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2.8 Hydrostatic Force on a Plane Surface 57<br />

Diaphragm<br />

(a)<br />

Case<br />

Diaphragm<br />

stop<br />

Electrical connections<br />

Armature<br />

Diaphragm<br />

Link pin<br />

Beam (strain gages deposited on beam)<br />

(b)<br />

F I G U R E 2.15 (a) Two different sized strain-gage pressure transducers<br />

(Spectramed Models P10EZ and P23XL) commonly used to measure physiological<br />

pressures. Plastic domes are filled with <strong>fluid</strong> and connected to blood vessels through a<br />

needle or catheter. (Photograph courtesy of Spectramed, Inc.) (b) Schematic diagram of<br />

the P23XL transducer with the dome removed. Deflection of the diaphragm due to<br />

pressure is measured with a silicon beam on which strain gages and an associated<br />

bridge circuit have been deposited.<br />

2.8 Hydrostatic Force on a Plane Surface<br />

V2.4 Hoover dam<br />

When a surface is submerged in a <strong>fluid</strong>, forces develop on the surface due to the <strong>fluid</strong>. The determination<br />

of these forces is important in the design of storage tanks, ships, dams, and other hydraulic<br />

structures. For <strong>fluid</strong>s at rest we know that the force must be perpendicular to the surface<br />

since there are no shearing stresses present. We also know that the pressure will vary linearly with<br />

depth as shown in Fig. 2.16 if the <strong>fluid</strong> is incompressible. For a horizontal surface, such as the bottom<br />

of a liquid-filled tank 1Fig. 2.16a2, the magnitude of the resultant force is simply F R pA,<br />

where p is the uniform pressure on the bottom and A is the area of the bottom. For the open tank<br />

shown, p gh. Note that if atmospheric pressure acts on both sides of the bottom, as is illustrated,<br />

the resultant force on the bottom is simply due to the liquid in the tank. Since the pressure is constant<br />

and uniformly distributed over the bottom, the resultant force acts through the centroid of the<br />

area as shown in Fig. 2.16a. As shown in Fig. 2.16b, the pressure on the ends of the tank is not<br />

uniformly distributed. Determination of the resultant force for situations such as this is presented<br />

below.

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