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Titus 2008 - 2009 Product Catalog | www.titus ... - Texas Air Products

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ENGINEERING GUIDELINES<br />

B<br />

B60<br />

TERMINAL CONTROLS AND ACCESSORIES<br />

Engineering Guidelines | Terminals, Controls and Accessories<br />

Some Basic Concepts-Pressure Measurement<br />

Three categories of pressure are<br />

connected with air handling:<br />

1. Static pressure may be thought of<br />

as the pressure in a tire or storage<br />

tank. It is exerted in all directions<br />

equally.<br />

2. Velocity pressure, as its name<br />

implies, is entirely a function of<br />

air velocity and its direction. It is<br />

the pressure you feel against your<br />

hand if you hold it outside the<br />

window of a moving car.<br />

3. Total pressure is the sum of static<br />

pressure and velocity pressure.<br />

It and static pressure are the<br />

pressures actually sampled by<br />

velocity sensors in terminals and<br />

by commonly used measuring<br />

devices, as described next.<br />

The interaction of static, velocity, and<br />

total pressures is illustrated by<br />

(Figure 105). The Pitot tube, which<br />

is used to measure velocities and<br />

pressures, is really a tube within a<br />

tube. The inner, or impact, tube senses<br />

both the velocity pressure and static<br />

pressure combined (total pressure).<br />

The outer tube, which communicates<br />

with the airstream through small holes<br />

in its wall, avoids the impact of the<br />

air movement and senses only static<br />

pressure.<br />

The U-tube manometer, connected to<br />

both parts of the Pitot tube, has the<br />

effect of subtracting static pressure<br />

from total pressure to give a reading of<br />

velocity pressure.<br />

Once the velocity pressure is known,<br />

the velocity can be calculated easily:<br />

where V = <strong>Air</strong> Velocity<br />

P = o<br />

v V p<br />

4005<br />

and<br />

P v = Velocity Pressure<br />

Knowing both the velocity and the<br />

cross-sectional area of the duct, the<br />

flow rate is then:<br />

cfm = Area x Velocity<br />

<strong>Titus</strong> <strong>2008</strong> - <strong>2009</strong> <strong>Product</strong> <strong>Catalog</strong> | <strong>www</strong>.<strong>titus</strong>-hvac.com<br />

2<br />

or V = 4005√P v<br />

P T<br />

P S<br />

P S<br />

Pitot Tube<br />

Connecting<br />

Tubing<br />

P V Difference in Liquid Level<br />

P T minus P S = P V<br />

Glass Manometer Tube<br />

P T<br />

Figure 105. Static, Velocity and Total Pressures Interaction

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