Orifice Flow & Plate Sizing CalculatorBadge rhg equation
Calculate orifice flow rate, differential pressure drop, and plate diameter for liquids and gases using ISO 5167 formulas. Instant sizing and Reynolds matrix.
Calculate orifice flow rate, differential pressure drop, and plate diameter for liquids and gases using ISO 5167 formulas. Instant sizing and Reynolds matrix.
Calculate orifice flow rate, differential pressure drop, and plate diameter for liquids and gases using ISO 5167 formulas. Instant sizing and Reynolds matrix.
Inside diameter of the upstream straight pipe section at operating temperature. ISO 5167-2 standard limits strictly require D between 50 mm (2 in) and 1000 mm (40 in). Pipe schedule wall thickness variations directly alter internal diameter and beta ratio.
Concentric square-edged circular restriction aperture. Must satisfy minimum diameter threshold d >= 12.5 mm (0.5 in). Edge sharpness must be maintained with edge radius r < 0.0004d to prevent discharge coefficient underestimation.
Static pressure differential measured between upstream and downstream pressure taps. Standard DP transmitters are scaled across spans of 25 mbar to 2500 mbar (10 to 1000 inH2O). High differential pressures in liquids risk flashing and cavitation.
Actual mass density of fluid passing the upstream tap under operating line temperature and pressure. For gases, density must be calculated via real gas equation of state taking compressibility factor Z into account.
Absolute internal fluid friction governing the pipe Reynolds number Re_D. Fully turbulent flow regime (Re_D >= 5000) is mandatory for Reader-Harris/Gallagher discharge coefficient stability.
Adiabatic exponent Cp/Cv defining expansion behavior for compressible gas media. Common values: diatomic gases (air, N2, O2) = 1.40; natural gas (CH4) = 1.30 to 1.32; superheated steam = 1.30.
Physical location of pressure sensing points altering L1 and L2 terms in ISO 5167 formulas. Flange taps (25.4 mm from plate faces) are universal in ASME piping; Corner taps dominate European compact assemblies; D and D/2 radius taps capture vena contracta recovery.
Because differential pressure is proportional to the square of flow (deltaP ~ Q²), reducing flow rate to 25% drops differential pressure to 6.25% of transmitter calibrated span. Transmitter sensing uncertainty multiplies fourfold, creating unacceptable metering errors below 30% flow. For wide dynamic processes, install split-range dual differential pressure transmitters.
If static pressure at the vena contracta drops below fluid vapor pressure (P_v), vapor cavities form and violently implode downstream. This destroys the downstream pipe bore, bevel edge, and invalidates ISO 5167 coefficients. Ensure cavitation index sigma = (P_upstream - P_v) / deltaP remains strictly above 2.5.
A microscopic rounding defect of merely 0.05 mm (0.002 in) on the upstream 90-degree square edge of the orifice plate causes fluid streamlines to round the corner with reduced vena contracta restriction. This artificially increases the effective discharge coefficient, leading to an undetected 2% to 4% flow rate under-measurement.
An orifice meter does not recover all differential pressure. Unrecoverable permanent loss deltaOmega approximately equals deltaP * (1 - beta^1.9). At beta = 0.50, exactly 73% of measured differential pressure is permanently lost as friction and turbulence heat, directly increasing pumping or compressor lifecycle power costs.
Resize the pipe internal diameter or re-span the differential pressure transmitter. When beta > 0.75, pipe wall roughness and upstream velocity profile distortions cause discharge coefficient uncertainty to escalate beyond +/-1.5%. When beta < 0.10, micro-roughness on the plate face dominates flow physics.
Gas expansion factor formula epsilon is invalid once differential pressure exceeds the critical acoustic ratio r_c = [2 / (kappa + 1)]^(kappa / (kappa - 1)) (~0.528 for air). Downstream backpressure changes can no longer propagate upstream. Switch to critical sonic nozzle formulations or install a multi-stage restriction orifice cascade.
Liquids accumulating behind the concentric orifice plate alter upstream approach profile and induce violent water hammer. Specify an eccentric or segmental orifice plate with opening flush with pipe bottom, or add an approved top vent hole for gas or bottom drain hole (diameter <= 0.1d) per ISO 5167-2 area compensation rules.
Viscous liquids or low-velocity operations drop the flow into laminar or transitional zones where the Reader-Harris/Gallagher equation breaks down. Replace the square-edge orifice plate with a conical entrance or quadrant-edge plate specifically designed and calibrated for viscous low-Reynolds flows (250 <= Re_D <= 10000).
Flow rate is calculated using the ISO 5167 equation Q = C_d * E * epsilon * (pi * d² / 4) * sqrt(2 * deltaP / rho), where C_d is the discharge coefficient (typically ~0.60 for turbulent pipe flow), E = 1 / sqrt(1 - beta⁴) is the velocity of approach factor, epsilon is the gas expansion factor (1.0 for liquids), d is the orifice bore diameter, deltaP is the measured pressure drop across taps, and rho is fluid density.
The recommended engineering sweet spot for beta ratio (d/D) is 0.30 to 0.60. While ISO 5167 permits a broader theoretical range between 0.10 and 0.75, ratios below 0.30 produce excessive permanent pressure loss, and ratios above 0.60 suffer from heightened sensitivity to upstream pipe wall roughness and velocity profile distortion.
Flange taps locate pressure sensing holes 25.4 mm (1.0 inch) upstream and downstream from the respective plate faces, making them easy to drill through pipe flanges in ASME piping systems. Corner taps locate pressure ports right at the junction of the pipe wall and plate face inside the flange carrier ring, maximizing pressure drop readings on European ISO/DIN installations and pipe sizes under 50 mm.
Permanent unrecoverable head loss across an orifice plate is calculated as deltaOmega = deltaP * (1 - beta^1.9). At a beta ratio of 0.2, approximately 95% of differential pressure is permanently lost; at beta = 0.5, 73% is lost; and at beta = 0.7, 49% is lost. This unrecovered pressure represents continuous energy dissipation dissipated as turbulence and heat.
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