The International Authority on Air System Components

AIR MOVEMENT AND CONTROLASSOCIATION INTERNATIONAL, INC.

ANSI/AMCAStandard 220-05

Laboratory Methods of TestingAir Curtain Units for

Aerodynamic Performance Rating

An American National StandardApproved by ANSI on March 29, 2012

(R2012)

ANSI/AMCA Standard 220-05(R2012)

Laboratory Methods of TestingAir Curtain Units for Aerodynamic Performance Rating

Air Movement and Control Association International30 W. University Drive

Arlington Heights, Illinois60004

AMCA Standard 220 was approved by the AMCA International membership on January 14, 2001 and as an American National Standard by the American National Standards Institute (ANSI) on 7 June 2005. The document was reaffirmed on March 29, 2012.

© 2012 by Air Movement and Control Association International, Inc.

All rights reserved. Reproduction or translation of any part of this work beyond that permitted by Sections 107 and 108 of the United States Copyright Act without the permission of the copyright owner is unlawful. Requests for permission or further information should be addressed to the Executive Director, Air Movement and Control Association International, Inc. at 30 West University Drive, Arlington Heights, IL 60004-1893 U.S.A.

Air Movement and Control Association International, Inc. will consider and decide all written complaints regarding its standards, certification programs, or interpretations thereof. For information on procedures for submitting and handling complaints, write to:

Air Movement and Control Association International30 West University DriveArlington Heights, IL 60004-1893 U.S.A.

AMCA International, Incorporatedc/o Federation of Environmental Trade Associations2 Waltham Court, Milley Lane, Hare HatchReading, Berkshire, United KingdomRG10 9TH

AMCA uses its best efforts to produce standards for the benefit of the industry and the public in light of avail-able information and accepted industry practices. However, AMCA does not guarantee, certify or assure the safety or performance of any products, components or systems tested, designed, installed or operated in accordance with AMCA standards or that any tests conducted under its standards will be non-hazardous or free from risk.

AMCA Publications

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Copyright

Objections

Disclaimer

David Johnson Berner International Corp.Committee Chair

Michael Coscarelli* Berner International Corp.

Frank Cuaderno Mars Sales Co., Inc.

James M. Jagers Alton

Brian K. Jones* Powered Aire, Inc.

Ken Lapinski Powered Aire, Inc.

Dennis Neibrook* Marley Engineered Products

Jack Peters** Loren Cook Co.

Steve Rosol* Mars Sales Co., Inc.

Vincent Vilarchao Marley Engineered Products

Paul Saxon AMCA International Staff

Joe Brooks AMCA International Staff

* Alternate Committee Member

** Corresponding Committee Member

Review Committee

Related AMCA Documents

AMCA Publication 11 Certified Ratings Program - Operating Manual

AMCA Publication 111 Laboratory Accreditation Program

AMCA Publication 211 Certified Ratings Program - Air Performance

ANSI/AMCA Standard 210 Laboratory Methods of Testing Fans for Aerodynamic Performance Rating

RelatedPublications

RelatedStandards

1. Scope . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1

2. Normative References . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1

3. Definitions / Units of Measure / Symbols . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1

3.1 Definitions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1

3.2 System of units . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3

3.3 Symbols and subscripts . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3

4. Instruments and Methods of Measurement . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3

4.1 Air curtain core velocity measurement . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3

4.2 Power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3

5. Equipment and Setups. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5

5.1 Air curtain airflow rate test . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5

5.2 Air velocity projection and outlet air velocity uniformity test . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5

6. Observations and Conduct of Tests . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5

6.1 Initial conditions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5

6.2 Data to be recorded . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5

7. Calculations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6

7.1 Average outlet air velocity . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6

7.2 Outlet air velocity . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6

7.3 Air curtain velocity projection . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6

7.4 Air curtain unit efficiency . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6

8. Report and Results. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7

8.1 Outlet air velocity uniformity test . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7

8.2 Air velocity projection test. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7

Annex A Uncertainty In Velocity Determination Using Pitot-Static Tube and Manometer (Informative) . . . . . . . . . . . 18

Annex B References (Informative) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 19

Contents

AMCA 220-05 (R2012) | 1

Laboratory Methods of TestingAir Curtain Units for Aerodynamic Performance Rating

1. Scope

The scope of this standard covers the performance testing of air curtain units.

The purpose of this standard is to establish uniform meth-ods for laboratory testing of air curtain units to determine aerodynamic performance in terms of airflow rate, outlet air velocity uniformity, power consumption, and air velocity projection, for rating or guarantee purposes.

It is not the purpose of this standard to specify the testing procedures to be used for design, production, or field testing.

2. Normative References

The following standard contains provisions which, through reference in this text, constitute provisions of this standard. At the time of publication, the edition indicated was valid. All standards are subject to revision, and parties to agreements based on this standard are encouraged to investigate the possibility of applying the most recent edition of the stan-dard indicated below.

ANSI/AMCA 210-99 Laboratory Methods of Testing Fans for Aerodynamic Performance Rating Air Movement and Control Association International, Inc., Arlington Heights, IL 60004 U.S.A., 1999.

3. Definitions / Units of Measure / Symbols

3.1 Definitions

3.1.1 Air curtain (airstream)A directionally-controlled airstream, moving across the entire height and width of an opening, which reduces the infiltration or transfer of air from one side of the opening to the other and/or inhibits insects, dust or debris from passing through. For the purposes of this standard, “air curtain” and “airstream” are synonymous.

3.1.2 Air curtain depthThe airstream dimension perpendicular to both the direction of airflow and the airstream width; the short dimension of the airstream.

3.1.3 Air curtain widthThe airstream dimension perpendicular to both the direction of airflow and the airstream depth; the long dimension of the airstream.

3.1.4 Air curtain unit (ACU)An air moving device which produces an air curtain.

3.1.5 Air discharge nozzleA component or an assembly, which may include adjustable vanes, in the ACU which directs and controls the airstream.

3.1.6 Air discharge nozzle depth (Nd)The inside dimension perpendicular to both the direction of airflow and the airstream width.

3.1.7 Air discharge nozzle width (Nw)The inside dimension perpendicular to both the direction of airflow and the nozzle depth.

3.1.8 Air discharge angle (q)The angle between the plane of the protected opening and the direction in which the air curtain leaves the discharge.

3.1.9 Psychrometrics (from ANSI/AMCA 210)

3.1.9.1 Dry-bulb temperature (td)The air temperature measured by a dry temperature sensor.

3.1.9.2 Wet-bulb temperature (tw)The temperature measured by a temperature sensor covered by a water-moistened wick and exposed to air in motion. When properly measured, it is a close approxima-tion of the temperature of adiabatic saturation.

3.1.9.3 Wet-bulb depressionThe difference between the dry-bulb and wet-bulb tempera-tures at the same location.

3.1.9.4 Stagnation (total) temperatureStagnation (total) temperature is the temperature which exists by virtue of the internal and kinetic energy of the air. If the air is at rest, the total temperature will equal the static temperature.

3.1.9.5 Static temperatureStatic temperature is the temperature which exists by virtue of the internal energy of the air only. If a portion of the internal energy is converted into kinetic energy, the static tempera-ture will be decreased accordingly.

3.1.9.6 Air density (ρ)Air density is the mass per unit volume of the air.

3.1.9.7 Standard airAir with a density of 1.2 kg/m3 (0.075 lbm/ft3), a ratio of specific heats of 1.4, a viscosity of 1.8185 × 10-05 Pa·s (1.222

2 | AMCA 220-05 (R2012)

×10-05 lbm/ft·s). Air at 20 °C (68 °F) temperature, 50% rela-tive humidity, and 101.3207 kPa (29.92 in. Hg) barometric pressure has these properties, approximately.

3.1.10 Pressure and head

3.1.10.1 PressureForce per unit area.

3.1.10.2 Absolute pressureThe value of a pressure when the datum pressure is abso-lute zero. It is always positive.

3.1.10.3 Barometric pressure (pb)The absolute pressure exerted by the atmosphere.

3.1.10.4 Gauge pressureThe value of a pressure when the datum pressure is the barometric pressure at the point of measurement. It may be positive or negative.

3.1.10.5 Velocity pressure (Pv)The portion of the air pressure which exists by virtue of the rate of motion only. It is always positive.

3.1.10.6 Static pressureThat portion of the air pressure which exists by virtue of the degree of compression only. If expressed as gauge pres-sure, it may be positive or negative.

3.1.10.7 Total pressureThe air pressure which exists by virtue of the degree of compression and the rate of motion. It is the algebraic sum of the velocity pressure and the static pressure at a point. Thus, if the air is at rest, the total pressure will equal the static pressure.

3.1.10.8 Pressure lossThe decrease in total pressure due to friction and turbulence.

3.1.11 Air curtain unit performance variables

3.1.11.1 Unit airflow rate (volume) (Q)The airflow volume which leaves the discharge nozzle, at standard air conditions, as measured in accordance with ANSI/AMCA 210, and reported in m3/s (cfm).

3.1.11.2 Average outlet air velocity (Va)The airflow rate produced by the air curtain unit divided by the cross sectional area of the discharge nozzle plane at free-air delivery. Refer to Section 7.1 for calculation of the value.

3.1.11.3 Outlet air velocity uniformity (U)An indicator of the consistency of air velocities across the air

curtain width, expressed as a percentage. Refer to Section 7.2.4 for calculation of the value.

3.1.11.4 Air curtain core velocity (Vcx)The maximum air velocity of the air curtain at point X as measured across both the air curtain depth and width at specified distances from the discharge nozzle, per Section 7.2.1.

3.1.11.5 Air curtain average core velocity (Vca)An average of air curtain core velocities measured along the air curtain width, at specified distances per Section 7.2.3.

3.1.11.6 Air curtain velocity projectionA set of average air curtain core velocities measured along the air curtain width at distances specified in Section 6.2.4.4.

3.1.11.7 Power rating of the air curtain unit (W)The amount of energy, expressed in kW, consumed by the drive motor(s) of the air curtain unit at free-air delivery.

3.1.11.8 Air curtain unit efficiency (hac)The ratio of the ACU air power to the power rating of the ACU. This value is based upon total fan efficiency given in ANSI/AMCA 210.

3.1.11.9 Air curtain unit target distanceA distance perpendicular to the discharge nozzle depth in meters (feet), determined by the sponsor of the test, for the purpose of setting up the test.

3.1.11.10 Air powerThe useful power delivered to the air. This is proportional to the product of the ACU airflow rate and total pressure.

3.1.12 Miscellaneous

3.1.12.1 Point of operationThe relative position on the air curtain performance curve corresponding to a particular airflow rate, pressure, power and efficiency.

3.1.12.2 Free-air deliveryFree-air delivery is that point of operation where the air curtain unit operates against zero static pressure.

3.1.12.3 DeterminationA determination is a complete set of measurements for a particular point of operation for the parameter being determined.

3.1.12.4 TestA series of determinations of various characteristics at a single point of operation of an air curtain unit.

AMCA 220-05 (R2012) | 3

3.2 System of units

SI units (The International System of Units - Le Systéme International d’Unités) [1] are the primary units employed in this standard, with I-P units given as the secondary refer-ence. SI units are based on the fundamental values of the International Bureau of Weights and Measures [1], and I-P values are based on the values of the National Institute of Standards and Technology that are, in turn, based upon the values of the International Bureau.

3.2.1 Basic unitsThe unit of length is the meter (m) or millimeter (mm); I-P units are the foot (ft) or inch (in.). The unit of mass is the kilogram (kg); the I-P unit is the pound-mass (lbm). The unit of time is either the minute (min) or the second (s). The unit of temperature is either the Kelvin (K) or the degree Celsius (°C); I-P units are the degree Rankine (°R) or the degree Fahrenheit (°F). The unit of force is the Newton (N); the I-P unit is the pound force (lbf).

3.2.2 Airflow rate and velocityThe unit of airflow rate is the cubic meter per second (m3/s); the I-P unit is the cubic foot per minute (cfm). The unit of velocity is the meter per second (m/s); the I-P unit is the foot per minute (fpm).

3.2.3 PressureThe unit of pressure is either the Pascal (Pa) or the millime-ter of mercury (mm Hg); the I-P unit is either the inch water gauge (in. wg), or the inch mercury column (in. Hg). Values in millimeters of mercury or inches of mercury shall be used only for barometric pressure measurements. The inch water gauge shall be based on a 1 inch column of distilled water at 68 °F under standard gravity and a gas column balancing effect based on standard air. The millimeter of mercury shall be based on a 1 inch column of mercury at 0 °C under stan-dard gravity in vacuo. The inch of mercury shall be based on a 1 inch column of mercury at 32 °F under standard gravity in vacuo.

3.2.4 Power, energy, and torqueThe unit of power is the watt (W); the I-P unit is the horse-power (hp). The unit of energy is the joule (J); the I-P unit is the foot-pound (ft-lb). The unit of torque is the Newton-meter (N·m); the I-P unit is the pound-inch (lb in.).

3.2.5 EfficiencyEfficiency is expressed on a per-unit basis. Percentage values can be obtained by multiplying by 100.

3.2.6 Rotational speedThere is no unit of rotational speed as-such in the SI system of units. The commonly used unit in both systems is the revolution per minute (rpm).

3.2.7 Gas propertiesThe unit of density is the kilogram per cubic meter (kg/m3); the I-P unit is the pound-mass per cubic foot (lbm/ft3). The unit of viscosity is the Pascal second (Pa·s); the I-P unit is the pound-mass per foot-second (lbm/ft·s). The unit of gas constant is the joule per kilogram kelvin (J/kg·K); the I-P unit is the foot-pound per pound-mass degree Rankine (ft·lb/lbm·°R).

3.2.8 Dimensionless groupsVarious dimensionless quantities appear in the text. Any consistent system of units may be employed to evaluate these quantities unless a numerical factor is included, in which case units must be as specified.

3.2.9 Physical constantsThe value of standard gravitational acceleration shall be taken as 9.80665 m/s2 at mean sea level at 45° latitude; the I-P value is 32.1740 ft/s2 at mean sea level at 45° latitude [1]. The density of distilled water at saturation pressure shall be taken as 998.278 kg/m3 at 20 °C; the I-P value is 62.3205 lbm/ft3 68 °F [2]. The density of mercury at saturation pres-sure shall be taken as 13595.1 kg/m3 at 0 °C; the I-P value is 848.714 lbm/ft3 at 32 °F [2]. The specific weights in kg/m3 (lbm/ft3) of these fluids in vacuo under standard grav-ity are numerically equal to their densities at corresponding temperatures.

3.3 Symbols and subscripts

See Table 1.

4. Instruments and Methods of Measurement

Instruments and methods of measurement shall be in compliance with ANSI/AMCA 210 except where specifically noted.

4.1 Air curtain core velocity measurement

Air curtain core velocity shall be measured with a Pitot-static tube and manometer, a hot-wire anemometer, or any other device which has an accuracy of ±5.0% of the air velocity being measured. Refer to Section 6.2 for details.

4.2 Power

Power shall be measured with a wattmeter having a certified accuracy of ± 1% of the observed reading.

4 | AMCA 220-05 (R2012)

Table 1Symbols and Subscripts

Symbol Description SI Unit I-P Unit

An Nozzle cross-sectional area m2 ft2Ha Air power of air curtain unit W hpHm Power input to motor W hpn Number of data points --- ---N Air curtain unit speed rpm rpmhac Air curtain unit efficiency per unit per unitρ Air density kg/m3 lbm/ft3Nd Air discharge nozzle depth mm inchesNw Air discharge nozzle width mm inchespb Barometric pressure Pa in. HgPt Total pressure Pa in. HgPv Velocity pressure Pa in. wgQ Air curtain unit airflow rate m3/s cfms Standard deviation --- ---q Air discharge angle degrees degreestd Dry-bulb temperature °C °Ftw Wet-bulb temperature °C °FU Outlet air velocity uniformity % %Va Velocity, average outlet m/s ft/sVcx Velocity, air curtain core, at point X m/s fpmVca Velocity, average (air curtain core) m/s fpmW Power rating of the ACU Watt Watt

AMCA 220-05 (R2012) | 5

5. Equipment and Setups

5.1 Air curtain airflow rate test

The air curtain unit shall be mounted with its inlet sealed to the test chamber in compliance with the requirements of Figure 1A. The seal shall be adequate enough to minimize leakage. The air discharge nozzle or adjustable vanes in the air discharge nozzle shall be set so as to provide a 15° ± 1° angle as shown in Figure 1B.

5.2 Air velocity projection and outlet air velocity uniformity test

The air curtain unit shall be placed in the testing area in compliance with the requirements of Figure 2 so that the inlet and outlet are unrestricted and the air curtain width is perpendicular to the floor. The air discharge nozzle or adjust-able vanes in the air discharge nozzle shall be set so as to provide a 15° ± 1° air discharge angle as shown in Detail A or B of Figure 1B. Units without an adjustable air discharge nozzle are not required to be angled and shall be mounted so that nothing interferes with the airstream for 3000 mm (120 in.).

6. Observations and Conduct of Tests

6.1 Initial conditions

The unit under test shall be energized and operated for not less than one minute to allow equilibrium conditions to become established before the first determination.

6.2 Data to be recorded

6.2.1 ACU Under testThe following information shall be recorded: Manufacturer, trade name, model number, impeller diameter, inlet and outlet areas, number of fans, number of motors and the motor nameplate data.

6.2.2 Test setupThe description of the test setup shall be recorded, including specific dimensions as required per Figures 1, 2, 3 and 4. Alternately, an annotated photograph of the setup shall be attached to the recorded data.

6.2.3 InstrumentsThe instruments and apparatus used in the test shall be listed. Names, model numbers, serial numbers, scale ranges, and calibration information shall be recorded.

6.2.4 Test data

6.2.4.1 Initial and final conditionsInitial and final readings of: ambient dry-bulb temperature (td), ambient wet-bulb temperature (tw), and ambient barometric pressure (pb) shall be recorded for each determination.

6.2.4.2 Airflow rate determinationTo establish the airflow rate at free-air delivery, a curve containing a minimum of three determinations is required per ANSI/AMCA 210. See Figures 1A and 1B. One determi-nation with the unit working against a pressure of 50 Pa (0.2 in. wg), one determination against a pressure of 25 Pa (0.1 in. wg) and one determination against a pressure of 2.5 Pa (0.01 in. wg) or less.

6.2.4.3 Outlet air velocity uniformity testThe outlet air velocity uniformity test shall be based on air curtain core velocity measurements taken on a minimum of five equally spaced test lines on Plane 1 located one air discharge nozzle depth away from, and parallel to, the air discharge nozzle width. The test line locations at the two ends of the plane shall be one air discharge nozzle depth in from each end as shown in Figure 3. The remaining test line locations shall be equally spaced and each space shall not exceed 100 mm (4 in.). Record the maximum air curtain core velocity readings along each test line within the plane.

6.2.4.4 Air curtain velocity projection test

General: The air velocity projection test shall be based on air curtain core velocity measurements taken on a minimum of three planes parallel to the plane of the air discharge nozzle as shown in Figure 4. The air curtain core velocities shall be recorded on a minimum of five equally spaced test lines across each plane. The test line locations at the two ends of each plane shall be located one air discharge nozzle depth in from each end as shown in Figure 4. The remaining test line locations shall be equally spaced and each space shall not exceed 100 mm (4 in.). Record the maximum air curtain air core velocity reading along the test lines within each plane. The sponsor of the test shall determine the number of test planes by specifying an ACU Target Distance, a minimum average air curtain core velocity, or both.

For ACU Target Distance Specified:The ACU Target Distance shall be a minimum of 1000 mm (40 in.), or whole multiples thereof.

For an ACU Target Distance greater than or equal to 3000 mm (120 in.), the air curtain core velocities shall be measured at Plane 2 [1000 mm (40 in.)], Plane 3 [2000 mm (80 in.)], and Plane 4 [3000 mm (120 in.)]. Additional

6 | AMCA 220-05 (R2012)

readings shall be taken at consecutively numbered planes located at 1000 mm (40 inch) intervals until the ACU Target Distance is reached.

For an ACU Target Distance of 2000 mm (80 in.), the air curtain core velocity shall be measured at Plane 2 [1000 mm (40 in.)], Plane 2A [1500 mm (60 in.)], and Plane 3 [2000 mm (80 in.)].

For an ACU Target Distance of 1000 mm (40 inches), the air curtain core velocity shall be measured at Plane 1A [500 mm (20 in.)], Plane 2 [1000 mm (40 in.)], and Plane 2A [1500 mm (60 in.)].

For Minimum Air Curtain Core Velocity Specified:The test shall be terminated upon measurement and calcu-lation of a value less than or equal to the specified minimum average air curtain core velocity.

The first reading shall be taken at Plane 2 [1000 mm (40 in.)]. If the reading is less than the minimum specified aver-age core velocity, readings shall be taken at Plane 1A [500 mm (20 in.)] and Plane 1 located Nd from the air discharge nozzle plane (See Figure 3) and the test concluded.

If the first reading is greater than the minimum specified average core velocity, the second reading shall be taken at Plane 3 [2000 mm (80 in.)]. If the second reading is less than the minimum specified average core velocity, the third reading shall be taken at Plane 2A [1500 mm (60 in.)] and the test concluded.

If the second reading is greater than the minimum speci-fied average core velocity, the third reading shall be taken at Plane 4 [3000 mm (120 in.)]. If the third reading is still greater than the minimum specified average core velocity, additional readings shall be taken at 1000 mm (40 in.) intervals until the minimum core velocity is attained.

7. Calculations

Calculations, except as noted below, shall be in compliance with the requirements of Section 9, ANSI/AMCA 210.

7.1 Average outlet air velocity

The average outlet air velocity shall be the unit airflow rate divided by the cross-sectional area of the discharge nozzle plane or:

Va = Q/An Eq. 7.1

7.2 Outlet air velocity

7.2.1 Air curtain core velocity (Vcx)The maximum air velocities of the airstream shall be obtained by traversing each test line x, as shown in Figure 3, and recording each maximum reading using instrumentation per Section 4.1. If velocity pressure is measured via Pitot-static tube or other velocity pressure measuring device, use Equation 7.2.1 to calculate Vcx:

VP

cxv=

2r Eq. 7.2.1 (SI)

VP

cxv= 1097r Eq. 7.2.1 (I-P)

7.2.2 Standard deviation (s)

s

VVn

n=

−

−

∑∑( )cxcx2

2

1 Eq. 7.2.2

Where n = number of test points 7.2.3 Average air curtain core velocity (Vca)

VV

ncacx=

( )∑ Eq. 7.2.3

7.2.4 Outlet air velocity uniformity (U)The outlet air velocity uniformity of the ACU shall be expressed as a percentage calculated from the average air curtain core velocity Vca and standard deviation s of Plane 1, Figure 3, using:

U sVca

ca= −

100 100 % Eq. 7.2.4

7.3 Air curtain velocity projection

The air curtain velocity projection shall be the average air curtain core velocities Vca, determined using Equation 7.2.3, for a set of test planes defined in Section 6.2.4.4.

7.4 Air curtain unit efficiency

7.4.1 Air power of air curtainThe air power of an ACU is calculated using the values Pt

AMCA 220-05 (R2012) | 7

and Q from an airflow rate test conducted per ANSI/AMCA 210.

Ha = PtQ Eq 7.4.1 (SI)

HPQ

at=

6362 Eq 7.4.1 (I-P)

7.4.2 Power input to motorThe power input to the motor is determined from the value of W corresponding to the value of Q used in Section 7.4.1.

Hm = W Eq 7.4.2 (SI)

H Wm =

745 7. Eq 7.4.2 (I-P)

7.4.3 Air curtain unit efficiency

haca

m

HH

= Eq 7.4.3

8. Report and Results

The test report shall be presented in consistent units. The following information shall be reported: Manufacturer, trade name, model number, impeller diameter, inlet and outlet areas, number of fans, number of motors and the motor nameplate data. The ACU airflow rate shall be presented graphically as shown in Figures 5A or 5B.

In addition, the report shall be in compliance with ANSI/AMCA 210, except as noted in Sections 8.1 and 8.2.

8.1 Outlet air velocity uniformity test

The locations and the results of the measurements shall be presented in a table with the calculated arithmetic average of the measured results, their standard deviation and unifor-mity, as shown in Figures 6A and 6B.

8.2 Air velocity projection test

The locations and the results of the measurements shall be presented in a table, and a performance curve meeting the requirements of ANSI/AMCA 210, with the calculated arith-metic average of the measured results, their standard devia-tion, and uniformity for each distance from the air discharge nozzle, as shown in Figures 6A and 6B and Figures 7A and 7B.

8 | AMCA 220-05 (R2012)

Figure 1AAirflow Rate Test Setup

Formulae:Airflow and pressure measurements to be made in accordance with Section 6 of this standard and calculations per ANSI/AMCA 210.

Notes:1. Unit can be mounted horizontally or vertically.2. If an ACU has multiple inlets, it shall be mounted so that all of the inlets are contained within the testing chamber.3. Air discharge nozzle angle setup as per Figure 1B.

AMCA 220-05 (R2012) | 9

Figure 1BAir Discharge Nozzle Angle Setup

Definitions:In determining Θ, the orientation of the ACU shall be established by the ACU’s normal application mounting position. The direc-tion of Θ is then defined as a 15° ± 1° angle away from the environment that the ACU is protecting or towards that which would normally be considered the outside.

Units without an adjustable air discharge nozzle are not required to be angled and shall be mounted so that nothing interferes with the airstream for 3000 mm (120 in.).

Notes:1. The examples above are not intended to represent every possible ACU mounting application, they are only to serve as

examples of how the direction of Θ shall be determined.2. For example, the nozzle setup of an ACU designed for outdoor application (not shown), shall be determined by the defini-

tion and the guidelines illustrated in the examples above. Following these criteria yields the direction of Θ to be the same as that shown in Example #2 (opposite that shown in Detail A and Detail B).

10 | AMCA 220-05 (R2012)

Figure 2Outlet Air Velocity Uniformity and Air Velocity Projection Test Setup

SIDEELEVATION

FRONTELEVATION

ROOM WALLS ROOM WALLS

MINIMUM 3000 mm1220 mm

MAXTARGET DISTANCE

TOP BAFFLE50 mm MAXACUd

AIRFLOW

50 mm MAXACU INLET

ACU AIRDISCHARGE

NOZZLE

LNwc

≥A ≥A ≥A

≥A≥A

ACUNd

c

Formulae:1. A = 2 Equivalent ACU Inlet Diameters

A cd= 4 *

p

* For ACU’s without a rectangular inlet, substitute the actual value of the inlet area for cd in equation. * For ACU’s with multiple inlets, substitute the sum of all inlet areas for cd in equation.

Notes:1. See Figures 3 & 4 for test plane locations.2. Air discharge nozzle angle setup as per Figure 1B.3. Center baffle(s) over center line of airflow.4. Nd = Air Discharge Nozzle Depth.5. Nw = Air Discharge Nozzle Width.6. If an ACU has multiple inlets, the nearest surface to each inlet (including the floor) shall be equal to the A value of that inlet.

If an ACU must be suspended above the floor, a bottom baffle identical to the top baffle must be used.

AMCA 220-05 (R2012) | 11

Figure 3Outlet Air Velocity Uniformity Test Setup

Formulae: 1. Cd = Test line spacing (See note 4)

C Gnd 100 mm (4 in.)=−≤

1

2. Vca = Average Air Curtain Core Velocity

VV

ncacx=

( )∑

3. s = Standard Deviation

s

VVn

n=

−

−

∑∑( )cxcx2

2

1

Notes:1. Air Curtain Unit setup as per Figure 2.2. Air discharge nozzle angle setup as per Figure 1B.3. n = number of test lines (x) (5 minimum).4. Calculated test line spacing (Cd) shall be less than or equal to 100 mm (4 in.) and rounded to the nearest multiple of 5 mm (1/4 in.).5. Nd = Air Discharge Nozzle Depth6. Nw = Air Discharge Nozzle Width7. Vcx = core (peak) air velocity along test line x

12 | AMCA 220-05 (R2012)

Figure 4Air Velocity Projection Test Setup

Formulae:1.) Cd = Internal test line spacing (See note 4)

C Gnd 100 mm (4 in.)=−≤

1

2.) Vca = Average Air Curtain Core Velocity

VV

ncacx=

( )∑

3.) s = Standard Deviation

s

VVn

n=

−

−

∑∑( )cxcx2

2

1

Notes:1. Air Curtain Unit setup as per Figure 2.2. Air discharge nozzle angle setup as per Figure 1B.3. n = number of test lines (x) (5 minimum).4. Calculated test line spacing (Cd) shall be less than or

equal to 100 mm (4 in.) and rounded to the nearest multiple of 5 mm (1/4 in.).

5. Plane locations shall be accurate to ± 25 mm (1 in.).6. Additional planes shall be spaced every 1000 mm (40

in.).7. Nd = Air Discharge Nozzle Depth8. Nw = Air Discharge Nozzle Width9. Vcx = core (peak) air velocity along test line x

AMCA 220-05 (R2012) | 13

Figure 5ATypical Air Curtain Unit Airflow Rate Performance Curve (SI)

890

860

870

880

FAN

SP

EE

D (R

PM

)

PO

WE

R IN

PU

T (k

W)

EFF

ICIE

NC

Y (p

er u

nit)

Sta

tic P

ress

ure

(Pa)

Airflow Rate (m3/s)

0.7

0.8

0.9

0

0.1

0.2

0.3

50

12.5

37.5

25

1.40 1.45 1.50 1.55 1.60

ACU MODEL: ___________________________________

ND: _______________ mm NW: _________________ mm

FREE DELIVERY CONDITIONS:

Airflow Rate: ________________________________ m3/s

Average Velocity: __________ m/s

Input Watts: __________

TEST NUMBER: _________________________

LABORATORY: _________________________

LOCATIONS: _________________________

ANSI/AMCA 220 Figure: 1

ANSI/AMCA 210 Inlet Chamber Figure: __________

Air Density: ___________ kg/m3

Efficiency: ___________ %

CURVE BY: __________________

DATE: __________________

14 | AMCA 220-05 (R2012)

Figure 5BTypical Air Curtain Unit Airflow Rate Performance Curve (I-P)

890

860

870

880

FAN

SP

EE

D (R

PM

)

PO

WE

R IN

PU

T (k

W)

EFF

ICIE

NC

Y (p

er u

nit)

Sta

tic P

ress

ure

(in. w

g)

Airflow Rate (CFM)

0.2

0.15

0.1

0.05

3000 3100 3200 3300 34000.7

0.8

0.9

0

0.1

0.2

0.3

ACU MODEL: ___________________________________

ND: _______________ in. NW: _________________ in.

FREE DELIVERY CONDITIONS:

Airflow Rate: ________________________________ cfm

Average Velocity: __________ fpm

Input Watts: __________

TEST NUMBER: _________________________

LABORATORY: _________________________

LOCATIONS: _________________________

ANSI/AMCA 220 Figure: 1

ANSI/AMCA 210 Inlet Chamber Figure: __________

Air Density: ___________ lbm/ft3

Efficiency: ___________ %

CURVE BY: __________________

DATE: __________________

AMCA 220-05 (R2012) | 15

Figure 6ASample Outlet Air Velocity Uniformity and Air Velocity Projection Calculations (SI)

16 | AMCA 220-05 (R2012)

Figure 6BSample Outlet Air Velocity Uniformity and Air Velocity Projection Calculations (I-P)

AMCA 220-05 (R2012) | 17

Plane Distance From ACU (mm)

20

18

16

14

12

10

8

6

4

2

0100 200 300 400

Aver

age

Cor

e Ve

loci

ty (V

ca) (

m/s

)

18.45

8.057.13

5.76

Figure 7ASample Air Velocity Projection Test (SI)

Figure 7BSample Air Velocity Projection Test (I-P)

Plane Distance From ACU (inches)

4000

3500

3000

2500

2000

1500

1000

500

0 4 40 80 120

Aver

age

Cor

e Ve

loci

ty (V

ca) (

fpm

)

3626

15821401

1131

18 | AMCA 220-05 (R2012)

Annex AUncertainty In Velocity Determination Using Pitot-Static Tube and Manometer (Informative)

Table of 5 Percent Uncertainty

Values given are based on an error equivalent to an indicating column lengthof 12 Pa (0.05 in. wg) in a vertical manometer having a 1:1 slope ratio.

Slope Ratio Minimum Usable Velocity

1:1 14 m/s (2800 fpm)2:1 10 m/s (2000 fpm)5:1 6 m/s (1250 fpm)10:1 5 m/s (900 fpm)20:1 3 m/s (630 fpm)

Source: David Johnson, Berner International Corporation, 1998

AMCA 220-05 (R2012) | 19

Annex BReferences (Informative)

[1] Page, C.H. and Vigoreaux, P. The International System of Units (SI) National Institute for Standards and Technology NBS Special Publication 330, 1972 Gaithersburg, MD, U.S.A. AMCA #1140

[2] ASME Steam Tables 1967, p.283 American Society of Mechanical Engineers New York, NY, U.S.A. AMCA #2312

AIR MOVEMENT AND CONTROLASSOCIATION INTERNATIONAL, INC.

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The Air Movement and control Association International, Inc. is a not-for-profit international association of the world’s manufacturers of related air system equipment primarily, but limited to: fans, louvers, dampers, air curtains, airflow measurement stations, acoustic attenuators, and other air system components for the industrial, commercial and residential markets.