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MOUND BREAKWATERS UNDER WAVE ATTACK

By Miguel A. Losada

Luis A, GiménezaCurto

Department of Oceanographical and Ports Engineer ing

University of Santander Santander

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CONTENTS

No. page

Introduction ?

Chapter 1. Flow characteristics 7

Introduction y Flow Chatacteristics under regular waves 8

Breaking jO Run-up and run-down 12

Reflex ion 2I Transmission 28 Interaction curves 28 Flow characterisitcs under irregular waves 31

An experimental comparison 40

Conclusions 4 5

Chapter 2. Mound stability 47

Introduction 4 7 Stability under regular waves 48

General statement 48 Stabi lity criterion t>2 The stability function ' 56

Experimental data 5 6

The fit model S8 Randomness in the structural response.

Confidence bands 66 Interact ion curves 71 Variation of stability with the slope angle 77

Stability under a sea state. The failure

probability 33 Conclusions go

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No. page

Chapter 3. Oblique wave attack 92

Introduction 92 Flow characteristics on a slope under oblique

regular wave attack 92 Stability of rubbl.e : mound breakwaters under

oblique regular wave attack 93 The stability of rubble mound breakwaters

under a .sea state with oblique incidence 104

Conclusions 104

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~3-INTRODUCTION

Until well into the 60's the only possible option to calculate a rubble mound breakwater was to use the deterministic classical formulae and to carry out experiments with regular waves. At that time laboratories began to incorporate techniques for the genera-tion of irregular waves in their exper iments regard ing breakwater stability. This new technique was not accompanied by a critical analysis of results; specially in the wide variation which must be expected as a consequence of the randomness of the structural response and wave attack.

It is common pract ise in laboratory ' reports to say that a spe_ cific section of the breakwater is stable under the action of a -sea state defined by certain determined parameters. This conclus-ion has normaly been obtained after the carrying out, in the best cases, of three experiments keeping the same sea state parameters.

It is clear that these results, obtained from a very small num ber of tests on an infinite sample space, does not provide guaran tees of stability of the construction under the action of this sa me sea state and even less generalisation of conclusions. This state of the art will continue to exist, on the other hand, for as long as causes of the phenomenom are unknown.

The attitude adopted by the designer of rubblemound breakwaters when choosing among existing calculus methods, should be

compati-ble with the actual phenomenom, bearing in mind the errors and im perfections of the method that he uses and attempting to evaluate the degree of uncertainty in his results.

We do not intend here to recommend the use of any one specific calculus method. This decision is the designer's priority. However,

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-4-in view of thé most recent research and results of this study, it appears reasonable to emphasise the high failure risk which exists calculating rubblemound breakwaters with the deterministic classi cal formulae.

Bruun (1979) has synthesised possible causes of failure or bre aking in rubblemound breakwaters. Localization in the construction of the eleven possible causes of failure can be seen in figure 1.1 Then eleven possible resulting damage_type^s are the following: 1) Knock-outs of single main layer units due to wave action. These

knock-outs can cause breaking in the armour units with a conse-quent weight loss and, therefore, jeopardise stability.

2) Lift-outs of main layer armour units by wave action, this being the commonly considered damage.

3) Slides of the entire main layer as a whole owing to lack of fric tion with underlying layers. This damage will occur, in general, on very steep slopes.

4) Gradual breakdown or failures due to fatigue because of continuous movements of the main layer armour units without great -displacements, this means that small initial damages can be im portant fof the definitive stability of the structure.

5) Scouring of the crown base or wave screen.

6) Damages in the inner layer (protected zone) due to overtop of the breakwater and overwash onto it.

7) Damage due to a lack of compactness in underly ing layers which allows water to flow inside, causing great lift-out forces on the crown and inner layers.

8) Toe erosion scouring of the lower part of the main layer. 9) Soil failures due to the low bearing capacity area.

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10) Discrepancies in the characteristics of materials used in construction. When quarry stones are used fundamentally, what can occur is that the armour units are.of different sizes, specific weights, etc.

11) Failure due to poor construction, which can leave weak -points in the structure.

It is obvious that there is no reason why these types of damage should occur in isolation, but that several of them -could arise at the same- time.

The subject to be discussed below, is flow characteristics on the slope and its structural stability 'from' '

-the point of view of damage 2, although damage types 1 and 4 will also be considered.

The analysis method to be followed consists of the following steps:

1) Analysis of the idealised model of the rubble mound breakwar, .•ter (undefined slope) under regular wave action. This

ana-lysis will be basically on. a empirical nature, being based on experimental laboratory results.

2) Application of regression techniques in order to obtain some behaviour models^

3) Determination of interaction curves, which quantify the pheno menom in a diagramme (H,T).

4) Application of the hypothesis of equivalence between regular waves and irregular waves.

5) Probabilistic analysis of the phenomena when the wave attack is a sea state.

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7

-CHAPTER 1 • FLOW CHARACTERISTICS

INTRODUCTION

Use of Iribarren's number, Iribarren and Nogales (1949), in the analysis of flow characteristic on sloping structures, was introduced by Battjes (1974a and b), who applied it to the cah se of flat slopes.

Ahrens and McCartney (1975) verify, by means of experimental results, the usefulness of Iribarren's number to describe

runup and stability on rough, permeable slopes, and furthermore -propose a fit models

This line of work was later followed by Bruun and Günbak (1976, 1977, and 1978) and Bruun and Johannesson (1977). Losa-da and Giménez-Curto, (1979a), propose an exponential-type mo-del, as a function of Iribarren's number, for stability of ru-bble mound breakwaters, introducing, on the other hand, inter-action curves for direct analysis of stability as a function of wave, height and period.

In this chapter an exponential model which depends upon Iriba rren's number is presented, for analysis of flow characteristics -run-up, run-down, reflexion and transmission- on rough, perme able slopes under regular wave action. Also interaction curves are defined, which quantify the phenomenon as a function of wa ve height and wave period.

Analy s i s of flow characteristics on sloping structures under irregular wave action has been carried out following a sem,i-em pirical or an empirical line by Saville (1962), Van Oorschot and d 'Angremond (1968), Battjes (1974a), Bruun and Johannesson (1977), Bruun and Günbak (1978), Kamphuis and Mohamed (1978).

By assuming the hypothesi s of equivalence, introduced by Savi lie (1962), and using the interaction curves, a new probabilistic approach to flow characteristics on sloping structures under a

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rLOW CHARACTERISTICS UNDER REGULAR WAVES

When a regular wave ttain reaches an undefined slope the following physical phenomena are produced: breaking, run-up and run-down, reflexion and transmission. Taking Z as a va riable to measure the phenomenon, it would be a function of the following parameters:

1. Parameters of the medium

~ Depth at the toe of the slope, d - Bottom slope, 3

- Specific weight of the water, v - Acceleration due to gravity, g - Kinematic viscosity, y

2 . Parameters of incident waves

Given that we are dealing with regular waves, these will be :

- Wave height , H - Wave period, T

- Wave approach angle, Q

3. Parameters of the structure

a) Geometry. It is defined by two parameters: - Slope angle, a

-A characteristic width, X

b) Characteristics of roughness permeability, which will depend on the following parameters:

- Type of armour units of the main layer

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9

-- S i z e of the armour units, which may he characterised by

the length of the side of the equivalent ^cube ^ . I = y W y W being the weight of the armour units and y their spe cific weight.

- Characteristics of the underlying layers.

Regarding rubblemound breakwaters designed according to tradi tional criteria, it is acceptable to say that the mean charac-T teristics of rougness and permeability depend only on the type of the armour units and their size.

From experiments described by the Technical Advisory Committee on Protection Against Inundation (1974), we may conclude that

-when incident wave height is considerably greater than the side of the equivalent cube the magnitude of the physical phenomena associated with the breaking of the wave on the slope are inde-pendent of the height of roughness and therefore of the size of the blocks.

On the other hand, when the wave breaks on smooth, impermeable slopes, experiments confirm that depth does not influence run-up, Saville (1956), Battjes and Roos (1975) and Hunt (1959),nor the reflexion coefficient, Moraes, (1970).

The aforementioned considerations suggest that flow characte ristics on a rough, undefined slope under the action of a regu lar wave train can be approximately governed by an expression -of the type:

f(Z, type of armour unit;a, X, Y ^ / p . 9, H, T, Q) 0 (1)

Taking the following dimensionless monomials:

2 generic dimensionless variable expressing flow •

a

0 •

H/L^ = 2T T H/gT^ H^/H T

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expression (1) remains , for each type of armour unit

z = f (a, e , H/L^, H^/\xT, \/H) (2)

According to Battjes (1974b), Reynolds' number /\xT holds, for smooth slopes, normally over a minimum tl^reshold above which it has no influence, and assuming perpendicular incidence (Q = 0) and neglecting the variable X/H (relative width of the breakwa-ter) which only has appreciable influence on the phenomenon of transmission, expression (2) can be further reduced to :

z = f(a, fl/L^) (3)

As is shown below, this fuction can be reduced to a simpler one of a single variable:

2 = f(Ir) (4)

Ir = tana/ /H/L^ being Iribarren's number. This fuction

holds for each type of armour unit and perpendicular incidence,

Breaking

In classical literature four types of breaking are defined, as points of reference, Iversen (1952), Patrick and Wiegel (1954), Galvin (1968): surging, collapsing, plunging and spilling.

Iribarren's number, which originated as an indication of whether or not wave breaking occurred on a flat slope , Iriba rren and Nogales (1949), produces not only this information but also how the wave breaks, Battjes (1974a, 1974b).

Table 1 shows the results of Günbak (1976) on a rough: slope, with coto. = 2,5 ,

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TABLE 1.1

Breaking on rip-rap slope (Günbak 1976)

TYPE OF BREAKING IRIBARREN NUMBER

Spilling — Plunging ir ^: 2 . 0

Blunging or collapsing 2.0 < Ir < 2.6 Collapsing or surging 2.6 < Ir < 3.1 Surging 3.1 < Ir

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In figure 1,1 the variables Z = Ru and Z - Rd are defined, these being the maximum and minimum levels referring to the S.W.L. reached by the water on the slope.

With r e f e r e n c e to equation (3) and taking Ru/H and Rd/H as

the dimensionle ss variable, we can, as a result, express:

Ru/H

=

f r a , H/L^) • (5aj

Rd/H = f(a, fi/L^) (5b)

Figures L2 to 1 . 7 show, against Iribarren's number, data co-rresponding to rough, permeable slopes taken from Ahrens and McCartney (1975) and Günbak (1979). All data correspond to -perpendicular wave incidence.

These figures also show the exponential model, Giménez-Curto (1979):

Ru/H = A {1 - exp(B.Ir)} (Sa) Rd/H = A {1 - exp(B.Ir)} , (6.b)

A and B being fit coefficients calculated by the least sgua red method,

A generalised correlation coefficient has also been calcula ted, defined by:

2 , 2,2

P = i - O^/Oy (7)

2 2

where o and a „ a r e variance with respect to the fitted

y

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R u / H 2. 0 0 T 1 . 7 5 1 . 5 0 1 . 2 5 1 . 0 0 0 . 7 5 0 . 5 0 0. 2 5 4-0 . 4-0 4-0 R U N - U P ON R I P - R A P S L O P E A H R E N S ' DATA {1975) ^ cot a = 2.50 cot

a =

3.50

« cot

a =

5.00

d / H > 3 . 8 5 4-0 . 4-0 4-0 1 . 4-0 4-0 2 . 4-0 4-0 3 . 4-0 4-0 L.'OO 5 . 0 0 5 . 0 0 7 . 0 0 8 . 0 0 I r i b a r r e n ' s N u m b e r , Ir

Fiq. 1. 2 . - R e l a t i v e r u n - u p v e r s u s I r i b o r r e n ' s Number on r J p- T a p slope. ( E x p e r i m e n t a l d a t a of A h r e n s , 1 9 7 5 )

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R u / H R d / H R U N - U P AND RUN-DOWN ON R I P - R A P S L O P E G U N B A K ' S DATA ( 1 9 7 5 ) cot

a =

2.50

F i g . 1 . 3 . - R e l a t i v e r u n - u p and r u n - d o w n v e r s u s Iribarren's Number on r i p - r a p slope ( E x p e r i m e n t a l d a t a of G ü n b a k , 1 975 )

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R u / H

R d / H

2 . 0 0 J 1 . 7 5 1 . 5 0 1 . 2 5 1 . 0 0 ^ 0 . 7 5 0 . 5 0 -0 . 2 5 0. 0 0 - 0 . 2 5 - 0 . 5 0 - 0 . 7 5 i - 1 . 0 0 - 1 . 2 5 - 1 . 5 0

+

)9r

^-R U N - U P AND ^-R U N - D O W N

ON QUARRYSTONE S L O P E

DAi .AND K A M E L ' S DATA (1969)

A

Relat

4"

Relat

9t

Relat

V® scale 0.50

ve scale 1.00

ve s c a l e 7 50

d / H >

2

.58

+

2 . 0 0 3 . 0 0 4 . 0 0 5 . 0 0 5 . 0 0 7 . 0 0 8 . 0 0 9 . 0 0 1 0 . 0 0

Iribarren's Number ^ Ir

F i g . X.L •- R e l a t i v e r u n - u p and run-Gov-,'n v e r s u s Iribarren's Number on quarrystone s l o p e . ( E x p e r i m e n t a l d a t a of D a i a n d Kam.el ^ t a k e n from Giinbak ^ 1 9 7 9 )

1

ON

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R u / H

2 . 0 0 r . 7 5 1 . 5 0 4 1 . 2 5 -f 1 . 0 0 + 0 . 7 5 0. 5 0 0 . 2 5 + 0 . 0 0 0 . 0 0

R U N - U P ON T E T R A P O D S S L O P E

J A C K S O N ' S DATA ( 1 9 5 8 )

c c t a = 1 . 2 5 , 1.50, 2 . 0 0 , 3.00

d / H > 3.00

i . O O 2 . 0 0 3 . 0 0 i - . O O 5 . 0 0 5 . 0 0 7 . 0 0 8 . 0 0

I r i b a r r e n ' s Number. Ir

Fig. 1. 5 . - Relative r u n - u p v e r s u s I r i b a r r e n ' s N u m b e r on t e t r a p o d s s l o p e . ( E x p e r i m e n t a l d a t e of J a c k s o n , t a k e n f r o m G ü n b a k . 1 9 7 9 ) 1 I

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R u / H R d / H R U N - U P AND R U N - D O W N ON DOLOS S L O P E W A L L I N G F O R D ' S DATA (1970) A cot a = 1.50 4 . c o t a = 2.00 « c o t a = 3.00 d / H > 1 . 5 0

•ig- 1 . 5 . - R e l a t i v e run - u p and r u n - d o w n v e r s u s I r i b a r r e n ' s Number on dolos s l o p e .

( E x p e r i m e n t a l d a t a of H y d r a u l i c s R e s e a r c h S t a tion ^ W a lligford , t a k e n from G ü n b a k J 9 7 9 )

I

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Ru/H

Rd/H

2 . 00 T 1 . 7 5 1 . 5 0 1 . 2 5 1 . 0 0 0 . 7 5 0 . 5 0 0 . 2 5 + 0. 0 0 - 0 . 2 5 0 . 5 0 0 . 7 5 -- 1 . 0 0 - 1 . 2 5 - 1 , 5 0

+

R U N - U P A N D R U P - D O W N

ON QUADRIPODS S L O P E

DAI AMD K A M E L ' S DATA (1959)

A

R e l a t i v e s c a l e 1.00

4- R e l a t i v e s c a l e 7.50

d / H >3.Si 7 . 0 0 8 . 0 0 9 . 0 0 1 0 . 00

I r i b a r r e n ' s N u m b e r , Ir

+

4 .

A

F i g . 1 . 7 . - R e l a t i v e r u n - u p and r u n - d o w n v e r s u s I r i b a r r e n ' s Number on q u a d r i p o d s s l o p e . ( E x p e r i m e n t a l d a t a of Dai a n d K a m e l , t a k e n f r o m G ü n b a k , 1 9 7 9 ) I

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3.00 r

Ru/H

Rd/H

1 . 0 0 - ^

Trend for i m p e r m e a b l e , smooth slope

Rip - rap { A h r e n s )

R i p - r a p ( G ü n b a k )

Q u a r r y stor^ ( D a i

B

Kamel)

" ^ - ^ Q u a d r i p o d s ( Dai

i

K a m e l )

Dolos { W a l l i n g f o r d )

Tetrapods ( J a c k s o n )

5.00 5.00 7.00 8.00

I r i b a r r e n ' s N u m b e r , Ir

Q u a d r i p o d s ( Dai ^ K a m e l )

Quarry stone ( Dai S K a m e l )

F i a . 1. e

t

D o l o s ( W a l l i n g f o r d )

^Rip - r a p { G ü n b a k )

C o m o a r i s o n of r e l a t i v e r u n - u p ar^d r u n - d o w n for s e v e r a l types of slope

J o

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f(x.)} 2 (8) 2 1 N N 2 O y) (9)

and where (x^,y^) and N are the points to be fitted and the number of them, and f(x) the curve being fitted.

Tables 1.2 and 1.3 give the results obtained in the fit.

Figure 1.8 shows the best fit curves together with a curve

-meable slopes, based on data of Technical Advisory Committee on•Protect ion against Inundation (1974), Battjes and Roos (1975) and Günbak (1976), It is concluded from this figure that it is not correct to apply a reduction factor depending only on the ~ type of armour unit to the run-up on smooth, impermeable slopes in order to obtain the run-up on rough:, slopes, as is

recommended by the Technical Advisory Committee on Protection against -Inundation (1974) , PIANC (1976 ), Stoa (1979).

B.^fl,^^i_on

Defining the reflexion coefficient (^.j.) the reflected

-wave height (H^)and the incident -wave height (H.) ratio, equation (3) is applied for reflexion as:

Figures 1.9, l.lOandlll represent reflexion data on rough , per meable slopes taken from Günbak (1979), Hydraulics Research Sta tion (19.70) and Sollitt and Cross (1972).

which represents the trend of these data for smooth, imper

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1 . 00 - r 0 . 8 0 - f 0 . 5 0 -0 . 4 -0 4 O . 2 0 0. 0 0 0. 0 0

R E F L E X I O N ON R I P - R A P SLOPE

GÜNBAK'S DATA ( 1 3 7 6 )

A c o t

a =

1

.50

+ c o t a = 2 . 5 0

1 . 0 0 3 . 0 0 U . 00 5 . 0 0

I r i b a r r e n ' s N u m b e r . Ir

0 0 F i g . 1. 9 . R e f l e x i o n c o e f f i c e n t v e r s u s I r i b a r r e n ' s Number on r i p r a p -( E x p e r i m e n t a l data of G ü n b a k , 19 7 6 ) ! 1

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1 . 00 r 0 . 8 0 + 0. 5 0 O . 4 0 0 . 2 0 4-0 . 4-0 4-0

R E F L E X I O N ON QUARRYSTONE S L O P E

S O L L I T T g C R O S S ' DATA ( 1 9 7 2 )

cot

a = 1.50

d / H >

3.9 5

0 . 0 0 1 . 0 0 2 . 0 0 3 . 0 0 4 . 0 0 5 . 0 0 6 . 0 0 7 . 0 0 8 . 0 0 9 . 0 0 1 0 . 0 0

I r i b a r r e n ' s Nunnber, Ir

F i g . 1 . 1 0 . - R e f l e x i o n c o e f f i c i e n t v e r s u s I r i b a r r e n ' s Number on q u a r r y s t o n e . ( E x p e r i m e n t a l d a t a of S o l l i t t and C r o s s , 1 9 7 2 ) 1

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1 . 0 0 Cr 0. 8 0 0 . 6 0 0 . 4 0 O . 2 0 O . 00 O R E F L E X I O N ON W A L L I N G F O R D ' S A c o t

a

=1

.50

^ c o t a = 2. 0 0

* c o t a = 3

. 0 0

d / H >

1.78

DOLOS S L O P E DATA

(1970)

I r i b a r r e n ' s N u m b e r , Ir F i g . 1 . 1 1 . - R e f l e x i o n c o e f f i c i e n t ( E x p e r i n-iental d a t a v e r s u s I r i b a r r e n ' s Number on of Hydraulics R e s e a r c h S t a t i o n ^ d o l o s . 1 9 7 0 )

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TABLE 1 . 2 ' ,

Fit and generalised correlation coefficients of the model defined in equation (6a) for run-up of water on rough, per-meable slopes.

TYPE OF ARMOUR UNIT A

Rip-rap

(Ahrens & McCartney) 1-7887 -0.4552 0.96

Rip-rap

(Günbak) 1.4510 -0.5230 0.81 Rubble

(Dai & Kamel) ^-^^^^ -0.5964 0.61

Tetrapods

(Jakson) 0.9341 -0.7502 0.74

Dolos

(Wallingford) ^''^^^ -0.5675 0.74 Quadripods

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-2 6

TABLE 1.3

Fit and generalised correlation coefficients of the model defined in equation {6b) for run-down of water on rough, per meable slopes.

TYPE OF ARMOUR UNIT A

Rubble (Dai a Kamel) -0.8523 -0.4256 0.60 Rip-rap (Günbak) -6.2204 -0.0398 0.93 Dolos (Wallingford) -1.0607 -0.2659 0.83 Quadripods

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1 . 0 0

y « ! = 1 i i 1 1 i 1 I

0 . 0 0 1 . 0 0 2 . 0 0 3 . 0 0 4 . 0 0 5 . 0 0 6 . 0 0 7 . 0 0 8 . 0 0

Iribarren's N u m b e r , Ir

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-.2 8

These figures also show the exponential model, Giménez-Curto (1979):

= A {1 - .exp(B.Ir)} (H)

Table i^4gives the values of coefficients obtained in the sa-me way as for run-up and run-down. The resulting curves are re presented in Figure 112 together with a curve which shows the -trend of data for smooth, impermeable slopes, Moraes (1970) and Battjes (1974a, 1974b).

Having defined the transmission coefficient (c^) as the trans mittéd wave height (H^) and the incident wave height (H) ratio, equation (3) is applied for transmission, for a specific break water width, as:

=-- f (a, H/L^) (12)

Figure 1.13 represents the results of transmission experiments carried out hy Sollitt and Cross (1972) as well as the

exponen-tial model, Giménez~Curto(1979):

= A {1 - exp(B.Ir)} (13)

with the resulting fit coefficients: A = 1.64, B = -0.01278 and p = 0.87.

INTERACTION CURVES

Interaction curves of each phenomenon analysed are defi-ned as the sets of points on the plane (H,T) which produce the

same quantitative manifestation of the phenomenon, Giménez-Curto (1979).

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1 . 0 0 0 . 8 0 + 0. 5 0 0 . 4 0 0 . 2 0 -\

TRANSMISSION THROUGH

A Q U A R R Y S T O N E B R E A K W A T E R

SOLLITT

8

CROSS'

DATA

(1972)

cot

a =

1.

50

d / H =

3.95

1 . 0 0 2 . 0 0 3 . 0 0 4 . 0 0 5 . 0 0 6 . 0 0 . 7 . 0 0 8 . 0 0 9 . 0 0 1 0 . 0 0

Iribarren's Number, Ir

F i g . 1 . 1 3 . - T r a n s m i s s i o n c o e f f i c e n t for a q u a r r y s t o n e b r e a k w a t e r ( S o l l i tt a n d C r o s s , 1 9 7 2 ) ! !

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" 3 0

TABLE 1.4

Fit and generalised correlation coefficients of the model defined in equation (11) for the reflection coefficient on rough, permeable slopes.

TYPE OF ARMOUR UNIT A B

Dolos

(Wallingford) Rubble

(Sollit &• Cross) Rip-rap (Günbak) 3.9990 0.5030 1.3508 -0.0197 -0.1248 -0. 0710 0. 83 0.70 0.9 7

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For perpendicular incidence and a specific type of armour unit the exponent ia1 model can be used:

Z = AH {1 - exp(B.Ir)} (14)

and expressing Iribarren's number as:

Ir = /g/2-ïï tana T/y/H (15)

a function of type:

f (Z,H,T,a) = 0 (16)

can be obtained, on elimination of Ir. Thus allowing repre-sentation of the curves Z = c t e on the plane (H,T) for each slope.

Figures 1.14 and 1.15 show some examples of interaction -curves of breaking and run-down phenomena. These -curves are limited by the curve which defines the wave stability limit. Maximum value of the wave slope has been taken as (H/L ) =

0.142 , which corresponds to Ir^ = 2.654 tana.

FLOW CHARACTERISTICS UNDER IRREGULAR WAVES

In the case of a sea state the variables type of breaking, Ru , Rd, H , H, may be considered random variables which a c r

' ' r' t ^

quire a value for every wave of the sea state.

The distribution function of these random variables may be obtained by assigning to each individual, irregular wave the same phenomenon value which would be produced by a periodic -wave train of the same height and the same period.

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2 0

H { m )

O 5 10 15 20 25

T ( s g )

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-34-It is important to note the statistical nature of this hypo thesis, which does not necessarily imply that each individual wave produces the same phenomenon manifestation as the equiva-lent regular wave train, but is less restrictive; it refers to averages of many values rather than to individual values.

This hypothesis, known as the hypothesis of equivalence, was introduced by Saville (1962) and was empirically proven by Van Oorschot and d 'Angremond (1968) and Battjes (1974a) for run-up on smooth slopes, and by Bruun and Johannesson (1977) and

Bruun and Günbak (1978) for run-up on rough, permeable slopes. Taking into account that the distribution fuction of Z is

-defined by:

(x) = Prob[z ^ x] (IT)

and that Z = x is and interaction curve, the result is:

(x) = SS^ p^(H,T) dH dT (18)

where the integration domain, D, is the shaded area in Figure 1.16 and p* (H ,T) is the joint probability density function of

wave heights and periods in the place occupied by thé slope.

Thus, knowing the joint probability density function of wa-ve heights and periods and interaction curwa-ves, by means of nu-meric integration it is possible to obtain the distribution of type of breaking, Ru, Rd, H _^ of H^ in a sea state.

Figures 1.17 and 1.18 show examples of distribution functions of type of breaking and H^.

It has been assumed that:

P(H,T)

P* (H ,T) = (19) j " " dT f"^p(H ,T )dH

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~35~

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36-1.0

05

<

co

O

CU CL. 0.0

Hs = A.Om.

Tz = 12.0 sg.

£ r.

0.6

H s =A.Om.

Tz =

8.0

s g .

e = 0.6

Distribution (H, T ) : C a v a n i d , A r h a n y E z r a t y

•1

I

Plunging

Plunging or C o l l a p s i n g Surging

Collapsing or Surging

F i g . 1 . 1 7 - - E x a m p l e of d i s t r i b u t i o n of type b r e a k i n g - R i p - r a p slope , cot a = 3 . 0 0 , h o r i z o n t a l bed w i t h d = 10.0 m .

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-37-F i g . 1 . 1 8 . - E x a m p l e of d i s t r i b u t i o n of r e f l e c t e d w a v e height.

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3 8

-where p(H,T) is a theoretical distribution, Longuet-Higgins (1975), (L.H.), Cavanie, Arhan and Ezraty (1976), (C.A.E.), and is breaking-wave height defined by the breaking limit

b

curve. This curve has been defined in the examples in accor dance with hiiffhell (1893), Miche (1944) , Goda (1970) and Reid and BretschneJ-der (1953) as- follows:

.2 0.142 gT' 2T T Deep water d'/L ^ 0 . 5 (20) 11^ = 0.142 L tanh (2fid/L) b Transitional water (21) 0.-1 4-d/L < 0,5 'b = bd 1+ad/gT' Shallow water d./L < 0.1 (22)

where L is the wave length and a and b fined by (Goda, 1970) are coefficients de = 43.75 {1 - exp(-19m)) (23) 1 . 56 b = l-f-exp(-19. 5m) (24)

m = tanQ being bottom slope.

Distribution of the maximum value of variables Ru, Rd, H^, H _^ in a sea state may be obtained by accepting statistical indepeu dence among the successive values acquired by each of these

va-riables within the sea state. Note that this hypothesis does not necessarily imply statistical independence among successive wave heights and periods.

Taking F (x) as the distribution function of maximum, value M Z

for Z in the sea state, it follows that:

N

(25)

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TABLE 1.5

Data of experiments from Kamphuis and Mohamed, 1978, on smooth, impermeable slopes and d - 0.90 m.

CASE SPECTRUM ^^(m) T^fsg) . T^(sg) ctga

A Bretschneider 0.0528 1.59 1,30 1.50 B Bretschneider 0,0755 1.43 1.20 2.00

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-40-Equation (25) shows the influence of duration on maximum v a

lues, Losada and Giménez-Curto (1979b),

The probabilistic method of analysis described here has been compared with experiments carried out by Kamphuis and Mohamed -(1978) regarding run-up on smooth, impermeable slopes. Two cases have been chosen, details of which are given in table 1.5, in

-which H is the significant wave height, T the mean zero-upcros_ sing period and T^ the spectral peak period.

The theoretical method has been applied with the following -criteria :

a) run-up on smooth, impermeable slopes is represented by the following model:

Ru/H = Ir for Ir4 2,5 (26a) Ru/H --^ 2,5 - (Ir-2.5)/3 for 2, 5 < Ir ^ 4. 0 (26b) Ru/H = 2.0 for 4,0 Ir (26c)

which is based on data from the Technical Advisory Committee of Protection Against Inundation (1974), Battjes and Roos

(1975) and Günbak (1976),

b) On the basis of this model, interaction curves have been ob-tained which, together with the breaking limit, are shown in figures 1.19 and 1.20.

c) Using equations (18) and (19) with joint distributions of wa ve heights.and periods of Bretschneider (1959), Longuet~Hig-gins (1975) and Cavanie, Arhan and Ezraty (1976), run-up dis tribution fuctions have been obtained.

Parameters of joint distributions of wave heights and period obtained from the spectral moments, are given in Table 1,6, Figures 1.21 and 1,22 represent the values obtained in the ex periments and the results obtained by the method described above, together with Rayleigh distribution, for cases A and B respectively.

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•41 0,100 H( m ) 0075 0,0 50 0.025 OOOO

Ru =

0.15 rn.

Ru =

0.10

m .

r

R u =

0,0

5 rn

T ( s g )

F i g . 1.19 I n t e r a c t i o n c u r v e s of r u n - u p on smooth, impermeable slope b a s e d on c q s . { 2 6 ) . c o t a = 1.50

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F i g . - 1. 2 0 . - I n t e r a c t i o n c u r v e s of r u n - u p on s m o o t h , impermeable slope b a s e d on e q s . ( 2 6 ) . c o t a = 2.00

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4 3

-TABLE 1.6

Values of parameters used in distributions for experimental comparison. PARAMETERS CASE DISTRIBUTION A -4 Brestschneider 1.74.10 1,30 - _ „ -4 Longuet-Higgins 1,74,10 ~ 1,23 - 0,41 Cavanié, Arhan - 4 ' 1.74,10 1,30 - 0.80 and Ezraty -4 Bretschneider 3.55.10 1,20 --4 Longuet-Higgins 3,55,10 - 1,10 - 0,41 B and Ezraty Cavanié, Arhan ^ -, -4 3.55.10 1.20 ~ 0.80

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20.0 15.0

Joint distribution (H , T )

1.- Bretschneider

1-

Longuet - Higgins

3.-

C a v a n i é , A r h a n a n d E z r a t y

E

o

D

a:

10.0 0.99 0.999

P r o b l R u n - up s Ru

F i g . 1 . 2 1 - E x p e r i m e n t a l c o m p a r i s o n of the p r o b a b i l i s t i c m e t h o d des c r i b e d herein ( C a s o A )

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-.45-30.0 25.0 2 0 0 _ 15.0

i

0.0 - - I 1

Joint distribution, ( H , T )

2 -

Longuet - Higgins

3

- Cavanié , A r h a n and E z r a t y

A>/

yf

//

// / /

^/ / /

yy y

b///

///

A E x p e r imental results of

Kamphuis a n d Mohamed

// /

77~7^

^

£

0 0.1 0 5 0 9 0.99 G.999

P r o b [ R u n - u p s R u

F i g . 1 . 2 2 . - E x p e r i m e n t a l comparison of the p r o b a b i l i s t i c m e t h o d c r i bed h e r e i n ( C a s p B ) d e s

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-CONCLUSIONS

1) For rough, permeable slopes, flow characteristics under the action of a regular wave train may be represented by a fun_ ction of the type:

z = A {1 - exp(B.Ir)} (27)

2) Run-up on rough, permeable slopes cannot be calculated on the basis of run-up on smooth, impermeable slopes by appli_ cation of a reduction coefficient that only depends on the type of armour unit.

3) Accepting the hypothesis of equivalence, distribution of -flow characteristics in sea state can be obtained on the ba sis of interaction curves and joint probability density funct ion of wave' heights and periods.

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CHAPTER 2 MOUND STABILITY

INTRODUCTION

Ahrens and McCartney (1975) introduced the use of Iribarren's number in the analysis of stability of rip-rap slopes.

Bruun and Johannesson (1976) emphasise the influence of the

-wave period and conclude that Iribarren's number is a determining factor for stability of the main layer of the mound and for flow characteristics.

Bruun and Johannesson (1977) and Bruun and Günbak (1977, 1978) insist on using Iribarren's number in the study of stability and propose using the hypothesis of equivalence for analysis under -irregular waves.

Losada and Giménez-Curto (1979a) present an exponential model as a function of Iribarren's number to represent rubblemound break water stability under regular waves, introducing, on the other

hand, interaction curves for analysis of stability as a funcion of wave height and period.

Finally, Losada and Giménez-Curto (1979b) propose a method for evaluating failure probability in marine constructions under a sea state, this being based on the interaction curve and on the hypoth sis of. equivalence , and also analy se'.the influence, of ' sea state d u

ration.

This chapter presents, all of these ideas, indicating in the

first place a general statement of the problem under regular waves which leads to the concept of stability function. Subsequently

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this function is calculated by means of the m,odel introduced by Losada and Giménez-Curto' (1979a) and finally the problem of sta bility under irregular waves is dealt with by way of a probabi-listic approxim.ation based on interaction curves and the hypothe_ sis of equivalence.

STABILITY UNDER REGULAR WAVES

Tnis considers the. problem of stability of main layer armour units of an undefined mound under regular wave action.

This chapter deals almost exclusively with the type of dama-ge (2) of those considered by Bruun (1979), that is, lift-outs of armour units caused by wave action. The following variables play a role, initially, in this phenomenon:

1. Parameters of the Medium: d, ^,y^^,g y (see chapter 1) 2. Parameters of incident waves: H, T, ö (see chapter 1) 3. Parameters of the Structure:

- slope angle a

- weight of the armour units W

- specific weight of the armour units y^ - thickness of the armour layer e

- interaction forces among armour units (friction and inter locking)

- characteristics of roughness and permeability of the ar-mour layer

- character ist ic s of the underly ing layers

Regarding rubble mound breakv/aters designed in accordance with traditional criteria, it can be accepted that .characteristics of underlying layers depend on those of the main layer (type of

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~49~

characteristics of friction and interlocking, as well as roughness and permeability, of the armour layer depend on:

- type of armour units - size

- way of placing them onto the slope

The size of armour units may be characterised by means of the -length of the side of the equivalent cube:

I = (W/y^)^^^ (1)

The thickness of the armour layer tends to be a s-pecific number of times the side of the equivalente cube:

e = nl (2)

Assuming that depth is moderately great, such that the influence of d and 3 can be ignored, and that the way of placing the ar mour units onto the slope is at random, it turns out that for__each

£ y £ £ _ . ° £ _ £ £ . 5 I 2 H . £ - - H 2 . i * stability conditions are governed by a function

of the type:

f(a, W, y^, H, T, e , y^, p , g) = 0 (3)

The equality expressed by this equation means the £^£:Li£.M.„ii" mit, that is, that for the wave conditions defined by H, T and Q, and given a, y^, y^f\i ^^"^ 9' weight W, which satisfies equation ~ (3) is the minimum that the armour units must possess in order to be stable. Therefore, function "f" , carries with it, tacitly, a stability criterion (damage or failure criterion).

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- 5 0

Taking the following six dimensionless monomials:

a

e

H^/IXT

H/L^ =

2iT H/gT^ equations (3) remains: f(a, yj/^y, S^, 6 , H^/^T, H/L^J = 0 (4)

Accepting, as for flow characteristics, that Reynolds • number^ H /\xT , is kept above a minimum threshold so that variations in its value do not significantly affect the resulting phenomenon, and assuming normal incidence of waves (Q = 0), equation (4)

be-comes:

f(a, W/y^, ü^,

H/L^) = 0 (5)

which can also be written as:

^ = y,yf( ar-

S^, H/L^) (6)

On the other hand, all theoretical formulae existing at present to calculate the weight of main layer armour units of a rubblemound breakwater, can be written in the following manner (PIANC ( 1976)):

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-51

or else as

(8)

where ^ is a dimensionless function depending on a in all cases, and on other parameter such as type of armour unit-., H, T, d, L,

friction coefficients and other empirical coefficients, according to the different formulations.

It can he seen tKat equation (6) has the same formal structure as equation (8), Comparing both expressions we can write:

f(a, S^,

H/L^) =

R(S^) ^, (a,

H/L^}

(9)

where function R:

^ = S^/(S^-1)'

encompasses the effect of (specific relative weight of armour units) in the function f, in accordance with the generality of exis ting theories, PIANC (1976).

Lastly, it is concluded that for each type of armour unit, having established a stability criterion, and in the case of normal

inci-dence of regular waves, function depends solely on a and H/L^ ('accepting the aforementioned hypotheses) . This function will be -known here as the stability function.

The weight that the armour units must possess, in order to -strictly fulfil the criterion which the stability function implici tly carries with it, is expressed, bearing in mind equations (6),

(9)

and

(10),

by

^ = yy^i> ill)

In the following paragraphs the stability function is studied, using experimental results of Iribarren, Ahrens and McCartney and HudsonC

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•-52-St a_bi y _ _ £ £ i teri on

The first problem faced in analysis of stability conditions is the definition of a stability of damage criterion.

A breakwater under specific wave conditions, can be stable or }LU.S.'Ë.S.k^£. ' said to be unstable v^hen incident waves produce a loss of armour units on its main lay er (damage) , The breakwater is stable if the waves are incapable of extracting any armour unit from its main layer.

Traditionally damage has been defined as the percentage of ar mour units displaced with respect to the total number of armour

units used in the construction of the main layer (classical defi nit ion),

This definition is inconsistent, given that damage depends therefore on the size of the main layer. If the dimensions of the latter were to be standardised in relation to the size of armour unit the classical definition of damage would be consistent.

One way to avoid the existing incosistency in the previous cri terion would be to define damage as the percentage of displaced armour units with respect to the number of them contained initia lly in a band of specific width around the S.W.L'. (Van de Kreeke (1969), Ouellet (1972), Günbak (1978)).

The main disadvantage of these definitions is that they do not provide clear information about the situation of the breakwater with respect to its total destruction.

Iribarren (1965) proposes a definition of breaking which gives a clear picture of the breakwater's future. We can express his -criterion in the following way:

A rubblemound breakwater has reached its breaking level when -the depth of damage on-its main layer is equal to -the lenght of the side of the equivalent cube I.

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-53

This is to say that the first layer of armour units of the main layer has been lifted (and displaced) in a area sufficien

tly so as to expose at least on armour unit of the second

la-yer of the main lala-yer to direct wave action. Once this situation has been reached the breakwater would be severely damaged and

it can be said that its total destruction is :::merely a question of time. (Note that interlocking of second layer armour units is much lower than that of outer armour u,nitsj.

In figure 2.1 two examples are shown, from experiments car-ried out by Iribarren, which correspond to this breaking situa tion (unpublished data).

To reach this state the waves must exceed a certain threshold In order to di splace an armour unit integrated in the main layer the wave must overcome friction and interlocking existing among armour units.

Generally speaking £ £ £ c t i o £ refers to resistance to extrac-tion of a microscopic type, due to roughness of armour units. Interlocking refers to resistence of a macroscopic type, depen-ding upon the shape of the armour units.

Once this threshold has been exceeded , the only resistance -whicn the armour unit can offer against its extraction by waves is its own weight..

Taking this into account it is understood that a main layer designed with a type of armour units which develop a great deal -óf interlocking among each other, will possess a much higher threshold of the aforementioned nature, and as a consequence wil 1 require less weight in order to resist wave action. However if this level is exceeded the armour unit is deprived of the contri_ bution of adjacent armour units and as its weight is low it is easly displaced by wave action. -Also if .thé a'rmour' unit breaks in to various -pieces, each one will- weigh even less and they will, as a consequence, be m.ore vulnerable, Magoon and Baird (1977).

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0.90 m. .60 .70 .80 .90 29.00 .10 .20 .30 .40 .50 .60 .70 .80 m. in wave flume 0.90 0.80 Q70 0.50 050 040 0.30 02 0 0.10 I n i t i a l profile S. V^/. L. Final profile b r e a k a g e ) ^ Quarrystones I r i b a r r e n ' s test cot a = 2.00 W = 01 Kg. T 1.50 sg. H ^ 0.19 m. .60 .70 .80 .90 29.00 .10 .20 .30 .40 .50 .60 .70 .80 m. in wave flurne

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When the waves overcome the friction and interlocking that exists among the armour units of the main layer, the only

re-sistence they can offer is their own weight. Under such condi tions they are easly displaced, even by lower waves, so that damage of type 4 can occur, caused by small displacements, Bruun (1979). In these movements some armour units will hit -against others and this can give rise to damages of t y p e , I ,

-Bruun (1979). Consequently it seems reasonable to use this threshold in the design, as a level of the damage starting point.

Therefore initiation of damage is defined as the minimum -wave height, for constant period, which is capable of overco-ming friction and interlocking among the armour units.

When interpreting experimental results the problem arises in distiguishing, once the fist armour units fall, which of them were part of the main layer, and therefore have been

ex-tracted, and which were not, with a view to finding out whether friction and inter locking have been overcome. For this reason it is necessary to establish a clear criterion.

Bearing in mind these aforementioned points, the initiation of damage situation is defined, in this study, as minimum wave height, for constant period, capable of producing extraction of at least ten per cent of the total number of armour units which are displaced until breaking of the breakwater by Iribarren's ^ criterion is reached.

Hegarding experiments by Ahrens and McCartney and Hudson, re suits of which are also used in this study, there has not been sufficient information available in order to apply the afore-mentioned criterion, and therefore criteria used by the authors

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-56-themselves will, be employed, In t_he case of Ahrens and McCartney that of zero_damage, which corresponds to a situation where there nas been hardly any stabilisation of armour units that were in ve ry unstable positions in construction, without appreciable armour unit displacement. In the case of Hudson, that of no__damage,

which corresponds to a maximum displacement of one per cent of the armour units used in construction of the main layer (classical de • finitioji. •

THE STABILITY FUNCTION

^ ^ £ Ê ê£ i{ n£ £ £ S . - ^ „£=* ^

The experimental results used in this study are those obtained by Iribarren (1965), Ahrens and McCartney (1975 ) and Hud son ((19 5 8), taken from Bruun and Johannesson (1977)).

All of these tests are with regular waves and perpendicular in cidence.

Regarding Iribarren's results, 93 experiments have been selec-ted on the basis of a homogenization, (31 with quarry stones, 40 with parallelopipedic blocks and 22 with tetrapods). These tests were carried out with a wave tlume of 31.5 m. long, 1.0 m wide and 1.5 m deep. Characteristics of the model, of waves and expe rimental technique are given in tables 2.1, 2.2 and 2.3,

Ahrens and McCartney (1975) conducted experiments on stability of rip-rap slopes. These tests were done with a wave flume of

193.55 m. long, 4.57 m wide and 6.10 m deep. The average weight, " ^^Qf varies from 12 to 5b Kgs. Armour units used were of diorite < with specific weight of 2.71 y m ' ^ . 48 experiments have been - < used (16 with cota = 2.50, 19 with cota = 3,50 and 13 with

cota = 5,00). Wave heights vary from 0,55 ' ' t o 1,83 m, and periods from 2.8 to 11.3 sg. Water depth is 4,57 m.

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-57-TABLE 2.1

C h a r a c t e r i s t i c s o f the m o d e l in Iribarren's tests

A r m o u r u n i t s S l o p e s P (g) 7 , ( g / c m ' ) T h i c k n e s s of a r m o u r l a y e r Q u a r r y stones 1.50 2.00 3 . 0 0 4 . 0 0 1 2 , 5 1 0 0 2.53 > 3 / ( 7 ) ( 1 0 ) ( 7 ) ( 7 ) ( 7 ) ( 2 4 ) 2.53 > 3 / P a r a l l e l o p i p e d i c . 1.50 2 . 0 0 3 . 0 0 1 2 . 5 1 7 . 5 7 3 1 0 0 1.54 2 . 1 0 3 . 0 0

21

b l o c k s ( 1 7 ) ( 1 4 ) ( 9 ) ( 1 ) ( 1 1 ) ( 8 ) ( 2 0 ) T e t r a p o d s 1.33 ( 8 ) 1.50 ( 7 ) 2 , 0 0 ( 7 ) 1 2 . 5 ( 3 ) 1 0 0 ( 1 9 ) 2 . 1 0

21

U n d e f i n e d slope; length o f the equivalent c u b e : / = (Ply^)^'^; v/eight o f the units o f s e c o n d a r y l a y e r 'v P / 2 0 ; variable core. P is the weight of a r m o u r units, is the s p e c i f i c weight o f a r m o u r units. T h e weight of the a r m o u r units is u n i f o r m ; it is i n -c l u d e d in the interval P ± O.IP at a p r o b a b i l i t y level of 95%. T h e n u m b e r s in brackets refer to the n u m b e r o f e x p e r i m e n t s c o n -sidered in this w o r k .

TABLE 2,2

C h a r a c t e r i s t i c s o f the waves in I r i b a r r e n ' s tests

R e g u l a r v/aves N o r m a l i n c i d e n c e R e l a t i v e depth (d/L) 0 . 0 5 - 0 . 3 5 D e p t h (d) 0 . 2 1 —0.15 m. Wave heights (H) 0.03 - 0 . 2 5 m. Wave periods (T) 0.91 - 5 . 0 2 sc. Wave steepness ( i Z / L , ) 0 . 0 0 1 5 - 0 . 1 0 2 7 R a t i o ( d / H ) > 2 . 3

H, T, L, d are the w a v e height, wave p e r i o d , wave length and d e p t h at toe of the break-w a t e r . L j is the deep-break-water break-wave length.

TABLE 2.3

E x p e r i m e n t a l t e c h n i q u e s i n Iriban-en's tests

O b j e c t i v e M e t h o d a d o p t e d

C a l i b r a t i o n of B e f o r e f i t t i n g the m o d e l i n the f l u m e a wave a b s o r b i n g r a m p w a s wave heights p l a c e d at the e n d ; v/ave heights were then m e a s u r e d at the m o d e l site.

C o n t r o l o f re- T e s t s were c o n d u c t e d w i t h sets of waves, s t o p p i n g the wave generator f l e e t e d waves before the d o u b l y r e f l e c t e d v/ave r e t u r n e d to the b r e a k w a t e r . A

guillotine was d r o p p e d near the m o d e l b r e a k w a t e r , so that the higher waves c a u s e d by s t o p p i n g the generator d i d n o t a f f e c t the m o d e l .

B r e a k a g e c r i - T h e b r e a k w a t e r is c o n s i d e r e d to be c r i t i c a l l y damaged w h e n the depth t e r i o n o f the damage i n the cover l a y e r reaches the length o f the e q u i v a l e n t

c u b e (Phy.)^^^. A t this stage the f i r s t l a y e r of the c o v e r l a y e r is c o m -pletely b r o k e n a n d the stability of the b r e a k w a t e r is e n d a n g e r e d .

S t a n d a r d i s a t i o n E a c h e x p e r i m e n t c o m m e n c e s w i t h a v,'ave height s e n s i b l y lov/er t h a n o f all tests t h a t of the i n i t i a t i o n of the fall o f a r m o u r units. T h e wave height is

in-creased by s m a l l steps u n t i l it reaches the breakage point. T h e m o d e l is n o t r e b u i l t for each new wave height.

F o r each v/ave height, ten sets of waves are a p p l i e d to the m o d e l . I f a stable p r o f i l e has n o t been established, the series o f ten sets is repeated. W h e n close to breakage, 50 sets o f waves are a p p l i e d a n d , w i t h p r o f i l e s t a k e n d i r e c t l y , tests are m a d e to see i f breakage p o i n t has been r e a c h e d .

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5 8

-Hudson's results have been taken from Bruun and Johanesson (1977), considering 21 experiments all v/ith quarry stones ( 9 with cota = 1.50, 5 with cota = 2.0 and 7 with cotu, = 4.0). Equipment used, characteristics of the model and the waves are very similar to those of Iribarren's experiments except that

the latter experimented with a wider range of wave characterise . tics than Hudson. The greatest difference lie in experimental technique. In Hudson's experiments waves occurring due to stop page of the generator ^ w.'hich are higher-, affected the break-water, while in Iribarren's, thank to the guillotine, this did not happen. Furthermore the model was reconstructed after the attack of every size of wave. These two differences in expe-rimental technique make Hudson's experiments very much on the safe side in comparison to Iribarren ' s, as on the one hand tne breakwater Is struck by some waves which are higher than those considered in the analysis and on the other the stabilising effect that low waves have on the mound is not taken into ac-count.

It has already been seen that once a stability criterion has been established, for each type of armour unit and in., the case of normal incidence of regular waves, the stability function derf pends solely on the slope angle (a) and on the wave steepness ~

(H/L^).

i) = i)(a, H/L^) (x2)

The previous chapter shows that flow characteristics on rough, permeable slopes are well represented by Iribarren's number as the

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sole parameter:

' Ir = tanCL//H/L^ (13)

consequently it is reasonable to believe that this parameter must play an important role in rubblemound breakwater stability.

Losada and Giménez-Curto (1979a) propose an exponential model as a function of Iribarren's number for analysis of stability of a rubblemound breakwater unüer regular waves.

Using this fit model we can write:

\\> = A(lr-Ir^) exp{ B(Ir-Ir^)} Ir ^. Ir^ (14)

where

Ir - tanoJ^/H/L^ (23) Ir^ = 2.654 tana (15)

A and B are fit coefficients which depend on the type of armour unit and slope angle.

Figures 2.2, 2.3 and 2.4 show the stability function drawn -against Iribarren's number tor various slope angles and types of armour unit according to Iribarren's experiments. The cofres-pondmg values of fit coefficients A and B and of Ir ^ are given in table 2.4 (Losada :and Giménez-Curto ( 1979a)).

un the other hand figures 2.5 and 2.6 represent the stability ruction against iribarren's number for experiments by Ahrens and McCartney and Hudson.

It is interesting to point out the great quantitative differen ces existing between Hudson's results and the equivalent ones of

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S T A B I L I T Y F U N C T I O N , W o O O O O O O O O O O O O O O O O O O O O O O !0 OJ Ol cn OD CD O —* O X )K -I- O O O O O O O O O •-^ ^ . - c

R P P Q

I I I I II II p o K ) . ' -ö O O c n O O O O

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S T A B I L I T Y FUNCTION^ W o o o o o o o o o o o o o C D o o o o o o O O — ' K> w cn -~J CO lO

0

n o O o o O

R P P

II I I II CO K >

.-^

O O c n O O O

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O

O

z

>-cn

< 1 — tn 0 . 1 1 0. 1 O 0 . 0 9 4-0 . 4-0 1 O . 00 O . 00 00 2 . 0 0 3 . 0 0 4 . 0 0 5 . 0 0 6 . 0 0 7. 00 8. 00 9 . 0 0 1 0 . 0 0 Iribarren's Number , Ir A c o t a = 1.33 -t- c o t a = 1.50 ^ c o t a =2.00

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-6

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