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Dwyer 172 User Manual

Page 2

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AIR VELOCITY

The total pressure of an air stream flowing in a duct is the sum of the static

or bursting pressure exerted upon the sidewalls of the duct and the impact

or velocity pressure of the moving air. Through the use of a pitot tube

connected differentially to a manometer, the velocity pressure alone is

indicated and the corresponding air velocity determined.

For accuracy of plus or minus 2%, as in laboratory applications, extreme

care is required and the following precautions should be observed:

In making an air velocity check, select a location as suggested above,

connect tubing leads from both pitot tube connections to the manometer

and insert in the duct with the tip directed into the air stream. If the

manometer shows a minus indication reverse the tubes. With a direct

reading manometer, air velocities will now be shown in feet per minute. In

other types, the manometer will read velocity pressure in inches of water

and the corresponding velocity will be found from the curves in Bulletin H-

11. If circumstances do not permit an accurate traverse, center the pitot

tube in the duct, determine the center velocity and multiply by a factor of

.9 for the approximate average velocity. Field tests run in this manner

should be accurate within plus or minus 5%.

The velocity indicated is for dry air at 70°F (21.3°C), 29.9˝ Barometric

Pressure and a resulting density of .075=/cu. ft. For air at a temperature

other than 70°F, refer to the curves in Bulletin H-11. For other variations

from these conditions, corrections may be based upon the following data:

Air Velocity=1096.7 Pv

D

where Pv=velocity pressure in inches of water

D=Air density in lbs/cu. ft.

Air Density=1.325 x P

B

T

where P

B

= Barometric Pressure in inches of mercury

T = Absolute Temperature (indicated temperature plus 460)

Flow in cu. ft. per min. = Duct area in square feet x air velocity in ft.

per minute.

STATIC PRESSURE

In checking inlet and discharge fan and blower pressures, balancing

ventilation and dust collection systems, checking exhaust systems and

similar installations, air velocities above 700 ft. per min. (12.81 kms/hr)

can cause an appreciable error. It is recommended that the static

connection of the pitot tube or a static pressure tip be used. In using the

static pressure tip or pitot tube, the tip should be directed into the air

stream. For permanent installation, static pressure tips are recommended.

If not available, make connections, enter the duct perpendicular to the air

stream and finish off flush and smooth on the inside.

FURNACE DRAFT

Connect the terminal tube to the minus pressure gage opening and insert

it into the combustion chamber for over fire draft reading. If a drilled port

is not available insert through fire door but seal the crack. For last pass or

smoke pipe draft, connect into the breeching on the furnace side of any

draft control or damper. To determine draft loss through the furnace, make

connection as indicated for smoke pipe draft and add a second tube,

connecting the manometer differentially to the combustion chamber.

AIR FILTER TEST

To determine the pressure drop across an air filter, connect the

manometer differentially with one tubing from the downstream or blower

side of the filter to the right hand or minus pressure gage connection. Run

the second tubing from the upstream side of the filter to the other gage

connection. Use static pressure tips if available, with the tips directed into

the air stream, to eliminate possibility of error due to air velocity. Read the

pressure drop across the filter in inches of water and follow the filter

manufacturer’s recommendations for filter cleaning or replacement.

FR# 36-440380-00 Rev. 3

1. Duct diameter 4˝ (8.64 mm) or

greater.

2. Make an accurate traverse per

sketch at right and average the

readings.

3. Provide smooth, straight duct

sections 10 diameters in length

both upstream and downstream

from the pitot tube.

4. Provide an egg crate type

straightener upstream from

the pitot tube.

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