fluid_mechanics
292 Chapter 6 ■ Differential Analysis of Fluid Flow Arbitrary curve C ds V F I G U R E 6.20 The notation for determining circulation around closed curve C. A mathematical concept commonly associated with vortex motion is that of circulation. The circulation, , is defined as the line integral of the tangential component of the velocity taken around a closed curve in the flow field. In equation form, can be expressed as ≠ ˇ C V ds (6.89) where the integral sign means that the integration is taken around a closed curve, C, in the counterclockwise direction, and ds is a differential length along the curve as is illustrated in Fig. 6.20. For an irrotational flow, V f so that V ds f ds df and, therefore, ≠ ˇ C df 0 This result indicates that for an irrotational flow the circulation will generally be zero. (Chapter 9 has further discussion of circulation in real flows.) However, if there are singularities enclosed within the curve the circulation may not be zero. For example, for the free vortex with u Kr the circulation around the circular path of radius r shown in Fig. 6.21 is The numerical value of the circulation may depend on the particular closed path considered. V6.4 Vortex in a beaker which shows that the circulation is nonzero and the constant K 2p. However, for irrotational flows the circulation around any path that does not include a singular point will be zero. This can be easily confirmed for the closed path ABCD of Fig. 6.21 by evaluating the circulation around that path. The velocity potential and stream function for the free vortex are commonly expressed in terms of the circulation as and ≠ 2p 0 v K 1r du2 2pK r f 2p u c 2p ln r (6.90) (6.91) The concept of circulation is often useful when evaluating the forces developed on bodies immersed in moving fluids. This application will be considered in Section 6.6.3. v θ ds B C D A dθ θ r F I G U R E 6.21 in a free vortex. Circulation around various paths
6.5 Some Basic, Plane Potential Flows 293 E XAMPLE 6.6 Potential Flow—Free Vortex GIVEN A liquid drains from a large tank through a small opening as illustrated in Fig. E6.6a. A vortex forms whose velocity distribution away from the tank opening can be approximated as that of a free vortex having a velocity potential f 2p u FIND Determine an expression relating the surface shape to the strength of the vortex as specified by the circulation . SOLUTION Since the free vortex represents an irrotational flow field, the Bernoulli equation p 1 g V 2 1 2g z 1 p 2 g V 2 2 2g z 2 can be written between any two points. If the points are selected at the free surface, p 1 p 2 0, so that V 2 1 2g z s V 2 2 2g where the free surface elevation, z s , is measured relative to a datum passing through point 112 as shown in Fig. E6.6b. The velocity is given by the equation v u 1 0f r 0u 2pr We note that far from the origin at point 112, V 1 v u 0 so that Eq. 1 becomes z s 8p 2 r 2 g which is the desired equation for the surface profile. 2 (1) (Ans) F I G U R E E6.6a p = p atm F I G U R E E6.6b x z (2) z s y COMMENT The negative sign indicates that the surface falls as the origin is approached as shown in Fig. E6.6. This solution is not valid very near the origin since the predicted velocity becomes excessively large as the origin is approached. r (1) A doublet is formed by an appropriate source–sink pair. 6.5.4 Doublet The final, basic potential flow to be considered is one that is formed by combining a source and sink in a special way. Consider the equal strength, source–sink pair of Fig. 6.22. The combined stream function for the pair is c m 2p 1u 1 u 2 2 y P r 2 r r 1 Source a θ 2 θ 1 θ a Sink x F I G U R E 6.22 The combination of a source and sink of equal strength located along the x axis.
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6.5 Some Basic, Plane Potential Flows 293<br />
E XAMPLE 6.6<br />
Potential Flow—Free Vortex<br />
GIVEN A liquid drains from a large tank through a small<br />
opening as illustrated in Fig. E6.6a. A vortex forms whose velocity<br />
distribution away from the tank opening can be approximated<br />
as that of a free vortex having a velocity potential<br />
f <br />
2p u<br />
FIND Determine an expression relating the surface shape to<br />
the strength of the vortex as specified by the circulation .<br />
SOLUTION<br />
Since the free vortex represents an irrotational flow field, the<br />
Bernoulli equation<br />
p 1<br />
g V 2 1<br />
2g z 1 p 2<br />
g V 2 2<br />
2g z 2<br />
can be written between any two points. If the points are selected<br />
at the free surface, p 1 p 2 0, so that<br />
V 2 1<br />
2g z s V 2 2<br />
2g<br />
where the free surface elevation, z s , is measured relative to a datum<br />
passing through point 112 as shown in Fig. E6.6b.<br />
The velocity is given by the equation<br />
v u 1 0f<br />
r 0u <br />
2pr<br />
We note that far from the origin at point 112, V 1 v u 0 so that<br />
Eq. 1 becomes<br />
z s <br />
8p 2 r 2 g<br />
which is the desired equation for the surface profile.<br />
2<br />
(1)<br />
(Ans)<br />
F I G U R E E6.6a<br />
p = p atm<br />
F I G U R E E6.6b<br />
x<br />
z<br />
(2)<br />
z s<br />
y<br />
COMMENT The negative sign indicates that the surface falls<br />
as the origin is approached as shown in Fig. E6.6. This solution is<br />
not valid very near the origin since the predicted velocity becomes<br />
excessively large as the origin is approached.<br />
r<br />
(1)<br />
A doublet is formed<br />
by an appropriate<br />
source–sink pair.<br />
6.5.4 Doublet<br />
The final, basic potential flow to be considered is one that is formed by combining a source and<br />
sink in a special way. Consider the equal strength, source–sink pair of Fig. 6.22. The combined<br />
stream function for the pair is<br />
c m 2p 1u 1 u 2 2<br />
y<br />
P<br />
r 2<br />
r<br />
r 1<br />
Source<br />
a<br />
θ 2<br />
θ 1<br />
θ<br />
a<br />
Sink<br />
x<br />
F I G U R E 6.22 The combination of<br />
a source and sink of equal strength located along<br />
the x axis.