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212 Chapter 5 ■ Finite Control Volume Analysis<br />

When the gate is closed, the horizontal forces acting on the<br />

contents of the control volume are identified in Fig. E5.16c. Application<br />

of Eq. 5.22 to the contents of this control volume yields<br />

0 1no flow2<br />

(1)<br />

Note that the hydrostatic pressure force, gH 2 b2, is used. From<br />

Eq. 1, the force exerted on the water by the gate 1which is equal to<br />

the force necessary to hold the gate stationary2 is<br />

R x 1 2 gH 2 b<br />

which is equal in magnitude to the hydrostatic force exerted on<br />

the gate by the water.<br />

When the gate is open, the horizontal forces acting on the contents<br />

of the control volume are shown in Fig. E5.16d. Application<br />

of Eq. 5.22 to the contents of this control volume leads to<br />

<br />

cs<br />

urV nˆ dA 1 2 gH 2 b R x 1 2 gh 2 b F f<br />

Note that because the water at sections (1) and (2) is flowing<br />

along straight, horizontal streamlines, the pressure distribution at<br />

those locations is hydrostatic, varying from zero at the free surface<br />

to g times the water depth at the bottom of the channel (see<br />

Chapter 3, Section 3.4). Thus, the pressure forces at sections (1)<br />

and (2) (given by the pressure at the centroid times the area) are<br />

gH 2 b2 and gh 2 b2, respectively. Also, the frictional force between<br />

the channel bottom and the water is specified as F f . The<br />

surface integral in Eq. 3 is nonzero only where there is flow<br />

across the control surface. With the assumption of uniform velocity<br />

distributions,<br />

<br />

cs<br />

urV nˆ dA 1u 1 2r1u 1 2Hb 1u 2 2r1u 2 2hb<br />

Thus, Eqs. 3 and 4 combine to form<br />

ru 2 1Hb ru 2 2hb 1 2 gH 2 b R x 1 2 gh 2 b F f<br />

(2)<br />

(3)<br />

(4)<br />

(5)<br />

<br />

cs<br />

urV nˆ dA 1 2 gH 2 b R x<br />

If the upstream velocity, is much less than so that the<br />

Closed sluice<br />

gate<br />

Control volume<br />

H<br />

Control volume<br />

H<br />

Open sluice<br />

gate<br />

h<br />

z<br />

x<br />

u<br />

(a)<br />

Control volume<br />

Water only<br />

F I G U R E E5.16<br />

Control volume<br />

H h,<br />

u 1 ,<br />

contribution of the incoming momentum flow to the control surface<br />

integral can be neglected and from Eq. 5 we obtain<br />

R x 1 2 gH 2 b 1 2 gh 2 b F f ru 2 2hb<br />

By using the continuity equation, m # bHu 1 bhu 2 , Eq. (6)<br />

can be rewritten as<br />

R x 1 2 H 2 b 1 2 h 2 b F f m # 1u 2 u 1 2<br />

Hence, since u 2 7 u 1 , by comparing the expressions for R x (Eqs.<br />

2 and 7) we conclude that the reaction force between the gate and<br />

the water (and therefore the anchoring force required to hold the<br />

gate in place) is smaller when the gate is open than when it is<br />

closed.<br />

(Ans)<br />

(b)<br />

Water only<br />

u 1<br />

R x<br />

1_<br />

( 2 γ H )<br />

Hb<br />

Section (2)<br />

u 2<br />

1_<br />

( 2 γ H )<br />

Hb 1_<br />

Section F f ( )<br />

(c)<br />

R x<br />

(1)<br />

(d)<br />

2 γ h hb<br />

u 2<br />

(6)<br />

(7)<br />

The linear momentum<br />

equation can<br />

be written for a<br />

moving control<br />

volume.<br />

V5.9 Jelly fish<br />

All of the linear momentum examples considered thus far have involved stationary and nondeforming<br />

control volumes which are thus inertial because there is no acceleration. A nondeforming<br />

control volume translating in a straight line at constant speed is also inertial because there is<br />

no acceleration. For a system and an inertial, moving, nondeforming control volume that are both<br />

coincident at an instant of time, the Reynolds transport theorem 1Eq. 4.232 leads to<br />

D<br />

Dt sys<br />

Vr dV 0 0t cv<br />

Vr dV cs<br />

VrW nˆ dA<br />

When we combine Eq. 5.23 with Eqs. 5.19 and 5.20, we get<br />

0<br />

0t cv<br />

Vr dV cs<br />

VrW nˆ dA a F contents of the<br />

control volume<br />

(5.23)<br />

(5.24)<br />

When the equation relating absolute, relative, and control volume velocities 1Eq. 5.142 is used with<br />

Eq. 5.24, the result is<br />

0<br />

0t cv<br />

1W V cv 2r dV cs<br />

1W V cv 2rW nˆ dA a F contents of the<br />

control volume<br />

(5.25)

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