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6.5 Some Basic, Plane Potential Flows 289<br />

ψ = constant<br />

y<br />

φ = constant<br />

v r<br />

r<br />

θ<br />

x<br />

F I G U R E 6.17<br />

source.<br />

The streamline pattern for a<br />

A source or sink<br />

represents a purely<br />

radial flow.<br />

Also, since the flow is a purely radial flow, v u 0, the corresponding velocity potential can be<br />

obtained by integrating the equations<br />

It follows that<br />

0f<br />

0r m<br />

2pr<br />

1 0f<br />

r 0u 0<br />

f m 2p ln r<br />

(6.82)<br />

v r<br />

~ v r<br />

r<br />

1__ r<br />

If m is positive, the flow is radially outward, and the flow is considered to be a source flow. If m<br />

is negative, the flow is toward the origin, and the flow is considered to be a sink flow. The flowrate,<br />

m, is the strength of the source or sink.<br />

As shown by the figure in the margin, at the origin where r 0 the velocity becomes infinite,<br />

which is of course physically impossible. Thus, sources and sinks do not really exist in real flow<br />

fields, and the line representing the source or sink is a mathematical singularity in the flow field.<br />

However, some real flows can be approximated at points away from the origin by using sources or<br />

sinks. Also, the velocity potential representing this hypothetical flow can be combined with other<br />

basic velocity potentials to approximately describe some real flow fields. This idea is further discussed<br />

in Section 6.6.<br />

The stream function for the source can be obtained by integrating the relationships<br />

to yield<br />

v r 1 r<br />

0c<br />

0u m<br />

2pr<br />

v u 0c<br />

0r 0<br />

c m 2p u<br />

(6.83)<br />

It is apparent from Eq. 6.83 that the streamlines 1lines of c constant2 are radial lines, and from Eq.<br />

6.82 the equipotential lines 1lines of f constant2 are concentric circles centered at the origin.<br />

E XAMPLE 6.5<br />

Potential Flow—Sink<br />

GIVEN A nonviscous, incompressible <strong>fluid</strong> flows between<br />

wedge-shaped walls into a small opening as shown in Fig. E6.5.<br />

The velocity potential 1in ft 2 s 2, which approximately describes<br />

this flow is<br />

f 2 ln r<br />

y<br />

v r<br />

π_<br />

6<br />

FIND Determine the volume rate of flow 1per unit length2 into<br />

the opening.<br />

r<br />

R<br />

θ<br />

F I G U R E E6.5<br />

x

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