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614 Chapter 11 ■ Compressible Flow<br />

If the linear momentum equation 1Eq. 5.222 is applied to the Fanno flow through the control<br />

volume sketched in Fig. 11.19a, the result is<br />

p 1 A 1 p 2 A 2 R x m # 1V 2 V 1 2<br />

where is the frictional force exerted by the inner pipe wall on the <strong>fluid</strong>. Since and<br />

m # R x A 1 A 2 A<br />

rAV constant, we obtain<br />

p 1 p 2 R x<br />

A rV1V 2 V 1 2<br />

(11.84)<br />

The differential form of Eq. 11.84, which is valid for Fanno flow through the semi-infinitesimal<br />

control volume shown in Fig. 11.19b, is<br />

dp t wpD dx<br />

A<br />

rV dV<br />

(11.85)<br />

The wall shear stress, t w , is related to the wall friction factor, f, by Eq. 8.20 as<br />

Friction forces in<br />

Fanno flow are<br />

given in terms of<br />

the friction factor.<br />

By substituting Eq. 11.86 and A pD 2 4 into Eq. 11.85, we obtain<br />

or<br />

(11.86)<br />

(11.87)<br />

(11.88)<br />

Combining the ideal gas equation of state 1Eq. 11.12, the ideal gas speed-of-sound equation 1Eq.<br />

11.362, and the Mach number definition 1Eq. 11.462 with Eq. 11.88 leads to<br />

Since V Ma c Ma 1RTk, then<br />

or<br />

dp<br />

p f rV 2 dx<br />

p 2 D r d1V 2 2<br />

0<br />

p 2<br />

dp<br />

p fk 2<br />

dp fr V 2<br />

f 8t w<br />

rV 2<br />

2<br />

dx<br />

D<br />

rV dV<br />

dx<br />

Ma2<br />

D k Ma2 d1V 2 2<br />

0<br />

2 V 2<br />

V 2 Ma 2 RTk<br />

d1V 2 2<br />

d1Ma2 2<br />

dT<br />

V 2 Ma 2 T<br />

(11.89)<br />

(11.90)<br />

Section (1) Section (2)<br />

Flow<br />

Control volume<br />

p 1 A 1 p 2 A 2<br />

R x<br />

(a)<br />

Semi-infinitesimal control volume<br />

Flow<br />

D<br />

(b)<br />

pA<br />

τw<br />

π<br />

δx<br />

(p + δ p)A<br />

D<br />

δ x<br />

F I G U R E 11.19 (a) Finite<br />

control volume. (b) Semi-infinitesimal control<br />

volume.

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