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172 Chapter 4 ■ Fluid Kinematics<br />

Inflow<br />

portion of<br />

control surface<br />

CS in<br />

δ n<br />

^<br />

n<br />

θ<br />

δA<br />

V<br />

^<br />

n<br />

θ<br />

δV = δ n δA<br />

δ = V δt<br />

V<br />

^<br />

n<br />

θ<br />

δ<br />

V<br />

(a)<br />

F I G U R E 4.15<br />

(b)<br />

Inflow across a typical portion of the control surface.<br />

(c)<br />

By integrating over the entire outflow portion of the control surface, CS out , we obtain<br />

B # out <br />

cs out<br />

dB # out <br />

cs out<br />

rbV cos u dA<br />

The flowrate of a<br />

parameter across<br />

the control surface<br />

is written in terms<br />

of a surface integral.<br />

The quantity V cos u is the component of the velocity normal to the area element dA. From the<br />

definition of the dot product, this can be written as V cos u V nˆ . Hence, an alternate form of<br />

the outflow rate is<br />

B # out <br />

csout<br />

rbV nˆ dA<br />

(4.16)<br />

In a similar fashion, by considering the inflow portion of the control surface, CS in , as shown<br />

in Fig. 4.15, we find that the inflow rate of B into the control volume is<br />

B # in <br />

csin<br />

rbV cos u dA <br />

csin<br />

rbV nˆ dA<br />

(4.17)<br />

We use the standard notation that the unit normal vector to the control surface, nˆ , points out from the<br />

control volume. Thus, as is shown in Fig. 4.16, 90° 6 u 6 90° for outflow regions 1the normal<br />

component of V is positive; V nˆ 7 02. For inflow regions 90° 6 u 6 270° 1the normal component<br />

of V is negative; V nˆ 6 02. The value of cos u is, therefore, positive on the CV out portions of the<br />

control surface and negative on the CV in portions. Over the remainder of the control surface, there is<br />

no inflow or outflow, leading to V nˆ V cos u 0 on those portions. On such portions either V 0<br />

1the <strong>fluid</strong> “sticks” to the surface2 or cos u 0 1the <strong>fluid</strong> “slides”along the surface without crossing it2<br />

1see Fig. 4.162. Therefore, the net flux 1flowrate2 of parameter B across the entire control surface is<br />

B # B# rbV nˆ dA a<br />

out in cs out<br />

rbV nˆ dAb<br />

cs in<br />

<br />

cs<br />

rbV nˆ dA<br />

(4.18)<br />

where the integration is over the entire control surface.<br />

CS in<br />

CS<br />

V • ^<br />

n < 0<br />

^<br />

n<br />

V = 0<br />

^<br />

n<br />

V • ^<br />

n = 0<br />

(a) (b) (c)<br />

^<br />

n<br />

CS out<br />

^<br />

V • n > 0<br />

F I G U R E 4.16<br />

Possible velocity configurations<br />

on portions of the control surface:<br />

(a) inflow, (b) no flow<br />

across the surface, (c) outflow.

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