WATER FLOW 1279
Bends The effect of the presence of bends is to induce
secondary flow currents which are responsible for the addi-
tional energy dissipation:
hK
V
bb
2
2 g
. (25)
The bend loss coefficient, K b , depends on the ratio of the
bend radius, r, to the pipe diameter, d, as well as the bend
angel. For a 90 bend and r / d ratio varying from 1 to 12,
values of K b range from 0.20 to 0.07.
Gates and Gate Valves The gate and gate valve loss can
be expressed as:
hK
V
gg
2
2 g
(26)
The value of the loss coefficient, K g , for gates depends on
a variety of factors. The value of K g for the case having the
bottom and sides of the jet suppressed ranges from 0.5 to 1.0.
for typical values of K g for gate valves see Table 7.
Energy-discharge Relation
In pressure conduit flow, the water is transmitted through a
closed boundary conveying structure without a free surface.
Figure 3 illustrates graphically the various forms of energy
losses which could take place within the conduit. The follow-
ing energy relation can be written:
hh h hlfent tc (28)
in which h end entrance loss, h tc transition loss, h f skin
friction loss. If H denotes the total head required to produce
the discharge and h v represents the existing velocity head,
H h l h v. (29)
Writing Eq. (29) in terms of the velocity heads and their
respective loss coefficients,
HC
V
K
V
K
VV
f
LV
D
K
l
v
2
2
2
2
2
2
2
gggg
g
ent
1
2
tc
2
2
1
2
22
2
−
⎛
⎝⎜
⎞
⎠⎟
⎡
⎣
⎢
⎢
VV 22
2 g
⎤
⎦
⎥,
(30)
where K v combined velocity head and exit loss coefficient.
By the continuity equation:
AV^11 A V2 2 (31)
and
VA
A
12 22 V
1
2
2
22 gg
.^
Equation (30) could be expressed as,
HC
V
V
K
A
A
K
A
A
fL
gD
K
l
v
2
2
2
2
2
1
2
2
2
1
2
2
2
2
1
2
g
g ent tc
⎛
⎝⎜
⎞
⎠⎟
−
⎛
⎝
⎜
⎞
⎠
⎟
⎡⎡
⎣
⎢
⎢
⎤
⎦
⎥
⎥
(32)
in which
CK
A
A
K
A
A
fL
D
lt ent^2 cKv
1
2
2
2
1
2
2
1
2
⎛
⎝⎜
⎞
⎠⎟
−
⎛
⎝⎜
⎞
⎠⎟
⎡
⎣
⎢
⎢
⎤
⎦
⎥
g ⎥
(33)
V
C
H
l
(^212)
1
/ 2 g (34)
QAV
A
C
gH
CA H
22
2
1
12
2
2
2
/
g ,
(35)
TABLE 7
K g for gate values
Fully open 0.2
3
(^4)
open 1.3
1
(^2)
open 5.5
1
(^4)
open 24.0
Exit Loss In general the entire velocity head is lost at
exit and the exit loss coefficient, K e is unity in the equation:
hK
V
ee
2
2 g
. (27)
hent
htc
TEL
Transition
H
hl
–V^2 /2g
hf
hv
p/y
FIGURE 3 Energy relations.
C023_003_r03.indd 1279C023_003_r03.indd 1279 11/18/2005 11:12:13 AM11/18/2005 11:12:13 AM