Dwyer Instruments 160S series Скачать руководство пользователя страница 1

Series 160S Pitot Tubes

are designed to meet the need

of the environmental testing field for an inexpensive, yet
accurate and reliable way to measure the flow of particu-
late-laden air or gas streams. These pitot tubes use large
5/16˝ diameter stainless steel tubing for both total and stat-
ic pressures to avoid plugging. Versatile 1/8˝ female NPT
connections enable  use with  any type of piping or tubing.
Two barbed  tubing adapters are included for use with 3/16˝
I.D. rubber or vinyl tubing.

This instrument was built to allow measurement of flows by
the procedures detailed in U.S. Environmental Protection
Agency publication 40 CFR Change 1, Application A,
Method 2. For complete information, refer to that publica-
tion and the procedures contained within. 

INTRODUCTION

The 

total pressure

of a flowing air stream in a duct or pipe

is the sum of  the 

static

or bursting pressure exerted on the

sidewalls and the 

velocity

or impact pressure of the mov-

ing air.  The difference between 

total

and 

static

pressure is

called 

velocity pressure

, which can be used to determine

the linear rate of air movement expressed in FPM (feet per
minute). A pitot tube has two tubes arranged to sense both
pressures simultaneously. By connecting these two tubes
differentially to a manometer, 

velocity pressure

is indicat-

ed directly and the corresponding air velocity can be calcu-
lated after applying the appropriate correction factor.
For maximum accuracy of ±2%, as in laboratory applica-
tions, care is required and the following recommendations 
should be followed.

1.   Duct diameter should  be 4˝ or larger.
2.   Point 

total pressure

opening upstream facing flow 

and 

static pressure

opening downstream pointing in 

the direction of the flow. The faces of both openings 
must be perpendicular to the airflow.

3.   Make an accurate traverse per drawings; calculate the

the velocities at each point and average them. 

4.   Take readings in a smooth, straight duct section a

minimum of 8

2

duct diameters in length upstream

and 1

2

diameters downstream from the pitot tube. 

5.   Provide an egg-crate type straightener upstream from

the pitot tube.  

Series 160S “S” Type Pitot Tubes

Operating Instructions

Bulletin H-12

DWYER INSTRUMENTS, INC. 

Phone: 219/879-8000

www.dwyer-inst.com

P.O. BOX 373 • MICHIGAN CITY, INDIANA 46361, U.S.A. 

Fax: 219/872-9057

e-mail: [email protected]

TAKING AIR VELOCITY READINGS

To measure air velocity with a Series 160S Pitot Tube, make
a 13/16˝ (20 mm) opening in side of duct. Permanent-
mount models require a 1˝ female NPT opening. Note: per-
manent mounting is not recommended with insertion
lengths over 24˝ (61 cm) due to risk of excessive deflection.
Connect tubing from total pressure port to high pressure
side of manometer and from static pressure port to the low
pressure side. If reading is negative, reverse connections.

Make a series of readings traversing the duct in horizontal
and vertical planes. Using velocity pressures recorded at
each location, calculate velocities and average them for 
final velocity value. If circumstances do not permit or
require an accurate traverse, center the pitot tube in the
duct, determine the pressure differential (velocity pressure),
calculate actual center velocity, and multiply this value by
0.9. Tests run in this manner should be accurate within 
±5%.

CALCULATING VELOCITY

Air Velocity

= 1096.2 (Cp)       Pv

D

where:

Pv  = Sensed pressure difference (velocity 

pressure) in inches of water column 

D   =  Air density in lbs./ft.

3

(dry air = .075) 

Cp =  Pitot tube coefficient: 0.84 

Air Density

= 1.325   X   P

B

T

P

B

=  Barometric pressure in inches of 

mercury

T

=  Absolute Temperature (Indicated 

Temperature in °F plus 460)

Flow in cubic feet per minute equals duct cross sectional
area in square feet x air velocity in feet per minute.

With dry air at 29.9 inches of mercury, air velocity can 
be read directly from temperature correction charts on
reverse.

H-12rev  9/18/03  4:18 PM  Page 1

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