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NOTE ON

THE POSSIBLE USE

OF A

PERFORATED, 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 [il

a =

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 component

Is given by

u = c(_e 0X +

BsiOX

nt)

(2)

B

K(1)

- K0

K(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 part

of 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 area

of 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 , then

ni

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 solid

boundary. 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'Lid

to arrIve in the chamber in

the

form

of jets.

If

H

s the hydrostatic head rorrespondig

to the ma.lium of

the crest elevation at the

ai.l,

the

velocity of the jet will

be

y =

\J2gH

if H

Is coistant,

The

jet

(3)

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 the

tube 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

(4)

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 the

Reynolds 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 differential

equation of the motion of the free surface in the chamber would be

tt

(i

2

L.b

where f = frictIon term, F

driv±ng force. 2 7 /T,

-

= a distance,

y

vertical 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.

(5)

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

t

4

The 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)

-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

(7)

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 subject

to 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 free

surface. 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

(8)

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 may

be 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 units

was

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 or

15

ft0 above the highest

tides. 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.

(9)

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