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Eclipse Engineering Guide

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Sharp Edge<br />

C d = 0.60<br />

The flow of air or gas through an orifice can be determined<br />

by the formula<br />

h<br />

Q = 1658.5 x Ax C g d<br />

where Q =flow, cfh<br />

A =area of the orifice, sq. in. (see Pages 57 & 58)<br />

Cd =discharge coefficient of the orifice<br />

(see above)<br />

h =pressure drop across the orifice,″ w.c.<br />

g =specific gravity of the gas, based on standard<br />

air at 1.0 (see Pages 19, 20, & 22 thru 24.)<br />

1. Sizing Orifice Plates<br />

To calculate the size of an orifice plate, this equation can<br />

be rearranged as follows:<br />

A= Q x<br />

g<br />

1658.5 x C h<br />

d<br />

2. Effect of Changes in Operating Conditions on<br />

Flow through an Orifice – General Relationship<br />

Q2 A2 Cd2 h2 g1 = x x x<br />

Q1 A1 Cd1 h g 1 2<br />

If any of the factors in this relationship remain constant<br />

from Condition 1 to Condition 2, they can be dropped out of<br />

the equation, yielding these simplified relationships. Each of<br />

them assumes only one factor has been changed.<br />

2a.Flow Change vs. Orifice Area Change<br />

Q2 A2 =<br />

Q1 A1 2b.Flow Change vs. Pressure Drop Change<br />

Q2 h2 =<br />

Q 1<br />

Reentrant<br />

0.72<br />

h 1<br />

This is the so-called “square root law.”<br />

2c.Flow Change vs. Specific Gravity Change<br />

Q2 g1 =<br />

Q g 1 2<br />

CHAPTER 1 – ORIFICES & FLOWS<br />

COEFFICIENTS OF DISCHARGE FOR VARIOUS TYPES OF ORIFICES<br />

Round Edge<br />

0.97<br />

Short Pipe<br />

0.82<br />

Converging<br />

depends on angle. See<br />

curve at right.<br />

Coefficient of Discharge (Cd )<br />

0.95<br />

4<br />

0.93<br />

0.91<br />

0.89<br />

0.87<br />

0.85<br />

ORIFICE FLOW FORMULAS<br />

3.Effect of Changes in Operating Conditions on Pressure<br />

Drop Across an Orifice–General Relationship:<br />

2 h2 Q2 = x A1 2<br />

x Cd1 2<br />

x g2 ( h1 Q ) ( ) ( )<br />

1 A2 Cd2 g1 Again, if any of the factors in this equation are unchanged<br />

from Condition 1 to Condtion 2, they can be dropped out to<br />

form simplified relationships:<br />

3a.Pressure Drop Change vs. Flow Change<br />

2 h2 Q2 =<br />

h 1<br />

Q 1<br />

This is the square root law, stated another way.<br />

3b.Pressure Drop Change vs. Orifice Area Change<br />

2 h2 A1 =<br />

h 1<br />

A 2<br />

3c.Pressure Drop Change vs. Specific Gravity Change<br />

h2 g2 =<br />

h 1<br />

Orifices and Nozzles Discharging from Plenum<br />

0.83<br />

0 2 4 6 8 10 12 14 16 18 20 22 24<br />

Angle of Convergence in Degrees<br />

(<br />

(<br />

g 1<br />

)<br />

)<br />

This relationship may not apply where specific gravity has<br />

been changed by a change in gas temperature. See Page 25.<br />

4. Effect of Changes in Gas Temperature on Flow and<br />

Pressure Drop through an Orifice<br />

Raising a gas’s temperature has two effects – it increases<br />

the volume and decreases the specific gravity, both in proportion<br />

to the ratio of the absolute temperatures. If we are concerned<br />

with changes in mass flows (scfh), these relationships<br />

must be used:<br />

4a.Flow Change vs. Temperature Change<br />

Q2 Q1 =<br />

TADS1 TABB2 4b.Pressure Drop Change vs. Temperature Change<br />

h2 TABS2 h<br />

=<br />

1 TABS1 to maintain constant scfh<br />

NOTE: The loss is least at 13˚

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