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2.3 Pressure Variation in a Fluid at Rest 45<br />

A 2<br />

F 2 = pA 2<br />

F 1 = pA 1<br />

A 2<br />

A 1<br />

A 1<br />

(a)<br />

F I G U R E 2.5<br />

(a) Hydraulic jack, (b) Transmission of <strong>fluid</strong> pressure.<br />

(b)<br />

If the specific<br />

weight of a <strong>fluid</strong><br />

varies significantly<br />

as we move from<br />

point to point, the<br />

pressure will no<br />

longer vary linearly<br />

with depth.<br />

2.3.2 Compressible Fluid<br />

We normally think of gases such as air, oxygen, and nitrogen as being compressible <strong>fluid</strong>s since<br />

the density of the gas can change significantly with changes in pressure and temperature. Thus, although<br />

Eq. 2.4 applies at a point in a gas, it is necessary to consider the possible variation in g<br />

before the equation can be integrated. However, as was discussed in Chapter 1, the specific weights<br />

of common gases are small when compared with those of liquids. For example, the specific weight<br />

of air at sea level and 60 °F is 0.0763 lbft 3 , whereas the specific weight of water under the same<br />

conditions is 62.4 lbft 3 . Since the specific weights of gases are comparatively small, it follows<br />

from Eq. 2.4 that the pressure gradient in the vertical direction is correspondingly small, and even<br />

over distances of several hundred feet the pressure will remain essentially constant for a gas. This<br />

means we can neglect the effect of elevation changes on the pressure in gases in tanks, pipes, and<br />

so forth in which the distances involved are small.<br />

For those situations in which the variations in heights are large, on the order of thousands of<br />

feet, attention must be given to the variation in the specific weight. As is described in Chapter 1,<br />

the equation of state for an ideal 1or perfect2 gas is<br />

where p is the absolute pressure, R is the gas constant, and T is the absolute temperature. This relationship<br />

can be combined with Eq. 2.4 to give<br />

and by separating variables<br />

p 2<br />

p 1<br />

r p<br />

RT<br />

dp<br />

dz gp RT<br />

dp<br />

p ln p 2<br />

p 1<br />

g R z 2<br />

where g and R are assumed to be constant over the elevation change from z 1 to z 2 . Although the<br />

acceleration of gravity, g, does vary with elevation, the variation is very small 1see Tables C.1 and<br />

C.2 in Appendix C2, and g is usually assumed constant at some average value for the range of elevation<br />

involved.<br />

z 1<br />

dz<br />

T<br />

(2.9)

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