Orifice / Venturi:
$Q = C_d \cdot \frac{\pi d^2}{4}\cdot \sqrt{\dfrac{2\Delta P}{\rho(1-\beta^4)}}$Pitot Tube:
$V = \sqrt{\dfrac{2\Delta P}{\rho}},\quad Q = V \cdot A$Reynolds Number:
$Re = \dfrac{V \cdot D}{\nu}$Compare 4 flow meter types side by side. Select fluid (water/oil/air), adjust pipe diameter and differential pressure to instantly compute volumetric flow rate, mass flow rate, velocity and Reynolds number.
Orifice / Venturi:
$Q = C_d \cdot \frac{\pi d^2}{4}\cdot \sqrt{\dfrac{2\Delta P}{\rho(1-\beta^4)}}$Pitot Tube:
$V = \sqrt{\dfrac{2\Delta P}{\rho}},\quad Q = V \cdot A$Reynolds Number:
$Re = \dfrac{V \cdot D}{\nu}$The core principle for orifice, venturi, and pitot tubes is the conservation of energy, described by Bernoulli's equation for incompressible flow. The pressure drop across a constriction is related to the increase in fluid velocity.
$$Q = C_d \cdot A_t \cdot \sqrt{\dfrac{2\Delta P}{\rho(1-\beta^4)}}$$Where:
$Q$ = Volumetric Flow Rate [m³/s]
$C_d$ = Discharge Coefficient (accounts for friction & geometry, ~0.6 for orifice, ~0.98 for venturi)
$A_t$ = Throat/Orifice Area = $\pi d^2/4$
$\Delta P$ = Differential Pressure [Pa]
$\rho$ = Fluid Density [kg/m³]
$\beta$ = Diameter Ratio $d/D$
The term $(1-\beta^4)$ corrects for the change in the pipe's cross-sectional area.
For a Pitot Tube, it measures the stagnation pressure versus static pressure to find the local velocity at a single point, which is then used to estimate flow in a known pipe area.
$$V = \sqrt{\dfrac{2\Delta P}{\rho}}, \quad Q = V \cdot A$$Where:
$V$ = Local Fluid Velocity [m/s]
$A$ = Cross-sectional Area of the Pipe = $\pi D^2/4$
This assumes a uniform velocity profile, which is rarely true, so it often requires a correction factor.
Natural Gas Pipelines: Venturi meters are often used for high-accuracy, high-volume custody transfer where minimizing pressure loss saves on pumping costs over hundreds of miles. The smooth bore also handles the clean gas well without clogging.
Chemical Process Plants: Orifice plates are ubiquitous for monitoring flow of various process streams due to their simplicity, low cost, and ease of replacement. Different materials (e.g., Hastelloy) can be used for corrosive fluids.
Aircraft Airspeed Indicators: The pitot-static tube is a critical sensor on every aircraft, measuring dynamic pressure to calculate airspeed. Its reliability and simple mechanical principle are vital for flight safety.
Wastewater Treatment: Electromagnetic flow meters are ideal here because they can measure the flow of conductive, sludge-filled water without any obstruction that could get clogged. They also have no moving parts to wear out.
While experimenting with this tool, you might encounter a few easily misunderstood points, so it's good to keep them in mind before using it in practice. First, you might tend to think "if the differential pressure ΔP is the same, the flow rate Q is also the same," but that's a major mistake. It's because the discharge coefficient $C_d$ is completely different. For example, for water flowing in the same pipe (D=100mm) with a differential pressure set to 10kPa, the calculated flow rate for an orifice ($C_d≈0.61$) versus a venturi ($C_d≈0.98$) differs by about 1.6 times. If you switch between them in the tool, the difference becomes immediately clear.
Next, don't underestimate the importance of fluid selection. Some people are surprised when selecting oil, asking, "Why is the flow rate so much lower than for water?" This is because density ρ is part of the equation. Even with the same differential pressure, a fluid with higher density (heavier) is harder to accelerate. For instance, for oil with a density of about 800 kg/m³ and water with about 1000 kg/m³, theoretically, water would flow at a rate about √(1000/800)≈1.12 times greater. For air (density about 1.2 kg/m³), the difference is even more dramatic.
Finally, remember that this simulation calculates under "ideal conditions". In real-world applications, the inlet shape of the pipe or upstream flow disturbances affect the discharge coefficient, and fluid temperature changes alter viscosity and density. Especially in the low Reynolds number region (where viscous effects are strong), $C_d$ is not constant. The tool's results are merely a "first approximation". For detailed design or measurement, you'll need the detailed correction formulas specified in the JIS or ISO standards for each flow meter.
Water (ρ=1000 kg/m³) flows through 100 mm carbon steel pipe with 65 mm orifice plate. Measured differential pressure: 85 kPa. Cd=0.61, β=0.65. Using Q = Cd × A₂ × √(2ΔP/ρ), throat area A₂ = π(0.0325)²/4 = 0.00331 m². Q = 0.61 × 0.00331 × √(2×85000/1000) = 0.0118 m³/s (42.5 m³/h). Mass flow ṁ = 1000 × 0.0118 = 11.8 kg/s. Velocity V = 0.0118/(π×0.05²/4) = 1.5 m/s. Reynolds Re = ρVD/μ ≈ 150,000 (fully turbulent, valid for orifice).