Key Equations
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.
The principles behind this flow rate calculation tool are widely applied in CAE and various engineering fields. The first that comes to mind is "verification of CFD (Computational Fluid Dynamics) analysis". After analyzing a complex flow path with CFD, you calculate something like, "the flow rate at the inlet or outlet is about this much." You can use a quick estimation with a simple calculation like this tool to verify if that result is in the physically correct order of magnitude. CFD can easily become a black box, so it's important to hone your intuition with such fundamental calculations.
Another is "piping system design and pump selection". When designing piping for a plant or building, you often need to work backwards to determine the required differential pressure (i.e., pump head) to ensure the necessary flow rate. By using this tool to iteratively find the ΔP needed to achieve your target flow rate, you can directly apply it to pump specification studies. Especially when using an orifice, the pressure loss is significant, making it a key parameter directly linked to pump power consumption.
Furthermore, it is deeply connected to "aerodynamic design for automobiles and aircraft". The principle of the Pitot tube is exactly what's used in car speedometers and aircraft airspeed indicators. Selecting "air" in the tool and experiencing the relationship between differential pressure (dynamic pressure) and flow velocity directly contributes to a fundamental understanding of aerodynamic measurement. Moreover, the smooth flow path shape of a venturi relates to the concepts behind "diffuser and nozzle design in fluid machinery". The perspective on how to efficiently accelerate or decelerate flow is also applied in the design of turbine blades and engine intake manifolds.
Once you're comfortable with this tool, try moving to the next step. First, I recommend "delving deeper into the nature of the discharge coefficient $C_d$". Why is it around 0.6 for an orifice and close to 1 for a venturi? The answer lies in "energy loss" and "velocity profile". For an orifice, flow separation at the constriction creates vortices (turbulence), converting kinetic energy into heat (a loss). $C_d$ is the correction factor for this in the theoretical formula. If you open a textbook, you'll likely see $C_d$ expressed as a function of the beta ratio β and the Reynolds number $Re$.
Regarding the mathematical background, I want you to appreciate the power of "dimensional analysis". Even for phenomena involving many variables like the flow rate equation $Q = f(D, d, \Delta P, \rho, \mu)$, using Buckingham's π theorem allows you to consolidate them into relationships between dimensionless numbers ($C_d, \beta, Re$). This becomes a powerful tool for organizing experimental data and correlating models at different scales with actual machines.
The next topic you should learn is "flow rate calculation for compressible fluids". This tool assumes water, oil, or low-speed air, so it uses the constant density (incompressible) formula. However, for gases flowing at high speeds (e.g., compressed air in pipes or flow around aircraft), as the velocity approaches the speed of sound, density changes significantly, and the flow reaches a limiting state called "choke". As your next learning step, researching keywords like "venturi nozzle" and "critical pressure ratio" will reveal another important aspect of fluid mechanics.