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

Section 6.6 Superposition of Basic, Plane<br />

Potential Flows<br />

6.59 Obtain a photograph/image of a situation that mimics the superposition<br />

of potential flows (see Ex. 6.7). Print this photo and<br />

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

6.60 Potential flow against a flat plate 1Fig. P6.60a2 can be described<br />

with the stream function<br />

c Axy<br />

where A is a constant. This type of flow is commonly called a “stagnation<br />

point” flow since it can be used to describe the flow in the<br />

vicinity of the stagnation point at O. By adding a source of strength<br />

m at O, stagnation point flow against a flat plate with a “bump” is obtained<br />

as illustrated in Fig. P6.60b. Determine the relationship between<br />

the bump height, h, the constant, A, and the source strength, m.<br />

6.63 One end of a pond has a shoreline that resembles a half-body<br />

as shown in Fig. P6.63. A vertical porous pipe is located near the<br />

end of the pond so that water can be pumped out. When water is<br />

pumped at the rate of 0.08 m 3 s through a 3-m-long pipe, what will<br />

be the velocity at point A? Hint: Consider the flow inside a halfbody.<br />

(See Video V6.5.)<br />

Pipe<br />

A<br />

y<br />

5 m<br />

15 m<br />

F I G U R E P6.63<br />

(a)<br />

y<br />

O<br />

x<br />

6.64 Two free vortices of equal strength, but opposite direction<br />

of rotation, are superimposed with a uniform flow as shown in<br />

Fig. P6.64. The stream functions for these two vorticies are<br />

c 3;12p24 ln r. (a) Develop an equation for the x-component<br />

of velocity, u, at point P1x,y2 in terms of Cartesian coordinates x<br />

and y. (b) Compute the x-component of velocity at point A and<br />

show that it depends on the ratio H.<br />

U<br />

y<br />

P(x, y)<br />

H<br />

h<br />

x<br />

A<br />

H<br />

x<br />

Source<br />

(b)<br />

F I G U R E P6.60<br />

6.61 The combination of a uniform flow and a source can be used<br />

to describe flow around a streamlined body called a half-body. (See<br />

Video V6.5.) Assume that a certain body has the shape of a halfbody<br />

with a thickness of 0.5 m. If this body is placed in an airstream<br />

moving at 15 m/s, what source strength is required to simulate flow<br />

around the body?<br />

6.62 A vehicle windshield is to be shaped as a portion of a halfbody<br />

with the dimensions shown in Fig. P6.62. (a) Make a scale<br />

drawing of the windshield shape. (b) For a free stream velocity of<br />

55 mph, determine the velocity of the air at points A and B.<br />

y<br />

B<br />

Windshield<br />

r<br />

1.5 ft<br />

U = 55 mph<br />

θ<br />

x<br />

A 2.0 ft<br />

F I G U R E P6.62<br />

F I G U R E P6.64<br />

6.65 A Rankine oval is formed by combining a source–sink pair,<br />

each having a strength of 36 ft 2 s and separated by a distance of 12 ft<br />

along the x axis, with a uniform velocity of 10 fts 1in the positive x direction2.<br />

Determine the length and thickness of the oval.<br />

*6.66 Make use of Eqs. 6.107 and 6.109 to construct a table showing<br />

how /a, ha, and /h for Rankine ovals depend on the parameter<br />

pUam. Plot /h versus pUam and describe how this plot could<br />

be used to obtain the required values of m and a for a Rankine oval<br />

having a specific value of / and h when placed in a uniform <strong>fluid</strong><br />

stream of velocity, U.<br />

6.67 An ideal <strong>fluid</strong> flows past an infinitely long, semicircular<br />

“hump” located along a plane boundary, as shown in Fig. P6.67.<br />

Far from the hump the velocity field is uniform, and the pressure is<br />

p 0 . (a) Determine expressions for the maximum and minimum values<br />

of the pressure along the hump, and indicate where these points<br />

are located. Express your answer in terms of r, U, and p 0 . (b) If<br />

the solid surface is the c 0 streamline, determine the equation of<br />

the streamline passing through the point u p2, r 2a.

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