Orifice Flow Calculator

Enter the orifice diameter, discharge coefficient, pressure differential, and fluid density to get volumetric flow rate, mass flow rate, and jet velocity using Q = Cd·A·√(2ΔP/ρ).

Quick Facts

Orifice equation
Q = Cd·A·√(2ΔP/ρ)
Volumetric flow through a sharp-edged orifice or nozzle driven by a pressure differential ΔP.
Typical Cd values
0.60 – 0.98
Sharp-edged orifice ≈ 0.61; short tube ≈ 0.80; well-rounded bell-mouth nozzle ≈ 0.95–0.98.
Torricelli's law
v = √(2gh)
Special case when the pressure differential comes from a fluid head h (ΔP = ρgh) — density cancels out.
Incompressible-flow limit
ΔP / P₁ ≲ 0.1
This calculator assumes incompressible flow; large pressure ratios in gases need compressible-flow equations.

Your Results

Calculated
Volumetric Flow Rate
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Q = Cd·A·√(2ΔP/ρ), in liters per minute
Flow Rate (US units)
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Same flow rate in US gallons per minute
Mass Flow Rate
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ṁ = ρ × Q, in kilograms per second
Jet Velocity
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v = Cd × √(2ΔP/ρ) at the orifice

Ready

Enter the orifice geometry, pressure differential, and fluid density, then press Calculate.

How the Orifice Flow Equation Works

An orifice is a defined opening — a drilled hole in a plate, a nozzle, or a valve port — that restricts flow and creates a pressure drop as fluid passes through it. The orifice flow equation, Q = Cd·A·√(2ΔP/ρ), predicts the volumetric flow rate Q through that opening from its cross-sectional area A, the pressure differential ΔP across it, the fluid density ρ, and an empirical discharge coefficient Cd that accounts for real-world losses. It is one of the most widely used relationships in fluid mechanics, underlying orifice-plate flow meters, hydraulic valve sizing, spray-nozzle design, and tank-drainage calculations.

Deriving Q = Cd·A·√(2ΔP/ρ)

Start from Bernoulli's equation between a point well upstream of the orifice (pressure P1, velocity ≈ 0 in a large reservoir or pipe) and the jet just past the opening (pressure P2, velocity v): P1 + ½ρv1² = P2 + ½ρv2². Neglecting the small upstream velocity and any elevation change gives an ideal, frictionless jet velocity of v_ideal = √(2ΔP/ρ), where ΔP = P1 − P2 — the same relationship behind Torricelli's law for a draining tank. Real flow always falls short of that ideal because of viscous friction and the vena contracta, the point just downstream of a sharp-edged orifice where the jet narrows to less than the hole's geometric area. The discharge coefficient Cd (typically 0.6–0.98) is the ratio of actual to ideal flow, so the actual flow rate becomes Q = Cd·A·√(2ΔP/ρ), with A = π/4 × d² for a circular orifice of diameter d.

Choosing Cd and where the equation breaks down

Cd depends on the orifice's edge geometry, its thickness-to-diameter ratio, and the Reynolds number of the flow: a thin sharp edge gives Cd ≈ 0.60–0.61, a short cylindrical tube (length about equal to its diameter) gives Cd ≈ 0.80, and a smooth, rounded bell-mouth entrance can reach Cd ≈ 0.95–0.98. This simple form also assumes the orifice sits in a large reservoir or a pipe whose diameter is much larger than the orifice, so upstream velocity is negligible; for an orifice plate installed in a pipe of comparable diameter, engineers apply an additional beta-ratio correction (per ISO 5167 / ASME MFC-3M). The formula further assumes steady, single-phase, incompressible flow — accurate for liquids and for gases only when ΔP stays small relative to the absolute upstream pressure (roughly ΔP/P1 below about 10%); beyond that, use compressible-flow or choked-flow equations. For liquids, also confirm the downstream pressure stays above the fluid's vapor pressure, or cavitation will reduce the real flow below the calculated value.

Frequently Asked Questions

What is the orifice flow equation?
The standard orifice flow equation is Q = Cd·A·√(2ΔP/ρ), where Q is the volumetric flow rate, Cd is the discharge coefficient, A is the orifice's cross-sectional area, ΔP is the pressure differential across the orifice, and ρ is the fluid density. It comes from applying Bernoulli's equation between the upstream flow and the orifice jet, then correcting the ideal result for real-world losses with Cd.
What discharge coefficient (Cd) should I use?
For a thin, sharp-edged circular orifice, Cd ≈ 0.60–0.61 is standard. A short cylindrical tube (length about equal to its diameter) typically runs Cd ≈ 0.80, and a smooth, well-rounded bell-mouth nozzle can reach Cd ≈ 0.95–0.98 because it avoids the vena contracta. Manufacturer data or a calibration test is more reliable than a generic value when precision matters.
Does this formula work for compressed gases as well as liquids?
Only approximately. The equation assumes incompressible flow, which holds well for liquids and for gases when the pressure drop is small relative to the absolute upstream pressure (roughly ΔP/P1 below about 10%). At larger pressure ratios — and especially near or beyond the choked-flow limit (about 0.528 for air) — gas density changes significantly through the orifice, and compressible-flow equations are needed instead of this incompressible form.