19.09.2019 Views

fluid_mechanics

Create successful ePaper yourself

Turn your PDF publications into a flip-book with our unique Google optimized e-Paper software.

314 Chapter 6 ■ Differential Analysis of Fluid Flow<br />

y<br />

g<br />

v z<br />

v z<br />

(a)<br />

R<br />

r θ<br />

z<br />

dr<br />

(b)<br />

r<br />

z<br />

F I G U R E 6.34<br />

The viscous flow in a horizontal,<br />

circular tube: (a) coordinate<br />

system and notation used<br />

in analysis; (b) flow through<br />

differential annular ring.<br />

V6.13 Laminar<br />

flow<br />

The velocity distribution<br />

is parabolic<br />

for steady, laminar<br />

flow in circular<br />

tubes.<br />

is only a function of the radial position within the tube—that is, v z v z 1r2. Under these conditions<br />

the Navier–Stokes equations 1Eqs. 6.1282 reduce to<br />

and integrated 1using the fact that 0p0z constant2 to give<br />

r 0v z<br />

0r 1<br />

2m a 0p<br />

0z b r2 c 1<br />

Integrating again we obtain<br />

(6.143)<br />

(6.144)<br />

(6.145)<br />

where we have used the relationships g r g sin u and g u g cos u 1with u measured from the<br />

horizontal plane2.<br />

Equations 6.143 and 6.144 can be integrated to give<br />

p rg1r sin u2 f 1 1z2<br />

or<br />

p rgy f 1 1z2<br />

(6.146)<br />

Equation 6.146 indicates that the pressure is hydrostatically distributed at any particular cross<br />

section, and the z component of the pressure gradient, 0p0z, is not a function of r or u.<br />

The equation of motion in the z direction 1Eq. 6.1452 can be written in the form<br />

1 0<br />

r 0r ar 0v z<br />

0r b 1 0p<br />

m 0z<br />

v z 1<br />

(6.147)<br />

4m a 0p<br />

0z b r2 c 1 ln r c 2<br />

Since we wish v z to be finite at the center of the tube 1r 02, it follows that c 1 0 3since<br />

ln 102 4. At the wall 1r R2 the velocity must be zero so that<br />

c 2 1<br />

4m a 0p<br />

0z b R2<br />

and the velocity distribution becomes<br />

0 rg sin u 0p<br />

0r<br />

0 rg cos u 1 0p<br />

r 0u<br />

0 0p<br />

0z m c 1 0<br />

r 0r ar 0v z<br />

0r bd<br />

v z 1<br />

(6.148)<br />

4m a 0p<br />

0z b 1r2 R 2 2<br />

Thus, at any cross section the velocity distribution is parabolic.<br />

To obtain a relationship between the volume rate of flow, Q, passing through the tube and the<br />

pressure gradient, we consider the flow through the differential, washer-shaped ring of Fig. 6.34b.<br />

Since v z is constant on this ring, the volume rate of flow through the differential area dA 12pr2 dr is<br />

dQ v z 12pr2 dr

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!