Calculate gas flow rates with compressibility corrections. Convert between standard and actual conditions, determine flow velocities, and check for choked flow.
The Gas Flow Rate Calculator uses the isothermal compressible flow equation to determine gas flow rates through pipes. Unlike incompressible flow calculations used for liquids, gas flow must account for density changes as pressure drops along the pipe, making compressibility corrections essential for accurate results.
For isothermal gas flow through a pipe, the volumetric flow rate is calculated using:
Q = (π/4)D² × √((P1² - P2²) / (ρavg × f × L/D))
Where:
Gas volume depends on pressure and temperature. To compare flows at different conditions, volumes are converted to standard conditions (0°C, 101.325 kPa):
Qs = Qa × (Pa / Ps) × (Ts / Ta)
Where Qs is the standard flow rate, Qa is the actual flow rate, and the subscripts s and a denote standard and actual conditions respectively. Standard flow is expressed as Nm³/h (normal cubic meters per hour) or SCFM (standard cubic feet per minute).
| Gas | Molecular Weight (g/mol) | Specific Heat Ratio (k) |
|---|---|---|
| Air | 28.97 | 1.40 |
| Nitrogen | 28.01 | 1.40 |
| Oxygen | 32.00 | 1.40 |
| Natural Gas | 17.40 | 1.30 |
| Carbon Dioxide | 44.01 | 1.29 |
| Hydrogen | 2.016 | 1.41 |
| Argon | 39.95 | 1.67 |
Choked flow occurs when the gas velocity reaches sonic speed at the pipe exit. Once choked, further reducing downstream pressure does not increase the flow rate. The critical pressure ratio depends on the specific heat ratio (k) of the gas:
P2/P1 < (2 / (k + 1))^(k / (k - 1))
For air (k = 1.4), the critical ratio is approximately 0.528, meaning choked flow occurs when the outlet pressure drops below 52.8% of the inlet pressure. Under choked conditions, the mass flow rate is limited by the upstream conditions and pipe geometry.
Here you will find the answers to the frequently asked questions about gas flow rate calculations.
Incompressible flow assumes constant fluid density, which is valid for liquids and gases at very low velocities. Compressible flow accounts for density changes that occur as gas pressure and temperature vary along the pipe. For gases, compressibility effects become significant when the Mach number exceeds 0.3 or when the pressure drop exceeds about 10% of the inlet pressure. This calculator uses the isothermal compressible flow equation to accurately model gas behavior.
Standard conditions provide a reference point for comparing gas volumes measured at different pressures and temperatures. The most common standards are Normal conditions (0°C, 101.325 kPa) used internationally with units like Nm³/h, and Standard conditions (15.6°C / 60°F, 101.325 kPa / 14.696 psia) used in North America with units like SCFM. This calculator converts actual flow to normal conditions (0°C, 101.325 kPa).
Choked flow occurs when gas velocity at a restriction reaches the speed of sound (Mach 1). At this point, further reducing the downstream pressure will not increase the flow rate. Choked flow is determined by the critical pressure ratio, which depends on the specific heat ratio of the gas. For air (k = 1.4), the critical ratio is about 0.528. This calculator warns you when choked flow conditions are detected.
To calculate gas flow rate through a pipe, you need the pipe diameter, inlet and outlet pressures, gas temperature, pipe length, and pipe roughness. The isothermal compressible flow equation relates these parameters to the volumetric flow rate, accounting for friction losses and gas expansion along the pipe. The gas density is calculated from the ideal gas law using the molecular weight and operating conditions.
Gas flow rates can be expressed in actual or standard units. Actual flow units include m³/h (cubic meters per hour) and CFM (cubic feet per minute), which represent the volume at operating conditions. Standard flow units include Nm³/h (normal cubic meters per hour) and SCFM (standard cubic feet per minute), which represent the equivalent volume at standard reference conditions. Mass flow in kg/h is independent of pressure and temperature.
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