fluid_mechanics
294 Chapter 6 ■ Differential Analysis of Fluid Flow which can be rewritten as tan a 2pc m b tan1u 1 u 2 2 tan u 1 tan u 2 1 tan u 1 tan u 2 (6.92) From Fig. 6.22 it follows that y Source Sink A doublet is formed by letting a source and sink approach one another. x and These results substituted into Eq. 6.92 give so that tan u 1 tan u 2 tan a 2pc m r sin u r cos u a r sin u r cos u a b 2ar sin u r 2 a 2 c m 2ar sin u 2p tan1 a r 2 a b 2 (6.93) The figure in the margin shows typical streamlines for this flow. For small values of the distance a c m 2ar sin u sin u mar 2p r 2 2 a p1r 2 a 2 2 (6.94) since the tangent of an angle approaches the value of the angle for small angles. The so-called doublet is formed by letting the source and sink approach one another 1a S 02 while increasing the strength m 1m S 2 so that the product map remains constant. In this case, since r1r 2 a 2 2 S 1r, Eq. 6.94 reduces to c K sin u r (6.95) where K, a constant equal to map, is called the strength of the doublet. The corresponding velocity potential for the doublet is f K cos u r (6.96) Plots of lines of constant c reveal that the streamlines for a doublet are circles through the origin tangent to the x axis as shown in Fig. 6.23. Just as sources and sinks are not physically realistic entities, neither are doublets. However, the doublet when combined with other basic potential flows y x F I G U R E 6.23 doublet. Streamlines for a
TABLE 6.1 Summary of Basic, Plane Potential Flows 6.6 Superposition of Basic, Plane Potential Flows 295 Description of Velocity Flow Field Velocity Potential Stream Function Components a Uniform flow at angle a with the x axis 1see Fig. 6.16b2 f U1x cos a y sin a2 c U1 y cos a x sin a2 u U cos a v U sin a Source or sink 1see Fig. 6.172 m 7 0 source m 6 0 sink Free vortex 1see Fig. 6.182 7 0 counterclockwise motion 6 0 clockwise motion Doublet 1see Fig. 6.232 f m c m v r m 2p ln r 2p u 2pr f 2p u c 2p ln r v r 0 v u 0 f K cos u r c K sin u r v u 2pr v r K cos u r 2 v u K sin u r 2 a Velocity components are related to the velocity potential and stream function through the relationships: u 0f . 0x 0c v 0f 0y 0y 0c v 0x r 0f 0r 1 0c v r 0u u 1 0f r 0u 0c 0r provides a useful representation of some flow fields of practical interest. For example, we will determine in Section 6.6.3 that the combination of a uniform flow and a doublet can be used to represent the flow around a circular cylinder. Table 6.1 provides a summary of the pertinent equations for the basic, plane potential flows considered in the preceding sections. 6.6 Superposition of Basic, Plane Potential Flows As was discussed in the previous section, potential flows are governed by Laplace’s equation, which is a linear partial differential equation. It therefore follows that the various basic velocity potentials and stream functions can be combined to form new potentials and stream functions. 1Why is this true?2 Whether such combinations yield useful results remains to be seen. It is to be noted that any streamline in an inviscid flow field can be considered as a solid boundary, since the conditions along a solid boundary and a streamline are the same—that is, there is no flow through the boundary or the streamline. Thus, if we can combine some of the basic velocity potentials or stream functions to yield a streamline that corresponds to a particular body shape of interest, that combination can be used to describe in detail the flow around that body. This method of solving some interesting flow problems, commonly called the method of superposition, is illustrated in the following three sections. Flow around a half-body is obtained by the addition of a source to a uniform flow. 6.6.1 Source in a Uniform Stream—Half-Body Consider the superposition of a source and a uniform flow as shown in Fig. 6.24a. The resulting stream function is c c uniform flow c source Ur sin u m 2p u (6.97)
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294 Chapter 6 ■ Differential Analysis of Fluid Flow<br />
which can be rewritten as<br />
tan a 2pc<br />
m b tan1u 1 u 2 2 tan u 1 tan u 2<br />
1 tan u 1 tan u 2<br />
(6.92)<br />
From Fig. 6.22 it follows that<br />
y<br />
Source<br />
Sink<br />
A doublet is formed<br />
by letting a source<br />
and sink approach<br />
one another.<br />
x<br />
and<br />
These results substituted into Eq. 6.92 give<br />
so that<br />
tan u 1 <br />
tan u 2 <br />
tan a 2pc<br />
m<br />
r sin u<br />
r cos u a<br />
r sin u<br />
r cos u a<br />
b 2ar sin u<br />
r<br />
2 a 2<br />
c m 2ar sin u<br />
2p tan1 a<br />
r 2 a b 2<br />
(6.93)<br />
The figure in the margin shows typical streamlines for this flow. For small values of the distance a<br />
c m 2ar sin u sin u<br />
mar<br />
2p r<br />
2 2<br />
a p1r 2 a 2 2<br />
(6.94)<br />
since the tangent of an angle approaches the value of the angle for small angles.<br />
The so-called doublet is formed by letting the source and sink approach one another 1a S 02<br />
while increasing the strength m 1m S 2 so that the product map remains constant. In this case,<br />
since r1r 2 a 2 2 S 1r, Eq. 6.94 reduces to<br />
c K sin u<br />
r<br />
(6.95)<br />
where K, a constant equal to map, is called the strength of the doublet. The corresponding velocity<br />
potential for the doublet is<br />
f K cos u<br />
r<br />
(6.96)<br />
Plots of lines of constant c reveal that the streamlines for a doublet are circles through the origin<br />
tangent to the x axis as shown in Fig. 6.23. Just as sources and sinks are not physically realistic<br />
entities, neither are doublets. However, the doublet when combined with other basic potential flows<br />
y<br />
x<br />
F I G U R E 6.23<br />
doublet.<br />
Streamlines for a