests showed that
the run-up over the structure
was not very large, even in the case of waves at the wall
breaking partially0
Erosion at the Toe
Placing the structure on a rubble-mound mattress with
natural slope, it was possible to observe that the stability
of the mound was not Impaired,. No stones were displaced
for wave heights of 15 to 18 ft0, the total depth of water being
equivalent to
36
ft. The average weight of the stone unitswas
equivalent to 200 lbs. No strong pumping action
could be observed at the toe.
Combined Breakwater and Quay Wall
On the basis of the flume results It is feasible to conceive a structure which could be used as a combined
break-water and quay unit, as indicated in Figure
15.
Such a struc-ture could be built 10 or15
ft0 above the highesttides. The design should involve bracing of the chamber made of porous wall so as to allow equilibrium of the level to take place
rapidly for a wave Impinging at the wall under a given incidence. Such a structur3 should be competitive, in spite
of the possible
difficulties involved in order to prevent Important
shear
stresses from occurring around the holes and to take care of accompanying phenomena such as transient cavitation developing
at the walls of the holes,
BIbliography
1.
Rayleig.
"Theory of Sound".(Dover) , New York.
20 Sexl "tTher der von E0G0 Richardson entdeckten Annular
Effect". Zeitschrift der Physik,
1930, p. 3L9.
30 Townsend "Structure of Turbulent Shear Flow". Cambridge University Press.
¿ To1lrnien W0 "tTher die Entstchu.ng
der Turbulenz, Nachr, Wigs., G8ttingen (1929).
5
MacLachian, NW
"Theory of Vibrations".(Dover) New York.
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