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7/27/2019 Thesis Tidal Power
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a
Ab Ac B
a/bh
Cd Cd Cd,eff CP CT f
F r
U/
gh
g
h
hd ho kt Kc U/LL, L1, L2 n
p
P
Pa Pd Pf Pt P+Pd)t
u= (u, v)T
U
2, 4, 4
T
x,b, y,b
( )
ai A
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b
PW T
X
z
( )b,t b t ( )1,2,3,4,5
u
u, v, w x,y,z
Tf
xx, xy, yy
t
b
c=
gh
F(U,Q)G(U,Q)
F, G, Rx, Ry, i,k,p
hm lv, lh M
n
Q=( u
x, u
y, v
x, v
y)T
Rx(U) Ry(U)
S(U)
U= (u,uh,vh)T Uh, Qh
e ,e B,E G SA M
{k} {lk,}
{k}
( )
( )b ( )
( )L,R
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a2
A
c L
0 A
1
c dxFGC Ft Pmax Q
Qmax, QX,max X= 1, 2, 30, 1 0, 1 0, 1
V, I,L,C, R ()e ( )1,2,3,4 ( )0
b
hc he
j
j=
1l
L
m1, m2 S
xb
0, 1 0, 1 0, 10,
1
0, 1
0,
1
T =0+1)
s b
V, I,L,C, R ( )0
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K
Qc Qf Q
f,0
ul
U0 x0
x,y
(a, b)
E(Y) HI HV
J, Js L1, L2 q, m
S
T
x= (x, y)
Y= (h,uh,vh)T = (1, 2) q qs wq, wqs
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7/27/2019 Thesis Tidal Power
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2
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Impounded Area, A
Barrage
Adjoining Ocean or Sea
t1 t2 t3 t4
Ab
21gAba
2
= a
(t)
a
g
t
Ab
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7/27/2019 Thesis Tidal Power
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7/27/2019 Thesis Tidal Power
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|u.n|3
dAC AC
u n A
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P o w e r
D i s s i p a t e d
T o t a l R e s i s t a n c e t o F l o w
( n a t u r a l a n d d u e t o t i d a l d e v i c e s )
A
B
C
D
E x t r a c t e d P o w e r
T o t a l P o w e r D i s s i p a t e d
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7/27/2019 Thesis Tidal Power
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16/27
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7/27/2019 Thesis Tidal Power
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F r= u/
gh,
u
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h
g
2/3
1/3
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A
u
T
2 4 2
ai = 1
2,
p
X
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u2 = 2u
41 2
At4 = ( 2/ 4)A
ub4 = u
ut4 = 4uu1 = u
3
AT
X
ub4 = u
At1 = 2A
p+1
2u2 =p2t+
1
222u
2,
p3t
+1
22
2u2 =p+
1
22
4u2.
t
p= p2t p3t=12
u2
1 24
.
T
A=
1
2u2
1 24
.
X T =u2A2(4 1) .
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X
T
A=u22(1 4) .
2 =1 +4
2 ,
2
4
P =T 2u=1
2u3A2
1 24
=
1
2u3A
(1 +4)
2
1 24
.
CT CP
T = 1
2u2A
1 24
=
1
2u2ACT,
P = 1
2u3A
(1 +4)
2
1 24
=
1
2u3ACP.
4 4 = 1/3 2 = 2/3 CT = 8/9
CP = 16/27
X
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41 2
ub 4
At 1
At 4
ub 4
ut 4
u1 = u
3
AT Mixing
5
u5
A/B
X
A/B
B 1
u = ub4
X
X= 0
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4= 1/3
u2AB24+u2A (1 B2) =uAu5,
u5=u1 B (1 24)2
.
B = 0
u5 u
PW
PW =1
2u3A2
24+
1
2u3A
1B
21
2u
A
Bu25,
PW =1
2u3A2(1 4)2
1 B (1 +4)
2
.
= P
P+PW=
(1 +4)
(1 +4) + (1 4) (1 B2) .
4 = 1/3
PW =P /2 2/3 B = 0
4 = 2 = 1
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41 2
ub 4
At 1
At 4
ub 4
ut 4
u1 = u
3
AT Mixing
5
u 5 = u
A/B
X
4
u4b= u (1 B2)
(1 B2/4) =4u,
4>1
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p p4
p p4=12
u2
24 1
=
1
2u2
(1 B2)2
(1
B2/4)
2 1
.
p2t p3t =p p4+12
u2
1 24
,
p2t p3t =1
2u2 (1 B2)
2
(1 B2/4)2 2
4 .
T
A=
1
2u2
(1 B2)2
(1 B2/4)2 24
.
pA/B p4A/B T =u2A2(4 1) + u2A/B (1 B2)
(1 B2)(1 B2/4) 1
.
p
p4 =
T B
A
+u22
4
B (1 4)2
(1 B2/4),
24(22 1 4) +B2
224+2 342
= 0.
B
2 4
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B = 0
2 = (1 +4)/2
B 1
2 1 4 1 B
2 = (1 +4)
(1 +B) +
(1 B)2 +B (1 1/4)2.
2
P =
1
2 Au3
2 (1 B2)2
(1 B2/4)2 2
4 .
B
4 = 1/3
Pmax=1
2Au3
16
27
1
1 B2
.
CP =1627 1
1 B2 ,
B
1 + 2B
CP = P
12
u3A+uAp=
CP1 +BCT
,
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X
B > 0
X
(p p4) A
1/B 24
X=u2A (1/B 2)
(1 B2)
(1 B2/4) 1
,
p
p4
X=1
2u2A
24
(1 4) (4 1) .
4
B >0
B = 0
4 = 1 X = 0
p4 p5 = u2 2B (1 4)2
4(1 B2/4) .
PW =1
2u3A2
24+
1
2u3A (1/B 2) 24 (A/B)
1
2u3 u (p4 p5)
.
PW =
1
2 u
3
A2(1 4)21 + B2(1 B2)24(1 B2/4)2 .
B = 0
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B >0
(p p5) uAC=T u. 2uT
= PP+PW
=2.
2 = 1 B
4
4 = 1/3 2 = 2/[3 (1 +B)]
= 23 (1 +B)
.
p= gz
z
h + a
a h h gh/2 + ga + O(a2/h) ga
a.
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p p4=4B (3 B)9 (1 B)2 u
2,
p5 p4= 8B9 (1 B) u
2,
CT = 8 (1 +B)
9 (1 B)2 .
B
CD CT/2
(p p4)/gh 1
F r2 = u2
gh
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Mixing
41 2 5
ub 4
h5
At 1
At 4
ub 4
u5ut 4
h
h1
= h
u1
= u
3
AT
X
h
b
u
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h A
b
ur ne rea(a) (b)
AA
b
A AA
h+u2
2g=h4+
u2242g
,
h+u2
2g =h2t+
u2222g
,
h3t+u222
2g =h4+
u2242g
.
h2t h3t = u2
2g
24 24
,
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T
gBbh=
u2
2g
24 24
.
1
2gb
h2 h24 T =u2bhB2(4 1) +u2hb (1 B2) (4 1) .
T
12gb h2 h24 Bbh u22 24 24= u2bhB2(4 1) +u2hb (1 B2) (4 1) .
h4 = Bh24
+h(1 B2)
4,
2= 4Bh
(h (1 4) +4(h h4))(4 4) ,
2=2 (4+4) (4 1)3 (B24 B44)1
4 + (24 1) (44)1 .
4 B
2 4
4 F r
h4 2
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0 0.2 0.4 0.6 0.8 10
0.5
1
1.5
2
4
Cp,
CP
0 0.2 0.4 0.6 0.8 10
0.2
0.4
0.6
0.8
1
1.2
Cp,
4
CP
4
F r= 0.1
B = 0.1
B = 0.2
B = 0.3
B = 0.4
B = 0.2
F r= 0.01
F r= 0.1
F r = 0.2
F r = 0.3
F r2
2 44+ 24F r
234
2 2B+F r2 24 44+ 24F r2 4 4+F r2
2 + 44 2B24 2
= 0.
4
F r
B
4
T
P = 2uT
T =1
2u2Bbh
24 24
=
1
2u2BbhCT,
P =1
2u3Bbh2
24 24
=
1
2u3BbhCP.
4
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4 = 1/3,
2
4
B 0
4 1
(4 1)3 B
2 = (1 +4)/2,
F r = 0
(1 B) 24 (24 2) 4+
24 B24 1
= 0,
4= 1 B21
B2/4
,
B
F r
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E4= u2
2g+h=
2
4 u2
2g +h4.
dE4/dh4= 0
h4
h4
d
d (h4/h)
24
= 2F r2
.
4
B 0
B 1
1
2gb
h2 (h h)2 T =bhu uhh h u
.
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0 0.2 0.4 0.6 0.8 115
10
5
0
5
10
4
4
Unphysical solutions
Real part of complex 4
Supercritical Bypass flow
Subcritical Bypass flow
0 0.2 0.4 0.6 0.8 10
0.2
0.4
0.6
0.8
1
Fr
B
4=0.01
0.99
0.8
0.50.2
Physically inadmissible
Physically admissible
F r = 0.14
B = 0.64
F r = 0.3
B = 0.2
4 4
1
2
h
h
33
2
h
h
2+
1 F r2 + CTBF r
2
2
h
h CTBF r
2
2 = 0.
h/h 0, 1
h
PW =1
2u3Bbh2
24+
1
2u3bh (1 B2) 24
1
2u3bh
h
h h2
+hbu (h4 h5) g.
P+PW =gubhh
1 F r2 1 h/(2h)
(1 h/h)2
.
gubhh
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= P
P+PW=
P
gubhh
1 F r2 1 h/2h
(1 h/h)21
.
F r 0
2
F r2
P= (2u) T
= 2uTgubhh
,
u
uT =gubhh h2 hh F r2 hhh h =gubhh,
F r2
h/h
h/h 0 F r 0
2
CTBF r
2/2
=2(1 h/(2h)) F r2 (1 h/h)1
1 F r2 (1 h/(2h))(1 h/h)2 .
F r2 (1 h/h)1
1
2
1 12
h
h
.
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1 1
2h/h
,
2
2
B
2
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0 0.2 0.4 0.6 0.8 10
0.2
0.4
0.6
0.8
1
2
=(1h/(2h))1
B
h/h=0.01
0.02
0.05
0.1
0.010.020.05
2 B F r = 0.05 F r = 0.15
2
2 B
2 B
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4 = 1/3
F r = 0)
F r < 0.1
B = 0.05
B = 0.4
4
4
4 = 1/2 4 = 1/6) 4
u2h
4= 1/3
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0 0.1 0.2 0.3 0.40
5
10
15
20
25
Fr
CT
Physically inadmissible
B=0.7
0.6
0.5
0.4
0.30.2
0.10.05
0 0.1 0.2 0.3 0.40
5
10
15
Fr
CT
B=0.4
B=0.05
Physicallyinadmissable
0 0.1 0.2 0.3 0.40
2
4
6
8
10
Fr
CP
Physically inadmissable
B=0.7
0.6
0.5
0.40.3
0.2
0.10.05
0 0.1 0.2 0.3 0.40
1
2
3
4
5
Fr
CP
B=0.4
B=0.05
Physicallyinadmissable
CT CP
CT
F r
4 = 1/3
CT F r 4 = 1/2 4 = 1/3 4 = 1/6
CP F r 4 = 1/3 CP F r 4 = 1/2
4 = 1/3 4= 1/6
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0 0.2 0.4 0.6 0.8 1
0.35
0.4
0.45
0.5
0.55
0.6
0.65
0.7
B
Fr=0.3
0.20.05 00.1
Physically inadmissible
0 0.2 0.4 0.6 0.8 10
0.05
0.1
0.15
0.2
B
h/h
Physically inadmissible
Fr=0.3 0.1
0.2
0.05
4= 1/3,
4= 1/3,
F r= 0
4
B 0.45 F r 0.2
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0 0.1 0.2 0.3 0.40
0.02
0.04
0.06
0.08
0.1
Fr
h/h
0.5
0.40.4
0.4
0.3
0.2
0.6
0.05
0.1
B=0.7
0 0.1 0.2 0.3 0.40
0.02
0.04
0.06
0.08
0.1
0.12
Fr
h/h
B=0.60.4
0.2
0.1
h/h
4 = 1/3 4 = 1/2 4 = 1/6
h/h
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102
2
2 < 1/2
2
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ux
+v
y +
wz
= 0,
ut
+uux
+vuy
+wuz
= X1
p
x+
2ux2
+2u
y 2 +
2uz2
,
v
t
+uv
x
+vv
y
+wv
z
= Y
1
p
x
+
2v
x2 +
2v
y 2 +
2v
z2 ,
wt
+uwx
+vwy
+wwz
=Z1
p
x+
2wx2
+2w
y 2 +
2wz2
,
u= (u, v, w)T
x= (x,y,z)T p
,
X, Y,
Z
u, u
u = u+ u
.
Tf
u = 1
Tf
t+Tft
udt, u
= 1
Tf
t+Tft
u
dt= 0.
Tf
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ux
+v
y +
wz
= 0,
x
ut
+uux
+vuy
+wuz
= X1
p
x+
1
x
ux
uu
+
1
y
uy
uv
+1
z
uz
uw
uu
u
v
u
w
uu=t
ux
+u
x
, uv=t
uy
+v
x
, uw=t
uz
+w
x
,
t
ut
+uux
+vuy
+wuz
= X1
p
x+
x
t
ux
+u
x
+
y tuy +vx + ztuz +wx ,
X= 2f v, Y =
2f u, , Z=
g,
g
f
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z
x
(x,y,t)
h(x,y)
y
u*(x,y,-h,t)=0
1
P
z g= 0.
P =Pa+g ( z) ,
Pa z=
ho
udz+
y
ho
vdz u(x , y, , t) x
u(x,y, ho, t) hox
v(x , y, , t)
y v(x,y, ho, t)ho
y +w(x , y, , t) w(x,y, ho, t) = 0.
z = (x,y,t)
z =ho(x, y)
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u(x,y, ho, t) = 0,
t+u(x , y, , t)
x+ v(x , y, , t)
y =w(x , y, , t).
t+
uh
x +
vh
y = 0,
h= ho+
u= 1
h
ho
udz, v=1
h
ho
vdz.
u
x
ho
ut
+u2
x +
uvy
+uw
z
dz=
ho
f vdz 1
ho
P
xdz+
ho
x
2t
ux
+
y
t
uy
+v
x
+
z
t
uz
dz.
uh
t +
xxu2h
x +
xyuvh
y =f vh 1
ho
P
xdz+
x
ho
2tux
dz 2t ux
x 2t u
x
ho
hox
+
y
ho
t
uy
+ v
x
dz t
uy
+v
x
y+
t
uy
+ v
x hohoy
+t
uz
t
uzho
,
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xx xy
xx= 1
hu2
ho
u2dz, xy = 1
huv
ho
uvdz.
y
yy = 1
hv2
ho
v2dz.
u v
xx, xy yy
ho
tux
dz=Thu
x,
T
u/y, v/x v/y. T
z= (x,y,t)
W.
z =ho(x, y)
x,b
b,x
=t
uz
ho
+ 2tux
ho
hox
+t
uy
+v
x
ho
hoy
.
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b,x
=t
uz
ho
.
b,y
y
t+
uh
x +
vh
y = 0,
uh
t +
u2h
x +
uvh
y =f vh gh
x
b,x
+
x
2Th
u
x
+
y
Th
u
y+
v
x
,
vh
t +
uvh
x +
v2h
y = f uh gh
y
b,y
+
x
Th
uy
+v
x
+
y
2Th
v
y
.
(b,x, b,y)T =t
uz
ho
,
vz
ho
T=Cdu|u|,
u = (u, v)T Cd
fDW C n
Cd= fDW8
= gC2
= gn2
h1/3.
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u(z) =uf
(z/zo) , uf=
|b|
1/2,
= 0.4
zo
Cd =
1 +
(zo/h)
2.
zo
zos zof
zof=2r
r,
r r
zof
t+
uh
x +
uh
y = 0,
uh
t +
u2h
x +
uvh
y = f vh gh
x+
b,x
,
vh
t +
uvh
x +
v 2h
y = f uh gh
y+
b,y
,
7/27/2019 Thesis Tidal Power
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t +ho
u
x +ho
v
y = 0,
u
t +g
x = b,x
ho+f v,
v
t+g
y = b,y
ho f u.
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7/27/2019 Thesis Tidal Power
66/253
7/27/2019 Thesis Tidal Power
67/253
t u r b i n e s
t u r b i n e s
t u r b i n e s
(a) Strait between two oceans (b) Bay or estuary
(d) Headland(c) Strait between an island and a
semi-infinite landmass.
(i)
(ii)
(i)
(ii)
t u r b i n e s
t u r b i n e s
t u r b i n e s
L
L
L
L
L2
L1
L
L1 L2
0
5
10
15
20
25
(a) (b) (c) (d)
(a)/(b)
(a)/(b)
(a)/(c)
(a)/(c)
(a)/(d)
(a)/(d)(c)/(d)
(c)/(d)
7/27/2019 Thesis Tidal Power
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7/27/2019 Thesis Tidal Power
69/253
7/27/2019 Thesis Tidal Power
70/253
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n+ 1
n
n= 15
n < 5
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U
t +
F(U,Q)
x +
G(U,Q)
y =S(U),
QRx(U)x
Ry(U)y
= 0,
U = (h,uh,vh)T Q =
( ux
, uy
, vx
, vy
)T
F(U,Q) =
uhu2h+gh2/2 2hT uxuvh hT
vx
+ uy
, G(U,Q) =
vh
uvh hT
vx
+ uy
v2h+gh2/2 2hT vy
,
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Rx(U) =
uhh
0
vhh
0
, Ry(U) =
0
uhh
0
vhh
, S(U) =
0
gh zx
x,b
+f vh
gh zy
y,b f uh
,
/t = h/t
gh= (gh2/2) ghz z= ho
T = 0
F(U) =
uho
ghoh
0
, G(U) =
vho
0
ghoh
,
ho(x, y)
U= (h,uho, vho)
T
n = 1
T = 0
(x, y)
Ne e(x, y)
i
e
U
t +
F(U,Q)
x +
G(U,Q)
y S(U)
ide= 0,
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e
QRx(U,Q)
x Ry(U,Q)
y
ide= 0.
Uh
i
U(x, y) Uh(x, y) =Mk
Uk(x, y)k(x, y) =Mk
Uk(x, y)k(x, y),
Q(x, y) Qh(x, y) =Mk
Qk(x, y)k(x, y) =Mk
Qk(x, y)k(x, y),
{Uk} {Qk}
{Uk} {Qk} {k} {k}
n
M
M= 1
2(n+ 1)(n+ 2)
t
e
M
k
Uklk
ide
e
ix
F (Uh,Qh) +i
yG (Uh,Qh)
de+
e
(F (Uh,Qh) nx+ G (Uh,Qh) ny) ide=
e
S (Uh) ide
{ak} (a1, . . . , aM)T ,k
M
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e
M
k
Qklk
ide+
e
ix
Rx(Uh) + i
yRy(Uh)
de
e
(Rx(Uh) nx+ Ry(Uh) ny) ide= 0,
n= (nx, ny)T
e e
e
n = 0
FGRx Ry
t
e
M
k
Uklk
ide
e
ix
F (Uh,Qh) +i
yG (Uh,Qh)
de+
e
F (Uh,Qh) nx+G (Uh,Qh) nyide= e
S (Uh) ide,
e
M
k
Qklk
ide+
e
ix
Rx(Uh) + i
yRy(Uh)
de
e
Rx(Uh) nx+Ry(Uh) nyide= 0.
{Uk} {Qk}
i = lk
M
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d
dt{Uk} = M1 [B+ E S] , {Qk} = M1 [A G] ,
M
M(i,k)=
e
lilkde, i, k M,
B(i) = Bx(i)+ By(i) =
e
lixF (Uh,Qh)
de+
e
liyG (Uh,Qh)
de,
E(i) =
e
S (Uh) lide,
S(i) =
e
li
F(Uh,Qh)nx+ G(Uh,Qh)ny
de,
A(i) =
e
Rx(Uh) nx+Ry(Uh) ny lide, G(i) = Gx(i)+ Gy(i)=
e
lixRx(Uh)
de+
e
liyRy(Uh)
de.
iM. {Uk} {Qk}
d
dt{Uk} =LU(Uh,Qh), {Qk} = LQ(Uh).
{U(p)k } {U(p+1)k } t
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U
(1)k
=U
(p)k
+ tLU(U
(p)h ,Q
(p)h ),
U(2)k
=
3
4{Upk} +
1
4
U
(1)k
+
1
4tLU(U
(1)h ,Q
(1)h ),
U
p+1k
=
1
3{Upk} +
2
3
U
(2)k
+
2
3tLU(U
(2)h ,Q
(2)h ),
{Q(i)k} =LQ(U(i)h ) t
t=
hm
0.5n2(
u2 +v2 +
gh)
hm
n= 1
n2
n
n
2n+ 1
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Cd
CT ot = Cd+kt,
kt
P
P = kt
Cd+ktPt,
Pt CT ot.
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kt
lv
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Top ViewLine
Discontinuity y
x
u
u=uv=v
y
z
lv
lhLine
Discontinuity
y
x
Top V ew
v=v
u=u
u
y
z
lv
Side View
z
xu5u
h5h
lv
u
u
v,
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lv
b
lv
lv
lv lh
lv
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A
B
A
hL uL hR uR
A
F(hL, u
L, v
L) B F(h
R, u
R, v
R)
hL u
L h
R u
R
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Line Discontinuity
Element, A
Element, B
x
y
hL
,uL
,vL
hR
,uR
,vR
x
t
hL
uL
vL
*
*
* hR
uR
vR
* * *
hL
uL
vL
hR
uR
vR
I+ = uL+ 2cL= uL+ 2c
L,
I = uR 2cR=uR 2cR,
(cL)2uL= (c
R)
2uR,
c(L,R) =
gh(L,R)
1
2
h
h
33
2
h
h
2+
1 F r2 + CTBF r
2
2
h
h CTBF r
2
2 = 0,
B
F r
h
h
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|hR hL| CT
4
h/h = p (F r, B , 4)
g(z) =z
1 p(F r, B , 4),
z=cL, F r= (I
+ 2z) /z, B =Ag/z2; uL>0,
z=cR, F r= (I + 2z) /z, B =Ag/z2; uL 0,
I+ 2g(z)
z2
z2g(z)2
[I+ I 2 (g(z) +z)] , z=cR; uL
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=ktu |u| , u
g(z) =z
1 p(F r, B , 4), =
2|x|Lf
3+ 3|x|Lf
2, |x| < Lf
1 , |x| Lf,
x
Lf
= 1/40
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2000
Cd= 5 103
4
Cd = 5 104
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Turbine fence
Upstream
Boundary
Downstream
Boundary
0 0.05 0.1 0.15 0.2 0.25 0.30
0.01
0.02
0.03
0.04
0.05
0.06
0.07
0.08
Fr
h/h
B=0.6
4
=1/3
B=0.2
4
=1/3
B=0.4
4
=1/3
0 0.05 0.1 0.150
0.005
0.01
0.015
Fr
h/h
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0 2000 4000 6000 8000 10000
0
1000
2000
3000
4000
0 2000 4000 6000 8000 10000
0
1000
2000
3000
4000
B = 0.6
4 = 1/3
Cd= 5 4 h= 10
10000
4= 1/3
= 1/40
n= 5
n.
n
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B = 0.25
Cd= 1105
B = 0.5, 0.6
t = 80000
104
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0 0.2 0.4 0.6 0.8 10
0.005
0.01
0.015
0.02
0.025
0.03
Position Along Fence
h/h
Intended Depth Change
Simulated Depth Change
1 2 3 4 5
6.75
6.8
6.85
6.9
x 104
n
P(W)
1 2 3 4 5
302.6
302.8
303
303.2
303.4
303.6
303.8
304
304.2
n
Q(
m3/s)
n
n
200 250 300 3505
5.1
5.2
5.3
5.4
5.5
5.6x 10
4
Q [m3/s]
P[W]
B=0.5
B=0.7
B=0.6
Cd = 1
105.
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O p e n B o u n d a r y
O p e n B o u n d a r y
Ub= (hb, ubhb, vbhb)T.
h(s, t)
s s(b) s
ti,
hb= h(s(b), ti) ub=uin+ 2
ghin ghb .
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x
t
h u*
*
hi n
ui n
vi n
hb
ub
vb
I+ I-
x
in
b
I =
u2gh
u(hho)g/ho ho
I+ =uin+ (hin ho)
g/ho
I =ub (hb ho)
g/ho
I
ub= (hb
ho)g/ho
I
ub hb
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I
hb ub = vb = 0
(x,y,t) =exp[(x+L/4)2/(3h)2]
u(x,y, 0) =(x,y,t)
g/ho,
ho= 100 (x, y) [L, 0][0, L/10]
L = 1000
x =L
x = 0
ub = hb = 0.
hm=L/20
E=
B/2B/2
0L/2
1
2g2 +
1
2hu2
dxdy.
L2
E
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5 4 3 2 1 0
x 105
100
100.1
100.2
100.3
100.4
100.5
100.6
x (m)
ho
+(
m)
5 4 3 2 1 0
x 105
100
100.1
100.2
100.3
100.4
100.5
100.6
x (m)
ho
+(
m)
5 4 3 2 1 0
x 105
100
100.1
100.2
100.3
100.4
100.5
100.6
x (m)
ho
+(
m)
5 4 3 2 1 0
x 105
100
100.1
100.2
100.3
100.4
100.5
100.6
x (m)
ho
+(
m)
n= 3
t= 0.44tf, t= 0.53tf, t= 0.61tf, t= 0.70tf.
tf= (L/2)/
gh
102, 105,
108,
n= 1, 2
i = (A/2) (kx+t) k = /
gho ho
=
A1 (k(x+L))e
jt
x 0,
H
(1)0
1 = 1
(kL) + (2ka/)
(kL)
(2ka/e) jka
(kL) ,
2 = 1jka (kL).
a/L = 0.1
ho = A/ho = 2.5 103
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2a
L
y
x
= ( A / 2 ) c o s ( k x + w t )
8 9 10 11 12
1
0.5
0
0.5
1
t/T
2/A
8 9 10 11 120.08
0.06
0.04
0.02
0
0.02
0.04
0.06
0.08
t/T
2/A
(L, 0)
(R, 0),
kL = 0.5.
hb, ub)
R
3L
hb=ho+ A (k(x+L))ejt , ub= jgk A (k(x+L))ejt , vb= 0,
kL = 0.5
(L, 0) (0, R)
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0 0.5 1 1.5 2 2.5 30
1
2
3
4
5
6
7
8
9
2||/A
kL
1 2 3 4 56.65
6.7
6.75
6.8
6.85
6.9
2||/A
n
2 3 4 5 60
1
2
3
4
5
6
7
8
R/kL
2||/A
kL=1.4
kL=3
kL=0.8
n
kL = 1.4
ka
1
kL = 1.4
kL = 0.8, 3
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g x
=u
t +u
u
x+
Cd |u| uh
,
x u
Cd
U,
L
1
g x
= Uu
t +
U2
Lu
u
x+
U2
hd
Cd |u| uh
,
hd
= 1
Kc=
L
U ,
=Cd =CdL
ho
L
ho
Kc
C
d
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0 10 20 30 400
0.2
0.4
0.6
0.8
1
L (km)
B/L
Ave~0.35
0 10 20 30 400
0.05
0.1
0.15
0.2
0.25
0.3
L (km)
Fr
0 0.5 1 1.5 20
0.5
1
1.5
2
Cd
1/K
c
Cd = 0.001
1/Kc 0.5, C
d 0.5 1/Kc 0.5, C
d 0.5
1/Kc 0.5, C
d 0.5
Q
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0 10 20 30 400
0.05
0.1
0.15
0.2
0.25
0.3
0.35
0.4
Reduction in velocity (%)
P/
(rawk
ineticflux)
Figure 1.3(a)
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u
t +u
u
x+g
x= FGC,
FGC
Q
cdQ
dt go =
L0
FGCdx 12
|ue| ue,
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c=
L0
A1c dx Ac(x) o(t)
o =a (t) a
ue
g)
Cdu
2/h
Cd
L0
FGCdx=
L0
Cdu2
h dx+
L0
Ftdx=
L0
Cdh
dx+1
|Q| Q,
Ft FGC 1
P =Q
L0
Ftdx= 1|Q| Q2,
ga
t = cdQ
dt + (0+1) |Q| Q, 0=
L0
CdhA2c
dx+1
2
1
(Ac)e
2.
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t= 1t
Q = ga (c)1 Q
0 = 0(c)2(ga)1
1 = 1(c)
2(ga)1
t =
dQ
dt + (0+1) |Q| Q.
0
0
0
1
1 = 0 1 1
Q 0
Pmax,
Pmax = gaQmax,
Qmax
0
0 = 0.22
0 0 0 0)
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0 5 10 15 20 25 300.5
0.55
0.6
0.65
0.7
0.75
0
Q/Qmax
o
o
Pmax= 0.38
1
2 (Ac)e |ue|3
,
1
N
B
4
L0
Ftdx= NCTB
2 u2 =1Q |Q| , CT = (1 B2)
2
(1 B2/4)2 24,
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2= (1 +4)
(1 +B) +
(1 B)2 +B(1 1/4)21
P=Q
L0
Ftdx= NCTB
2 ACu
3,
Pa=P =2P .
4 = 1/3
Pa = 2Pmax= 23(1 +B)gaQmax.
4= 1/3
4
CTB/2
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L W ho Cd A A/ho F r L/U C dL/h
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=(A/2)cos(wt-kx)TurbineFence
L
W
Ri
P2
P3
P1
x
yaa
Section aa
n = 3
4L
P1, P2
P3
4L, 0), (0, 0)
(L/2, 0)
u
y = 0
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( |u|)2 /2g
|u|
.
x
4 = 1/3
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5000 0 5000 10000
6000
4000
2000
0
2000
4000
6000
x (m)
y(m)
0.5 0 0.5 1 1.524.5
25
25.5
26
26.5
27
x/L
+h
o(m)
2 1 0 1 2 3 4
x 104
2
1
0
1
2
x 104
x (m)
y(m)
0.5 0 0.5 1 1.579
79.5
80
80.5
81
81.5
82
x/L
+h
o(m)
1000 0 1000 2000 3000
1500
1000
500
0
500
1000
1500
x (m)
y(m)
0.5 0 0.5 1 1.59.4
9.6
9.8
10
10.2
10.4
x/L
+h
o(m)
u
t/T = 8
y = 0
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105 3/
(4L, 0)
(5L, 0)
P1, P2 P3
P1
P3
P2
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0.4 0.6 0.8 1 1.2 1.4 1.6
x 105
0
0.5
1
1.5
2
2.5
3
3.5x 10
8
Q (m3/s)
AveragePower(W)
Extracted Power
Dissipated Power
Available Power
0 0.1 0.2 0.3 0.4 0.5 0.6 0.70.2
0.3
0.4
0.5
0.6
0.7
0.8
B
||(m)
Pt 1
Pt 2
Pt 3
0 0.1 0.2 0.3 0.4 0.5 0.60
10
20
30
40
50
60
70
80
90
B
Phase
Lag
(o)
Pt 1
Pt 2
Pt 3
P1, P2 P3
P1, P2 P3
2/3
P2 P3
P1
Cd
Cd
PGC
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a
Qmax 3/ ) P P /PGC P /Pf P /Pd Cd,eff Q/Qmax a/a0
Pf Pd
a/a0
(4L, 0)
(5L, 0)
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Cd,eff
Fr = 0 4 = 1/3 Fr = 0
Cd,eff = 0.35
Kc C
d
Cd
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3 4 5 6 7 80
0.2
0.4
0.6
0.8
1
P/Pmax
t/T
0 2 4 6 8 1 00
0.2
0.4
0.6
0.8
1
/M2
u()[m/s]
3 4 5 6 7 8
0
0.2
0.4
0.6
0.8
1
P/Pmax
t/T
0 2 4 6 8 1 00
0.2
0.4
0.6
0.8
1
/M2
u()[m/s]
4 = 1/3
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Cd,eff
Cd,eff=
CTB/2 F r = 0
Cd,eff Fr = 0
B
4
Fr = 0
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102
101
100
101
102
0
0.5
1
1.5
2x 10
8
CTB/2
MaximumAv
eragePower(W)
102
101
100
101
102
0
0.02
0.04
0.06
0.08
0.1
0.12
0.14
0.16
CTB/2
Fr
4=1/6
4=3/4
4=17/20
4=1/3*
4=1/3
Cd,eff=CTB/2
Cd,eff = CTB/2 Cd,eff F r = 0
B
4
1/3
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0 0.2 0.4 0.6 0.80
0.2
0.4
0.6
0.8
0.1
0.1
0.1
0.1
0.1
0.1
0.1
0.1
0.2
0.2
0.2
0.2
0.2
0.2
0.2
0.4
0.4
0.4
0.4
0.4
0.4
0.6
0.6
0.6
0.6
0.8
0.8
0.
B
4
0 0.2 0.4 0.6 0.80
0.2
0.4
0.6
0.8
0.1
0.1
0.1
0.
0.1
0.1
0.1
0.1
0.1
0.
0.5
0.5
0.5
0.5
0.5
0.5
0.9
0.9
0.9
0.9
0.9
0.9
0.9
B
4
B = 0.5.
Cd,eff
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0.1
0.1
0.1
0.1
0.2
0.2
0.2
0.2
0.3
0.3
0.3
0.3
0.3
0.3
0.4
0.4
0.4
0.4
0.4
0.4
0.5
0.5
0.5
0.5
0.5
0.5
0.5
0.6
0.6
0.6
0.6
0.6
0.6
0.6
0.7
0.7
0.7
0.7
0.7
0.7
0.7
0.8
0.8
0.8
0.8
0.8
0.8
0.80.9
0.9
0.9
0.9
0.9
0.9
0.9
B
4
0.2 0.4 0.6 0.8
0.1
0.2
0.3
0.4
0.5
0.6
0.7
0.8
0.9
0.1
0.1
0.1
0.
0.2
0.2
0.2
0.2
0.3
0.3
0.3
0.3
0.4
0.4
0.4
0.4
0.5
0.5
0.5
0.5
0.6
0.6
0.6
0.6
0.7
0.7
0.7
0.7
0.7
0.8
0.8
0.80
.8
0.8
0.8
0.8
0.9
0.9
0.9
0.9
0.9
0.9
B
4
0.2 0.4 0.6 0.8
0.1
0.2
0.3
0.4
0.5
0.6
0.7
0.8
0.9
0 .1
0.
1
0.1
0.
0.
2
0.2
0.2
0.2
0.
3
0.3
0.3
0.3
0.4
0.4
0.4
0.
0.5
0.5
0.5
0.5
0.6
0.6
0.6
0.6
0.6
0.6
0.6
0.7
0.7
0.7
0.7
0.7
0.7
0.7
0.8
0.8
0.8
0.8
0.8
0.8
0.8 0.9
0.9
0.9
0.9
0.9
0.9
0.9
0.9
B
4
0.2 0.4 0.6 0.8
0.1
0.2
0.3
0.4
0.5
0.6
0.7
0.8
0.9
0 0.2 0.4 0.6 0.8
0
0.2
0.4
0.6
0.8
B
a4
0.1
0.1
0.1
0.1
0.1 0.1
0.1
0.1
.1
.
0.2
0.2
0.2
0.2
0.2
0.2
.
.
0.4
0.4
0.4
0.4
0.4
0.4
.4.
0.6
0.6
0.6
0.6
.
0.8
0.8
0 0.2 0.4 0.6 0.8
0
0.2
0.4
0.6
0.8
B
a4
0.1
0.1
0.1
0.1
0.1
0.1
0.1
0 .1
0.
1
0.2
0.
2
0.2
0.2
0.2
0.20.2
0.2
0.4
0.4
0.4
0.4
0.4
0.4
0.6
0.6
0.6
0.6
0.6
.
0.8
0.8
0.8
.
0 0.2 0.4 0.6 0.8
0
0.2
0.4
0.6
0.8
B
a4
0.1
0.1
0.1
0.1
0.10.1
0.2
0.2
0.2
0.2
0.2
0.2
0.2
0.4
0.4
0.4
0.4
0.4
0.4
0.4
0.4
0.6
0.6
0.6
0.6
0.6
0.6
0.6
0.6
0.
0.8
0.8
.0.8
0.8
0.8
0
B >0.95
B > 0.9.
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0.4 0.6 0.8 1 1.2 1.4 1.6
x 105
0
0.5
1
1.5
2x 10
8
Q
AveragePower(W)
Line Sink
Roughness
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0 2000 4000 6000
3000
2000
1000
0
1000
2000
3000
x (m)
y(m)
3 m/s
0 2000 4000 6000
3000
2000
1000
0
1000
2000
3000
x (m)
y(m)
3 m/s
o20
32
1
0 2000 4000 6000
3000
2000
1000
0
1000
2000
3000
x (m)
y(m)
3 m/s
1
30o
3
2
0 2000 4000 6000
3000
2000
1000
0
1000
2000
3000
x (m)
y(m)
3 m/s
30 m40 m
0 2000 4000 6000
3000
2000
1000
0
1000
2000
3000
x (m)
y(m)
3 m/s
40 m40 m
30 m
2 1 0 1 2
x 104
1.5
1
0.5
0
0.5
1
1.5x 10
4
x (m)
y(m)
90 m
40 m
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6 6.5 7 7.50
1
2
3
4
x 105
t/T
P(W/m)
Point 1
Point 2
Point 3
6 6.5 7 7.50
0.5
1
1.5
2
2.5
x 105
t/T
P(W/m)
Point 1
Point 2
Point 3
a
Q0 3
P
PGC a/a0
hb=ho+(A/2) (tkx)
ub = g/hohb vb = 0 A= 3.5
Cd,eff 9.3 4= 1/3
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8 0 k m
4 0 k m
8 k m
Tidal Strait
1.5 1 0.5 0 0.5 1 1.5
x 105
0
5
10
15
20x 10
4
x (m)
y(m)
21
5 5.5 6 6.5 7 7.5 858
58.5
59
59.5
60
60.5
61
61.5
62
t/T
Pt 1
Pt 2
Cd = 0.0025
15 .
105 3/
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ga
(t) =cdQ
dt +0 |Q| Q+1 |Q| Q.
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R1
=
R0
=
V=
ga
(t)
V
Q
I
V = LdIdt
+RI+ C
Idt,
L
C
R
L = c
R0 =
83
0 |Q|
R1 = 83 1 |Q|
R1
R1
R1
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R0
g (1 4) = (c1+c4)dQ1dt
+ (0,1+0,4) |Q1| Q1+g (2 3) ,
g (2 3) = c2 dQ2dt
+0,2 |Q2| Q2+1 |Q2| Q2,
g (2 3) = c3dQ3
dt +0,3 |Q3| Q3,
Q = Q1 +Q2, ci 0,i
1 2 3
0,3 |Q3| c3
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1
2
3
4
Q
1
Q
2
Q
3
c2, c3 c1+c4 0,2, 0,3 0,1+0,4
c2, c3 c1 +c4 0,2, 0,3 0,1 +0,4
4= 1/3
Cd=
)
a
Qmax
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2000 0 2000 4000 6000 8000
4000
3000
2000
1000
0
1000
2000
3000
4000
5 m/s
4 6 8 10 12
x 104
0
5
10
15x 10
7
AveragePower(W)
Flowrate (m3/s)
4 6 8 10 12
x 104
0.7
0.8
0.9
1
1.1
1.2
1.3
(Q3
)max
/(Q3,0
)max
B=0
0.1
0.2
0.7
0.6
0.50.4
0.3
0 5000 10000 15000 20000
4000
2000
0
2000
4000
6000
8000
10000
12000
x (m)
y
(m)
8000 9000 1000011000120002000
1000
0
1000
x (m)
y(m)
5 m/s
5 m/s
Point 2(11250,650)
Point 1(8750,650)
4 6 8 10 12
x 104
0
0.5
1
1.5
2
x 108
Averag
ePower(W)
Flowrate (m3/s)
4 6 8 10 12
x 104
0.5
0.6
0.7
0.8
0.9
1
(Q1)max
/(Q1,0
)max
300 GW GC05
B=0
0.1
0.2
0.4
0.3
0.5
0.6
0.7
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0,20,3
=
(Q3,0)max(Q2,0)max
2.
(Q2,0)max (Q3,0)max
Q1
Q2=Q1
1 +
0,20,3
+ 10,3
1/21,
P=1 |Q2| Q22 = 1 |Q1| Q21
1 +
0,20,3
+ 10,3
1/23.
Pref=gQ2,0(2,0 3,0) =0,2 |Q2,0| Q22,0
P
gQ2(2,0 3,0) = P
2 |Q2,0| Q22,0=
10,3
0,30,2
1 + 0,20,31/21 +
0,20,3
+ 10,3
1/23
.
2 1/0,3
0,2/0,3 2
0,2/0,3 2/33/2
(Q2)max / (Q2,0)max 1/31/2,
0,2/0,3 0 2 (Q2)max / (Q2,0)max 1/3.
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0 1 2 3 4 50
0.25
0.5
0.75
1
1.25
1.5
1.75
2
2
0,2
/0,3
0 1 2 3 4 50.3
0.3375
0.375
0.4125
0.45
0.4875
0.525
0.5625
0.6
(Q2
)max
/(Q2,0
)max
2
Q1
Pmax=2g (2,0 3,0) Q2,0.
2,0 3,0 = a2 (t) (2,0 3,0) Q2,0 a2(Q2,0)max | (t)|3/2
Pmax = 0.562ga2(Q2,0)max .
a2 a2
2 = 1
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2000 0 2000 4000 6000 8000 1 0000
4000
3000
2000
1000
0
1000
2000
3000
4000
x (m)
y(m)
5 m/s
2 4 6 8 10
x 104
0
0.5625
1.125
1.6875
2.25x 10
8
AveragePower
(W)
Flowrate (m3/s)
2 4 6 8 10
x 104
0.5
0.75
1
1.25
1.5
(Q1
)max
/(Q1,0
)max,
(Q3)m
ax
/(Q3,0
)max
Current Limit
GC05
2000 0 2000 4000 6000 8000 1 0000
4000
3000
2000
1000
0
1000
2000
3000
4000
x (m)
y(m)
5 m/s
2 4 6 8 10
x 104
0
0.5625
1.125
1.6875
2.25x 10
8
AveragePower(W)
Flowrate (m3/s)
2 4 6 8 10
x 104
0.5
0.75
1
1.25
1.5
(Q1
)max
/(Q1,0
)max,
(Q3
)max
/(Q3,0
)max
CurrentLimit
GC05
2000 0 2000 4000 6000 8000 1 0000
4000
3000
2000
1000
0
1000
2000
3000
4000
x (m)
y(m)
5 m/s
4 6 8 10 12
x 104
0
0.625
1.25
1.875
2.5x 10
8
AveragePower(W)
Flowrate (m3/s)
4 6 8 10 12
x 104
0.5
0.75
1
1.25
1.5
(Q
1)m
ax
/(Q1,0
)max,
(Q3
)max
/(Q3,0
)max
CurrentLimit GC05
Cd =
0.0025
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g( b) =c dQdt
+ (0+1) |Q| Q, c= L
0
A1c dx,
Q
L
Ac
0 1
= b
b
dbdt = QS0, b= 1S0
Q dt,
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R1
=V=
S0
=a
(t)
ga
(t) =cdQ
dt + (0+1) |Q| Q+ 1
(S0/g)
t0
Q dt.
C = S0
g
L =c
R = (0+1) |Q| ,
1 |Q|
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0,1=0,1(c)
2/(ga) =a, b=a
b, Q= Q
ga/(c)
t= 1t
(t) =
dQ
dt + (0+1) |Q| Q +b,
dbdt
=Q,
= g
2cSo,
0
So
Ac 0
P =1|Q|3) 0
Pmax = gaQmax,
ga
Qmax
a
=ab/a,
0 0 1
0 0
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0 10 20 30 40 500.18
0.2
0.22
0.24
0.26
0.28
0.3
0
=9
=4
=2.5
=1.25
0 10 20 30 40 500.5
0.55
0.6
0.65
0.7
0.75
0.8
0
/
0
=9
=4
=2.5
=1.25
4 = 1/3
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=(A/2)cos(wt-kx)TurbineFence
L
Rai
x
y
W
Rab
n = 3
4L
Rab A Qmax 3 0 0 Cd,eff P PB
o
o
o
o
o
o
A
Qmax 0
ab/a ab
Cd,eff
PB
Cd= 0.0025 Rai=
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2 4 6 8
x 104
0
1
2
3
4
5
x 108
Flowrate (m3/s)
Avera
gePower(W)
0.6
0.5
0.4
B=0
0.8 0.70.75
0.9
0.85
0.3
0 0.2 0.4 0.6 0.80
2
4
ElevationAmplitude(m)
Blockage Ratio
0 0.2 0.4 0.6 0.80
50
100
PhaseLag(Deg)
|b|
|b|
Phase Lag
MaximumPower
|b|
| b|
4= 1/3
0
0
o
1
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101
100
101
102
0
1
2
3
4
5x 10
8
CTB/2
P(W)
Case 64
Case 61
101
100
101
102
0
0.02
0.04
0.06
0.08
0.1
0.12
0.14
0.16
CTB/2
Fr
Case 61
Case 64
Cd,eff = CTB/2 Cd,eff = CTB/2 Fr = 0 Cd,eff
4 = 1/3
4= 1/3.
Cd,eff)
Cd,eff
4 = 1/3
4 = 1/2
Cd,eff
F r= 0
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0 0.2 0.4 0.6 0.80
0.2
0.4
0.6
0.8
.
0.1
0.1
0.1
0.1 0.1
0.1
0.1
0.2
0.2
0.2
0.2
0.2
0.2
0.
2
0.2
0.4
0.4
0.4
0.4
0.4
0.
4
0.4
0.6
0.6
0.6
0.6 0.
6
0.8
0
0.8
B
a4
0 0.2 0.4 0.6 0.80
0.2
0.4
0.6
0.8
0.1
0.1
0.1
0.1
0.
0.2
0.2
0.2
0.4
0.4
0.4
0.6
0.6
0.8
B
a4
Cd,eff
Cd,eff
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1 0 1 2
x 104
1
0.5
0
0.5
1
x 104
x (m)
y(m)
Tidal fence
104
3/ .
= 0.21
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5000 10000 150000
0.5
1
1.5
2
2.5
3
3.5x 10
6
Flowrate (m3/s)
Averag
ePower(W)
Revised Calculation: 2.0E+06 W
Blanchfield et al. (2008): 2.8E+07 W
B=0
0.3
0.4
0.5
0.6
0.70.8
0.9
0 0.2 0.4 0.6 0.80
0.1
0.2
0.3
0.4
0.5
0.6
0.7
0.8
Elevation
Amplitude(m)
Blockage Ratio
0 0.2 0.4 0.6 0.80
2
4
PhaseLag(Deg)
|b|
|b|
Phase Lag
MaximumPower
|b| | b|
4 = 1/3
a
= 0.21
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S(b) =So
1 +
bhe
,
he So
dbdt
=Q (1 +b)
,
= a/he = 0
= 0
T =0 +1)
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S
o
L
A ( x )
x
Top View Side View
0 0.5 1 1.5 2 2.5 30
0.5
1
1.5
2
2.5
3
3.5
4
1/2
(V)
max
T
=0.075
T
=0.15
T
=0.5
= 1
= 0.5
T = 0.075.
t 1/2t
V
Q =dV/dt,
(1/2t) =
d2V
dt2 +1(0+1)
dV
dt
dV
dt +1
(1 + (+ 1)V )
1/(+1) 1
.
(1/2t) =
d2V
dt2 +1(0+1)
dVdt dV dt +V 2(V )2 + 22 (V)3 ,
= 1.
V
1/2
1T
0.5
= 1
T 0.15
T 0.15 0.5 = 1
T,
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7.613 0 9.811.5
1.45 0 8
= 1
= 1 he
ab/a 1.1
1.5S0 = 1
0.5
0 = 10 = 1 = 4 = 0
= 0.5),
= 0.5
= 0.5
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0 0.5 1 1.5 2
1
0.5
0
0.5
1
t/T
Q
0 0.5 1 1.5 20.2
0.3
0.4
0.5
0.6
0.7
0.8
0.9
1
1.1
1.2
1.3
1.4
1.5
1.6
1.7
1.8
t/T
S/S0
0 = 10 = 1 = 4 = 0
= 0.5
= 0.5
T
T
T
T
T 0
= 4
T
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0 0.5 1 1.5 20
0.2
0.4
0.6
0.8
1
t/T
P
= 2.5, T = 10.
0 0.5 1 1.5 20
0.2
0.4
0.6
0.8
1
t/T
P
= 4, T = 10.
0 0.5 1 1.5 20
0.2
0.4
0.6
0.8
1
t/T
P
= 9, T = 10.
0 0.5 1 1.5 20
0.2
0.4
0.6
0.8
1
t/T
P
= 2.5, T = 50.
0 0.5 1 1.5 20
0.2
0.4
0.6
0.8
1
t/T
P
= 4, T = 50.
0 0.5 1 1.5 20
0.2
0.4
0.6
0.8
1
t/T
P
= 9, T = 50.
P / (g2a2/ (c))
= 0.5
= 1
= 0
= 0.2
= 0.5
0 5 10 150
0.1
0.2
0.3
0.4
0.5
a2
/a
T=10, =0.5
T=100, =0.5
T=50, =0.5
T=10, =0.2
T=10, =0.05
a2,
a
T .
= 1.
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0
0
Pmax/gaQmax,
= 4 .
.
= 0.22
s =Smax Smin, s,0 >0
= 0
0
0
/0 s/s,0
0
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0 10 20 30 40 500
0.05
0.1
0.15
0.2
0
DimensionlessAveragePower
0.5 1 1.5
0.14
0.15
0.16
=2.5
=4
=9
0 20 40 60 80
0.14
0.16
0.18
0.2
0.22
0.24
0
=0.2
=0.5
=0
0 10 20 30 400.55
0.6
0.65
0.7
0.75
0
S
/S,0
,/
0
=0.5
=0
=0.2