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

6.44 The velocity potential<br />

f k1x 2 y 2 2 1k constant2<br />

may be used to represent the flow against an infinite plane boundary,<br />

as illustrated in Fig. P6.44. For flow in the vicinity of a stagnation<br />

point, it is frequently assumed that the pressure gradient along<br />

the surface is of the form<br />

0p<br />

0x Ax<br />

where A is a constant. Use the given velocity potential to show that<br />

this is true.<br />

y<br />

6.47 It is suggested that the velocity potential for the incompressible,<br />

nonviscous, two-dimensional flow along the wall shown in<br />

Fig. P6.47 is<br />

f r 4 3 cos 4 3 u<br />

Is this a suitable velocity potential for flow along the wall? Explain.<br />

3 π/4<br />

θ<br />

r<br />

F I G U R E P6.47<br />

x<br />

F I G U R E P6.44<br />

6.45 Water is flowing between wedge-shaped walls into a small<br />

opening as shown in Fig. P6.45. The velocity potential with units<br />

m 2 s for this flow is f 2 ln r with r in meters. Determine the<br />

pressure differential between points A and B.<br />

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

6.48 Obtain a photograph/image of a situation which approximates<br />

one of the basic, plane potential flows. Print this photo and<br />

write a brief paragraph that describes the situation involved.<br />

6.49 As illustrated in Fig. P6.49, a tornado can be approximated<br />

by a free vortex of strength for r 7 R c , where R c is the radius of<br />

the core. Velocity measurements at points A and B indicate that<br />

V A 125 fts and V B 60 fts. Determine the distance from point<br />

A to the center of the tornado. Why can the free vortex model not be<br />

used to approximate the tornado throughout the flow field 1r 02?<br />

y<br />

r<br />

__ π<br />

6<br />

r<br />

A<br />

θ<br />

B<br />

R c<br />

A<br />

B<br />

x<br />

0.5 m 1.0 m<br />

F I G U R E P6.45<br />

100 ft<br />

6.46 An ideal <strong>fluid</strong> flows between the inclined walls of a twodimensional<br />

channel into a sink located at the origin 1Fig. P6.462.<br />

The velocity potential for this flow field is<br />

where m is a constant. (a) Determine the corresponding stream<br />

function. Note that the value of the stream function along the wall<br />

OA is zero. (b) Determine the equation of the streamline passing<br />

through the point B, located at x 1, y 4.<br />

ψ = 0<br />

f m 2p ln r<br />

A<br />

y<br />

F I G U R E P6.49<br />

6.50 If the velocity field is given by V axî ay ĵ, and a is a constant,<br />

find the circulation around the closed curve shown in Fig. P6.50.<br />

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

y<br />

B (1, 4)<br />

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

O<br />

r<br />

θ<br />

π__<br />

3<br />

F I G U R E P6.46<br />

x<br />

x<br />

F I G U R E P6.50<br />

6.51 The streamlines in a particular two-dimensional flow field are<br />

all concentric circles, as shown in Fig. P6.51. The velocity is given by<br />

the equation v u vr where v is the angular velocity of the rotating<br />

mass of <strong>fluid</strong>. Determine the circulation around the path ABCD.

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