EPA Method 1 Sample & Velocity Traverses

EPA Reference Method

Method 1
Sample & Velocity Traverses

Complete interactive guide for determining the number and location of sampling points in stationary source stacks and ducts — with built-in calculators for every equation.

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Scope & Applicability

EPA Method 1 is titled "Sample and Velocity Traverses for Stationary Sources." It provides the procedure for determining the number of sampling or velocity measurement points and their location across a stack or duct cross-section.

The method applies to all EPA reference methods (Methods 2 through 8 and beyond) that require measuring gas velocity, extracting a gas sample, or both. Every test that uses a pitot tube, a sampling probe, or any other measurement device inserted into a stack depends on Method 1 to define where those measurements must be taken.

Key Point Method 1 does NOT measure anything by itself. It tells you HOW to set up the measurement grid. The actual velocity measurement is done by Method 2, and actual sampling by Methods 3–8.

The method covers two duct geometries:

  1. Circular (round) stacks and ducts — uses the log-linear rule to place points along two perpendicular diameters.
  2. Rectangular ducts — uses the log-Tchebycheff rule to distribute points across the cross-section grid.

The goal is always the same: ensure the set of measurement points is statistically representative of the entire gas flow so that the final calculated velocity and emission rate are accurate.

Important The sampling site must be selected to avoid cyclonic flow, reverse flow, or highly asymmetric velocity profiles. Method 1 requires the measurement location to be at least 8 stack diameters downstream and 2 stack diameters upstream of any flow disturbance (bend, fan, expansion, contraction). If this is not possible, additional traverse points may be required.
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Principle & Summary

The velocity profile in a duct is NOT uniform — it is higher near the center and lower near the walls due to friction and boundary layer effects. If you measure velocity at only one point, you get a wrong answer. Method 1 solves this by creating a traverse: a pattern of points that, when averaged, reproduces the true mean velocity.

How it works for circular ducts:

  1. Measure the stack inner diameter (D).
  2. Determine the minimum number of traverse points from a lookup table based on D.
  3. Place points along two diameters at distances specified by the log-linear rule (as fractions of D from the wall).
  4. Measure velocity or extract sample at each point.
  5. Compute the arithmetic average of all point values.

How it works for rectangular ducts:

  1. Measure duct width (W) and height (H) to compute area A = W × H.
  2. Determine minimum number of points from a lookup table based on A.
  3. Distribute points in a grid using the log-Tchebycheff rule for fractional positions.
  4. Measure and average as above.
Why Log-Linear? The log-linear weighting accounts for the shape of the turbulent velocity profile in fully developed pipe flow. It gives more weight to regions where the velocity gradient is steeper (near the wall) and less weight to the relatively flat center region. This produces a more accurate average than equal spacing.
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Circular Duct — Number of Traverse Points

For a circular stack, the minimum number of traverse points depends on the inside diameter D. The total number of points is always 2 × n, where n is the number of points per diameter. Points are placed on two perpendicular diameters.

Stack Diameter (ft) Min. Points per Diameter (n) Total Points (2n)
0.12 – 0.2536
> 0.25 – 0.5048
> 0.50 – 1.0510
> 1.0 – 2.0612
> 2.0 – 4.0714
> 4.0 – 8.0816
> 8.0918
Note If the diameter is measured in inches, convert to feet first: D(ft) = D(in) / 12. If measured in meters, convert: D(ft) = D(m) × 3.28084.
Calculator: Find Number of Traverse Points
Enter value in inches
Result
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Log-Linear Rule — Point Locations

Once you know how many points per diameter (n), the log-linear rule gives the fractional distance from the inside wall for each point. These fractions are multiplied by the radius (R = D/2) to get the actual insertion depth from each wall.

The points are arranged symmetrically: if the fractional distance from one wall is p, the corresponding point on the opposite side is at (1 − p) from that wall.

Points per Diameter (n) Fractional Distances from Wall (pi)
30.0594, 0.2500, 0.7500
40.0359, 0.1942, 0.6458, 0.8058
50.0257, 0.1463, 0.5000, 0.8537, 0.9743
60.0200, 0.1175, 0.4063, 0.5937, 0.8825, 0.9800
70.0163, 0.0983, 0.3404, 0.5000, 0.6596, 0.9017, 0.9837
80.0138, 0.0846, 0.2935, 0.4372, 0.5628, 0.7065, 0.9154, 0.9862
90.0119, 0.0746, 0.2590, 0.3866, 0.5000, 0.6134, 0.7410, 0.9254, 0.9881
Insertion Depth from Wall
di = pi × R = pi × (D / 2)
di
= insertion depth from wall for point i
pi
= fractional distance from wall (from table above)
R
= stack inside radius
D
= stack inside diameter
Calculator: Compute Point Locations (Log-Linear)
Same unit for all output depths
Point Locations (Depth from Wall)
Interactive cross-section showing traverse point layout
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Rectangular Duct — Number of Traverse Points

For rectangular ducts, the minimum number of points is based on the cross-sectional area. Points are distributed in a grid pattern.

Duct Area (ft²) Minimum Total Points
< 49
4 – 1212
> 12 – 2516
> 25 – 3620
> 36 – 4924
> 49 – 6430
> 6436

The total points must be arranged in a grid as close to square as possible. For example, 12 points could be arranged as 4 × 3 or 3 × 4.

Calculator: Rectangular Duct Traverse Points
Feet
Feet
Result
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Log-Tchebycheff Rule — Rectangular Point Positions

For rectangular ducts, point positions along each axis are determined by the log-Tchebycheff rule. The fractional positions depend on the number of measurement lines along that axis.

Lines per Axis Fractional Positions from Wall
30.136, 0.500, 0.864
40.097, 0.394, 0.606, 0.903
50.076, 0.321, 0.500, 0.679, 0.924
60.063, 0.270, 0.440, 0.560, 0.730, 0.937
70.054, 0.235, 0.390, 0.500, 0.610, 0.765, 0.946
80.047, 0.209, 0.351, 0.452, 0.548, 0.649, 0.791, 0.953
90.042, 0.189, 0.321, 0.413, 0.500, 0.587, 0.679, 0.811, 0.958
Position Along Axis
xi = ti × W   |   yj = tj × H
ti, tj
= fractional positions from log-Tchebycheff table
W
= duct width
H
= duct height
Calculator: Log-Tchebycheff Grid Positions
Feet
Feet
Grid Coordinates (from corner)
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Cross-Sectional Area Calculation

The cross-sectional area is needed to convert average velocity to volumetric flow rate. It is calculated differently for circular and rectangular ducts.

Circular Duct Area
A = π × (D / 2)² = π × D² / 4
A
= cross-sectional area
D
= inside diameter
π
= 3.14159265
Rectangular Duct Area
A = W × H
W
= duct width
H
= duct height
Calculator: Cross-Sectional Area
Inches
Cross-Sectional Area
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Pitot Tube Velocity Equation

The standard (Type S) pitot tube measures the velocity pressure (ΔP), which is the difference between total pressure and static pressure. This is converted to gas velocity using the following equation from EPA Method 2 (which relies on Method 1 for point placement).

Stack Gas Velocity
vs = Kp × Cp × √(ΔP × Ts / (Ms × Ps))
vs
= stack gas velocity (ft/s or m/s)
Kp
= pitot tube coefficient (typically 0.84 for standard Type S)
Cp
= 85.49 (for ft/s) or 34.97 (for m/s)
ΔP
= velocity pressure (in. H2O)
Ts
= absolute stack gas temperature (°R or °K)
Ms
= molecular weight of stack gas (lb/lb-mole)
Ps
= absolute stack gas pressure (atm)
Unit Consistency If using ft/s: Ts in °R = °F + 460, Ps in atm. If using m/s: Ts in °K = °C + 273, Ps in atm. Do NOT mix unit systems.
Calculator: Pitot Tube Velocity
in. H₂O
°F (for ft/s)
lb/lb-mole
atm
Stack Gas Velocity
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Gas Density Calculation

The dry gas density is needed for several emission calculations. It can be derived from the ideal gas law using molecular weight, temperature, and pressure.

Dry Gas Density
ρd = Md × Ps / (R × Ts)
ρd
= dry gas density (lb/ft³ or kg/m³)
Md
= dry molecular weight (lb/lb-mole or kg/kg-mole)
Ps
= absolute pressure (atm)
R
= 0.7302 (for lb, ft³, atm, °R) or 0.08206 (for g, L, atm, °K)
Ts
= absolute temperature (°R or °K)
Wet Gas Density
ρw = Ms × Ps / (R × Ts)
Ms
= wet molecular weight of stack gas
Calculator: Gas Density
lb/lb-mole
atm
°F
Gas Density
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Volumetric Flow Rate

The volumetric flow rate is the product of the average velocity (determined from Method 1 traverse + Method 2 pitot measurements) and the cross-sectional area.

Volumetric Flow Rate (Actual Conditions)
Qs = vs × A × 60
Qs
= volumetric flow rate (actual cubic feet per minute, ACFM)
vs
= average stack gas velocity (ft/s)
A
= cross-sectional area (ft²)
60
= conversion from seconds to minutes
Dry Volumetric Flow Rate (Standard Conditions)
Qsd = Qs × (1 − Bws) × (Tstd / Ts) × (Ps / Pstd)
Qsd
= dry standard volumetric flow rate (DSCFM)
Bws
= moisture fraction (from Method 4)
Tstd
= 528 °R (68 °F) or 293 °K (20 °C)
Pstd
= 1.0 atm
Calculator: Volumetric Flow Rate
ft/s
ft²
decimal (0 to 1)
°F
atm
Volumetric Flow Rate
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Stack Diameter from Circumference

In the field, it is often easier to measure the stack circumference (by wrapping a tape around the outside) than the diameter directly. The inside diameter must be derived by accounting for the wall thickness.

Inside Diameter from Circumference
D = (C / π) − 2 × t
D
= inside diameter
C
= outside circumference (measured with tape)
π
= 3.14159265
t
= wall thickness
Calculator: Inside Diameter from Circumference
Inches
Inches
Inside Diameter
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Quick Reference Summary

Use this table as a field reference card. All the key decisions and equations in one place.

Task Method / Rule Key Input
Circular: Number of pointsDiameter lookup tableInside diameter D
Circular: Point positionsLog-linear rulen (points/diameter), R = D/2
Rectangular: Number of pointsArea lookup tableA = W × H
Rectangular: Point positionsLog-Tchebycheff ruleGrid lines per axis
Inside diameterD = C/π − 2tCircumference C, thickness t
Cross-sectional area (circle)A = πD²/4Diameter D
Velocityv = KpCp√(ΔPT/MsPs)ΔP, Ts, Ms, Ps
Gas densityρ = MP/(RT)M, Ps, Ts
Volumetric flow (ACFM)Q = v × A × 60v, A
Dry std. flow (DSCFM)Qsd = Qs(1−Bws)(Tstd/Ts)(Ps/Pstd)Qs, Bws, Ts, Ps
Field Tip Always verify the inside diameter by measuring at least two perpendicular diameters with a tape or caliper at the sampling location. Never assume the nominal diameter equals the actual inside diameter — corrosion, buildup, and construction tolerances can cause significant errors.
Critical Reminder EPA Method 1 requires at least 8 stack diameters downstream and 2 diameters upstream of any flow disturbance. If this criterion cannot be met, you must either find a different location or add more traverse points and document the deviation. Regulatory agencies may reject data taken at non-compliant sites.

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