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Hydraulics, open channels and fluid power

Differential-pressure Venturi meter discharge

Volume flow through a Venturi from the upstream-to-throat pressure difference Δp, throat area At and diameter ratio β, for steady incompressible full-pipe flow with equal-elevation taps and a calibrated discharge coefficient.

Ref
HYD-16
Rev
v1
Field
Hydraulics, open channels and fluid power
Result
Q [m³/s]

A Venturi meter speeds the flow through a throat, lowering the pressure there. Bernoulli and continuity give Q = Cd At √[2Δp/(ρ(1 − β⁴))], where β is the throat-to-pipe diameter ratio and Cd corrects for friction. The flow varies with the square root of the pressure difference. Use a calibrated Cd; typical values are close to 0.98 for a well-made meter at high Reynolds number.

Volume flow through a Venturi from the upstream-to-throat pressure difference Δp, throat area At and diameter ratio β, for steady incompressible full-pipe flow with equal-elevation taps and a calibrated discharge coefficient.

Calculator

Solve for
m³/s
0.51.1
m²
1e-51
Pa
101e7
kg/m³
50014,000
0.10.9
  • Throat speed, Q/At3.92 m/s
  • Pipe speed, Q β²/At0.98 m/s
  • Velocity-of-approach factor, 1/√(1 − β⁴)1.033

What drives the result

Each variable is moved across its typical range while the others stay at the values above. The longest bar is the key driver.

Discharge (m³/s) current value 0.0392 m³/s
AtThroat areaKey driver
3.92e-53.92
ΔpUpstream-to-throat pressure difference
0.001431.43
ρLiquid density
0.01050.0554
βThroat-to-pipe diameter ratio
0.0380.0647
CdDischarge coefficient
0.020.044
  • A 7,500 Pa difference gives 0.0392 m³/s (39.2 litres per second), with a throat speed of 3.92 m/s.
  • Because Q follows √Δp, doubling the flow needs four times the pressure difference, which limits the range of one meter.
Chart data as tables

Ranked variables

VariableTypical rangeLowest resultHighest resultSwing (m³/s)Local stepChange in result
At Throat area1e-5 to 1 m²3.92e-53.923.92+10%+10 %
Δp Upstream-to-throat pressure difference10 to 1e7 Pa0.0014311.4311.43+10%+4.88 %
ρ Liquid density500 to 14,000 kg/m³0.010480.055440.04496+10%−4.65 %
β Throat-to-pipe diameter ratio0.1 to 0.9 0.037960.064720.02677+10%+1.58 %
Cd Discharge coefficient0.5 to 1.1 0.020.0440.024+10%+10 %

Sweep of Upstream-to-throat pressure difference

Upstream-to-throat pressure difference (Pa)Discharge (m³/s)
100.001431
56.230.003394
316.20.008049
1,7780.01909
10,0000.04526
56,2300.1073
316,2000.2545
1,778,0000.6036
1e71.431

Sweep one variable

Discharge (m³/s)Hover, touch, or use the arrow keys on the chart
00.511.5 10100100010k100k1M10M Upstream-to-throat pressure difference (Pa), log scale now 0.0392

Variables and how each one contributes

Q

Discharge

Result · m³/s

What the equation gives you. Everything else feeds it.

Cd

Discharge coefficient

· typical 0.5 to 1.1

The discharge coefficient, close to 1 for a good meter. Raises the flow in direct proportion. Raising it by 10 % (to 1.078) moves the result by +10 %, from 0.0392 to 0.04312 m³/s.

At

Throat area

m² · typical 1e-5 to 1

The throat area, in m². Raises the flow in direct proportion. Raising it by 10 % (to 0.011) moves the result by +10 %, from 0.0392 to 0.04312 m³/s.

Δp

Upstream-to-throat pressure difference

Pa · typical 10 to 1e7

The upstream-to-throat pressure difference, in Pa. Raises the flow with the square root of the pressure difference. Raising it by 10 % (to 8,250) moves the result by +4.88 %, from 0.0392 to 0.04111 m³/s.

ρ

Liquid density

kg/m³ · typical 500 to 14,000

The liquid density, in kg/m³. A denser liquid gives less flow for the same pressure difference, with a square-root effect. Raising it by 10 % (to 1,100) moves the result by −4.65 %, from 0.0392 to 0.03738 m³/s.

β

Throat-to-pipe diameter ratio

· typical 0.1 to 0.9

The throat-to-pipe diameter ratio, between 0 and 1. A larger ratio reduces the speed-up from pipe to throat, so a given pressure difference means more flow. Raising it by 10 % (to 0.55) moves the result by +1.58 %, from 0.0392 to 0.03982 m³/s.

Worked example with the values above

  1. Approach factor: 1 − β⁴ = 1 − 0.0625 = 0.9375.
  2. Speed term: √[2 × 7,500 / (1,000 × 0.9375)] = 4 m/s.
  3. Q = 0.98 × 0.01 × 4 = 0.0392 m³/s.

Assumptions and limits

  • Steady flow with the discharge coefficient suited to the installation and the Reynolds number.
  • For weirs: free discharge with an aerated nappe, a thin or broad crest as stated and negligible approach velocity.

Common mistakes

  • Measuring the head at the crest of the weir instead of upstream, beyond the drawdown.
  • Using a coefficient from a different weir type or scale.
  • Using the total head where the static head over the crest is needed, or the reverse.

Statistics and uncertainty

Discharge coefficients are calibrated values, normally good to 1 % to 5 %, and the head enters with a power of 1.5 to 2.5, so a 1 % error in head gives an error in flow of 1.5 % to 2.5 %.

Where it is used

  • Measuring flow in pipes, canals, rivers and flumes.
  • Setting weir crest levels and sizing overflows.

Maths you need

  • Discharge coefficient: the ratio of actual to ideal flow
  • Bernoulli equation: energy conservation along a streamline
  • Critical flow: flow at its minimum specific energy, with Froude number 1

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