This manual is periodically altered to incorporate new or updated information. The date revision level
of each page is indicated at the bottom of the page opposite the page number. A major change in the
content of the manual also changes the date of the manual, which appears on the front cover. Listed
below is the date revision level of each page.
Page Revision
All Pages Mar/05
All Pages May/97
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This product may be covered under pending patent applications.
While this information is presented in good faith and believed to be accurate, Fisher Controls does not guarantee
satisfactory results from reliance upon such information. Nothing contained herein is to be construed as a warranty or
guarantee, express or implied, regarding the performance, merchantability, fitness or any other matter with respect to the
products, nor as a recommendation to use any product or process in conflict with any patent. Fisher Controls reserves the
right, without notice, to alter or improve the designs or specifications of the products described herein.
This manual discusses gas flow measurement based on philosophies expressed in AGA (American
Gas Association) and API (American Petroleum Institute) guidelines.
NOTE: AGA and API do not certify manufacturers’ equipment for flow measurement. Products
of The Flow Computer Division of Emerson Process Management are in compliance with AGA and
API guidelines.
The American Gas Association (AGA) has published various reports describing how to measure the
flow of natural gas, starting with AGA Report No. 1, issued in 1930, describing the measurement of
natural gas through an orifice meter. This report was revised in 1935 with the publication of AGA
Report No. 2 and again in 1955 with the publication of AGA Report No. 3. The report was revised
again in 1969, 1978, 1985, and 1992, but has remained AGA Report No. 3 -- Orifice Metering of
Natural Gas and Other Related Hydrocarbons. Thus, AGA3 has become synonymous with orifice
metering.
In 1975, the American Petroleum Institute (API) adopted AGA Report No. 3 and approved it as API
Standard 2530 and also published it as Chapter 14.3 of the API Manual of Petroleum Measurement
Standards. In 1977, the American National Standards Institute (ANSI) also approved AGA Report No.
3 and referred to it as ANSI/API 2530. Thus references to API 2530, Chapter 14.3 and ANSI/API 2530
are identical to AGA Report No. 3. In 1980 (revised in 1984 and in 1996), AGA Report No. 7-Measurement of Fuel Gas by Turbine Meters--was published, detailing the measurement of natural gas
through a turbine meter.
While AGA No. 3 and AGA No. 7 detail methods of calculating gas flow, separate documents have
been created to explain the calculation of the compressibility factor, used in both AGA No. 3 and AGA
No. 7. The older method, called NX-19, was last published in 1963. A more comprehensive method
was published in 1985 as AGA Report No. 8. This report was revised in 1992.
In 1992, the API released Chapter 21, Section 1, which addressed the application of electronic flow
meters in gas measurement systems. It addresses the calculation frequency and the method of executing
the AGA calculations.
1-1 Introduction Rev Mar/05
Flow Manual
SECTION 2 – NATURAL GAS MEASUREMENT
2.1 AGA Report No. 7 - Measurement of Gas by Turbine Meters
2.1.1 General Description
AGA No. 7 covers the measurement of gas by turbine meters and is limited to axial-flow turbine
meters. Although the report covers meter construction, installation, and other aspects of metering,
this Flow Manual summarizes only the equations used in calculating flow.
The meter construction and installation sections are specific to axial-flow turbine meters, but the
flow equations are applicable to any linear meter, including ultrasonic and vortex meters.
2.1.2 Introduction
The turbine meter is a velocity measuring device. It consists of three basic components:
• The body
• The measuring mechanism
• The output and readout device
It relies upon the flow of gas to cause the meter rotor to turn at a speed proportional to the flow rate.
Ideally, the rotational speed is proportional to the flow rate. In actuality, the speed is a function of
passage-way size, shape, rotor design, internal mechanical friction, fluid drag, external loading, and
gas density.
Several characteristics that affect the performance of a turbine meter are presented in Section 5 of
AGA No. 7. Here is a summary of these characteristics:
Swirl Effect - Turbine meters are designed and calibrated under conditions approaching axial
flow. If the flowing gas has substantial swirl near the rotor inlet, depending on the direction,
the rotor can either increase or decrease in velocity. Buyer or seller can lose.
Velocity Profile Effect - If poor installation practices result in a non-uniform velocity profile
across the meter inlet, the rotor speed for a given flow rate will be affected. Typically, this
results in higher rotor velocities. Thus, less gas passes through the meter than the calculated
value represents. Buyer loses.
Fluid Drag Effect - Fluid drag on the rotor blades, blade tips and rotor hub can cause the
rotor to slip from its ideal speed. This rotor slip is known to be a function of a dimensionless
ratio of inertia to viscous forces. This ratio is the well known Reynolds number and the fluid
drag effect has become known as the “Reynolds number effect.” Basically, it slows the rotor
down, thus the Buyer wins.
Non-Fluid Drag Effect - Also decreasing rotor speed from its ideal speed are forces created
from non-fluid related forces, such as bearing friction and mechanical or electrical readout
2-1 Natural Gas Measurement Rev Mar/05
Flow Manual
drag. The amount of slip is a function of flow rate and density. Also know as “the density
effect.” It also benefits the buyer.
Accuracy - Accuracy statements are typically provided within ± 1% for a designated range.
Linearity - Turbine meters are usually linear over some designated flow range. Linear
means that the output frequency is proportional to flow.
Pressure Loss - Pressure loss is attributed to the energy required to drive the meter.
Minimum and Maximum Flow Rates - Turbine meters will have designated minimum flow
rates for specific conditions.
Pulsation - Error due to pulsation generally creates an error causing the rotor to spin faster,
thus resulting in errors that favor the seller. A peak-to-peak flow variation of 10% of the
average flow generally will result in a pulsation error of less than 0.25% and can be
considered as the pulsation threshold.
2.1.3 Basic Gas Law Relationship
The basic gas law relationships are presented similarly in the 1985 and 1996 versions of
AGA No. 7. The equation numbers shown here are from the 1996 version. The relationships
are:
))()()(())((
TRNZVP=For Flowing Conditions[AGA Equation 12]
ffff
and
TRNZVP= For Base Conditions [AGA Equation 13]
))()()(())((
bbbb
where: P = Absolute pressure
V = Volume
Z = Compressibility
N = Number of moles of gas
T = Absolute temperature
R = Universal gas constant
subscript
subscript
= Flowing conditions (use with P, V, and Z)
f
= Base conditions (use with P, V, and Z)
b
Since R is a constant for the gas regardless of pressure and temperature, and for the same number of
moles of gas N, the two equations can be combined to yield:
⎛
⎞
⎛
P
⎛
⎞
T
f
b
⎜
⎜
=
VV
2-2 Natural Gas Measurement Rev Mar/05
⎟
fb
⎜
⎟
⎜
T
P
⎝
f
b
⎠
⎝
⎞
Z
b
⎟
⎜
⎟
⎟
⎠
[AGA Equation 14]
⎜
⎟
Z
f
⎝
⎠
Flow Manual
2.1.4 Difference Between the 1985 and 1996 Versions
The difference between the versions as it applies to the flow calculations, is that the 1985 flow
equations included factors, such as
factor. In the 1996 version, the correction factors have been combined into multipliers. For example,
the pressure factors,
F
and Fb have been combined into the pressure multiplier, Pf /P
pm
F
, the measured pressure factor, and FPb, the base pressure
pm
b
P
1985:
P =
f
P
and
s
m
1996: Pressure Multiplier =
P =
b
P
s
P
b
PP • =
bm
P
f
P
b
2.1.5 AGA No. 7 – 1985 Version
2.1.5.1 The Flow Equation
Rotor revolutions are counted mechanically or electrically and converted to a continuously
totalized volumetric registration. Because the registered volume is at flowing pressure and
temperature conditions, it must be corrected to the specified base conditions for billing
purposes.
2.1.5.2 General Form of the Flow Equation and a Term-by-Term
Explanation
Q
Flow rate at base conditions (cubic feet per hour)
b
QQFFFFs
=[AGA Equation 15]
()( )( )
bfpmpbtmtb
()()
()
where: Qb = Volumetric flow rate at base conditions
Q
F
F
F
F
= Volumetric flow rate at flowing conditions
f
= Pressure factor
pm
= Pressure base factor
pb
= Flowing temperature factor
tm
= Temperature base factor
tb
s = Compressibility ratio factor
Qf Flow Rate at Flowing Conditions (Cubic Feet per Hour)
V
Q
where Q
V
= Flow rate at flowing conditions
f
= Volume timed at flowing conditions
f
f
=[AGA Equation 14]
f
t
= Counter differences on mechanical output
2-3 Natural Gas Measurement Rev Mar/05
Flow Manual
= Total pulses ×
1
on electrical output
K
t = Time
K = Pulses per cubic foot
F
where p
P
p
Where p
Fpb Pressure Base Factor
Pressure Factor
pm
= Pf + pa
f
f
= Atmospheric pressure, psia
a
is the contract base pressure in psia.
b
p
F
pm
f
=[AGA Equation 16]
73.14
= Static gauge pressure, psig
14 73.
F
=
pb
[AGA Equation 18]
p
b
This factor is applied to change the base pressure from 14.73 psia to another contract
pressure base.
F
Flowing Temperature Factor
tm
520
F
=
tm
[AGA Equation 19]
T
f
Where Tf = actual flowing temperature of the gas in degrees Rankine. °R = ° F +
459.76
F
°
Temperature Base Factor
tb
T
F
b
=
tb
[AGA Equation 20]
520
Where Tb = the contract base temperature in degrees Rankine.
This factor is applied to change the assumed temperature base of 60 deg F to the actual
contract base temperature.
s Compressibility Factor Ratio
Z
b
s
=[AGA Equation 21]
Z
f
where Zb = Compressibility factor at base conditions
Z
2-4 Natural Gas Measurement Rev Mar/05
= Compressibility factor at flowing conditions
f
Flow Manual
The compressibility ratio “s” can be evaluated from the supercompressibility factor “Fpv”,
which is defined as:
s = (F
2
)
pv
where FZZ
The calculation of the supercompressibility factor F
=
pvbf
is given in AGA Report NX-19 or
pv
AGA No. 8. For more information, refer to Section 3.
2.1.6 AGA No. 7 – 1996 Version
2.1.6.1 The Flow Equation
Rotor revolutions are counted mechanically or electrically and converted to a continuously
totalized volumetric registration. Since the registered volume is at flowing pressure and
temperature conditions, it must be corrected to the specified base conditions for billing
purposes.
2.1.6.2 General Form of the Volumetric Flow Equation
Qb Flow rate at flowing conditions
V
f
=[AGA Equation 15]
f
t
where Q
Q
= Flow rate at flowing conditions
f
V
= Volume timed at flowing conditions
f
= Counter differences on mechanical output
= Total pulses ×
1
×METER FACTOR on electrical pulse output
K
t = Time
K = K-Factor, pulses per cubic foot
METER FACTOR is a dimensionless term obtained by dividing the actual volume of gas
passed through the meter (as measured by a prover during proving) by the corresponding
meter indicated volume. For subsequent metering operations, actual measured volume is
determined by multiplying the indicated volume registered by the meter times the METER
FACTOR.
Qb Flow rate at base conditions (cubic feet per hour)
⎛
⎞
⎛
P
⎛
⎜
()
=
QQ
fb
⎜
P
⎝
⎞
T
f
b
⎜
⎟
⎟
⎜
T
f
b
⎠
⎝
⎞
Z
b
⎟
⎜
⎟
⎟
⎜
⎠
⎝
[AGA Equation 16]
⎟
Z
f
⎠
where: Qb = Volumetric flow rate at base conditions
Q
= Volumetric flow rate at flowing conditions
f
2-5 Natural Gas Measurement Rev Mar/05
Flow Manual
The P, T, and Z quotients in the above equation are the pressure multiplier, temperature
multiplier, and the compressibility multipliers, respectively. They are defined below.
Pressure Multiplier
Multiplierpressure=
where: Pf = pf + pa , in psia
P
f
[AGA Equation 17]
P
b
p
P
P
= Static gauge pressure, in psig
f
= Atmospheric pressure, in psia
a
= Base pressure, in psia
b
Temperature Multiplier
T
b
MultipliereTemperatur=
[AGA Equation 18]
T
f
where: Tb = Base temperature, °R
T
Absolute Flowing Temperature,
= Flowing temperature, °R
f
°R = ° F + 459.76°
Compressibility Multiplier
Z
b
MultiplierilityCompressib=
[AGA Equation 19]
Z
f
where: Zb = Compressibility at base conditions
Z
= Compressibility at flowing conditions
f
The compressibility multiplier can be evaluated from the supercompressibility factor, F
as follows:
pv
Z
b
=[AGA Equation 20]
Z
f
2
)(
F
pv
Where natural gas mixtures are being measured, compressibility values may be determined from the
latest edition of AGA Transmission Measurement Committee Report No. 8 “Compressibility Factors
of Natural Gas and Other Related Hydrocarbon Gases” or as specified in contracts or tariffs or as
mutually agreed to by both parties. For more information, refer to Section 3.
2-6 Natural Gas Measurement Rev Mar/05
Flow Manual
2.2 AGA Report No. 3 – Orifice Metering of Natural Gas
2.2.1 General Description
AGA Report No. 3 is an application guide for orifice metering of natural gas and other related
hydrocarbon fluids. This Flow Manual summarizes some of the equations used in calculating flow
and is based on part 3 of the report.
2.2.2 Differences Between 1985 and 1992 Versions of AGA No. 3
AGA No. 3 – 1992 version was developed for flange-tap orifice meters only. The pipe tap
methodology of the 1985 version is included as an appendix in the 1992 standard. This appendix is
identical to the 1985 version with the exception of F
implemented per the body of the 1992 standard. For F
AGA No. 8 to calculate compressibility. The new version is based on the calculation of a discharge
coefficient. The Reynolds number is a function of flow. It must be determined iteratively. In addition,
the orifice diameter and pipe diameter are both corrected for temperature variations from the
temperature at which they were measured. This requires additional parameters for the measured
temperature of the pipe and the orifice material.
, Ftb, Ftf, Fgr, and Fpr. These factors are to be
pb
, this indicates using the most recent version of
pr
The empirical coefficient of discharge has received much emphasis in the creation of the 1992
report. It is a function of the Reynolds Number, sensing tap location, pipe diameter and the beta
ratio. An expanded Regression data base consisting of data taken from 4 fluids (oil, water, natural
gas, air) from different sources, 11 different laboratories, on 12 different meter tubes of differing
origins and more than 100 orifice plates of different origins. This data provided a pipe Reynolds
Number range of accepted turbulent flow from 4,000 to 36,000,000 on which to best select the
mathematical model. Flange, corner, and radius taps; 2, 3, 4, 6, and 10 inch pipe diameters; and beta
ratios of 0.1, 0.2, 0.375, 0.5, 0.575, 0.660, and 0.750 were all tested.
Technical experts from the US, Europe, Canada, Norway and Japan worked together to develop an
equation using the Stolz linkage form that fits this expanded Regression Data Base more accurately
than any previously published equations. The empirical data associated with this data base is the
highest quality and largest quantity available today. This is perhaps the greatest improvement over
the 1985 equations. This mathematical model for the Coefficient of Discharge is applicable and most
accurately follows the Regression data base for nominal pipe sizes of 2 inches and larger, beta ratios
of 0.1 to 0.75 (provided that the orifice plate bore diameter is greater than 0.45 inch), and pipe
Reynolds number greater than or equal to 4000.
Concentricity tolerances have been tightened from the 1985 statement of 3%. The 1992 uses an
equation to calculate the maximum allowed eccentricity. Eccentricity has a major effect on the
accuracy of the coefficient of discharge calculations.
AGA No. 3 – 1992 version calls for the use of AGA No. 8 for the calculation of the
supercompressibility factor. As no specific version is specified, this implies using the most recently
released version, NX-19 or AGA No. 8 - 1985 version should not be used with the new version.
Unlike the 1985 report, the AGA No. 3 - 1992 report was divided into four parts:
• Part 1 - General Equations and Uncertainty Guidelines
2-7 Natural Gas Measurement Rev Mar/05
Flow Manual
• Part 2 - Specifications and Installation Requirements
• Part 3 - Natural Gas Applications
• Part 4 - Background, Development, Implementation Procedure, and Subroutine Documentation
for Empirical Flange Tapped Discharge Coefficient Equation
Part 3 provides an application guide along with practical guidelines for applying AGA Report No. 3,
Parts 1 and 2, to the measurement of natural gas. Mass flow rate and base (or standard) volumetric
rate methods are presented in conformance with North American industry practices.
2.2.3 AGA No. 3 – 1985 Version
The orifice meter is essentially a mass flow meter. It is based on the concepts of conservation of
mass and energy. The orifice mass flow equation is the basis for volumetric flow rate calculations
under actual conditions as well as at standard conditions. Once mass flow rate is calculated, it can
be converted into volumetric flow rate at base (standard) conditions if the fluid density at base
conditions can be determined or is specified.
AGA Report No. 3 defined measurement for orifice meters with circular orifices located
concentrically in the meter tube having upstream and downstream pressure taps. Pressure taps must
be either flange taps or pipe taps and must conform to guidelines found in the AGA 3 report.
This standard applies to natural gas, natural gas liquids, and associated hydrocarbon gases and
liquids. It was not intended for non-hydrocarbon gas or liquid streams.
2.2.3.1 Topics Worthy of Mention
Concentricity - When centering the orifice plates, the orifice must be concentric with the inside
of the meter tube to within 3% of the inside diameters. This is more critical in small tubes,
tubes with large beta ratios, and when the orifice is offset towards the taps.
Beta Ratio Limitations - Beta ratio, the ratio of the orifice to meter tube for flange taps, is
limited to the range of 0.15 to 0.7. For pipe taps, it should be limited to 0.2 to 0.67.
Pulsation Flow - Reliable measurements of gas flow cannot be obtained with an orifice meter
when appreciable pulsations are present at the place of measurement. No satisfactory
adjustment for flow pulsation has ever been found. Sources of pulsation include:
1.
Reciprocating compressors, engines or impeller type boosters
2.
Pumping or improperly sized regulators
3.
Irregular movement of water or condensates in the line
4.
Intermitters on wells and automatic drips
5.
Dead-ended piping tee junctions and similar cavities.
2.2.3.2 General Form of the Flow Equation
2-8 Natural Gas Measurement Rev Mar/05
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