Calculate coefficient of discharge (Cd), theoretical and actual flow rates for orifices, nozzles, weirs, and Venturi meters.
The coefficient of discharge (Cd) is the ratio of actual flow rate to theoretical flow rate through an orifice or flow device. It accounts for energy losses from friction, turbulence, and flow contraction at the vena contracta that reduce the actual flow below the ideal prediction.
Torricelli's theorem gives the theoretical velocity through an orifice: v = √(2gH), where H is the head of fluid. The theoretical flow rate Q_theo = A × v. In practice, Cd ranges from about 0.51 (Borda re-entrant orifice) to 0.98 (well-rounded nozzle). A standard sharp-edged orifice has Cd ≈ 0.61.
This calculator computes flow rates from known Cd values or determines Cd from measured flow data. It includes a database of standard discharge coefficients for common flow devices, Reynolds number estimation, and coefficient breakdown into velocity (Cv) and contraction (Cc) components. Check the example with realistic values before reporting. Use the steps shown to verify rounding and units. Cross-check this output using a known reference case.
Flow rate calculations for orifices and other devices require knowing Cd, which varies by geometry, Reynolds number, and installation conditions. Standard references list Cd for various devices, but applying them with correct units and determining theoretical flow requires multiple steps.
This calculator provides both forward (Cd → flow rate) and inverse (measured flow → Cd) calculations, with a built-in database of standard coefficients. It is useful for hydraulic engineers, students, and anyone designing or calibrating flow measurement devices.
Q_actual = Cd × A × √(2gH). Cd = Q_actual / Q_theoretical. Cd = Cv × Cc. Torricelli: v = √(2gH). Re = ρvD/µ.
Result: 6.04 × 10⁻³ m³/s actual flow (6.04 L/s)
v_theo = √(2 × 9.81 × 5) = 9.90 m/s. Q_theo = 0.001 × 9.90 = 9.90 × 10⁻³ m³/s. Q_actual = 0.61 × 9.90 × 10⁻³ = 6.04 × 10⁻³ m³/s = 6.04 L/s.
Torricelli's theorem (1643) states that the velocity of fluid through an orifice is v = √(2gH), identical to the velocity of a body falling freely from height H. This assumes inviscid, incompressible flow — a good approximation for water at moderate pressures.
The actual flow is less than the theoretical value because: (1) the flow contracts at the vena contracta, reducing the effective area; (2) friction along the orifice walls dissipates some kinetic energy; (3) turbulence creates additional losses. The coefficient of discharge captures all three effects in a single empirical number.
**Orifice plates** are thin plates with precisely machined holes, installed in pipelines. They are cheap but cause significant pressure loss (60-80% of differential pressure is not recovered). ISO 5167 provides detailed specifications for orifice flow measurement.
**Venturi meters** have a gradual contraction and expansion that minimizes losses. Cd ≈ 0.975 with only 10-20% unrecovered pressure loss. Used where permanent pressure loss must be minimized.
**Weirs** measure open channel flow. V-notch weirs are accurate for low flows; rectangular weirs handle higher flows. The Francis formula gives Q = 1.84 × L × H^1.5 for rectangular weirs.
To measure Cd experimentally, set up the orifice in a constant-head tank or pipeline with known area and head. Collect the discharged fluid in a graduated vessel over a measured time. Calculate Q_actual = Volume/Time, then Cd = Q_actual / (A × √(2gH)). Repeat at several head values to establish Cd vs Re behavior.
Cd is the ratio of actual flow to theoretical flow through an opening. It accounts for losses due to friction, turbulence, and vena contracta (flow contraction). Cd = Q_actual / Q_theoretical, and it is always ≤ 1.
The flow contracts as it passes through a sharp orifice, forming a vena contracta about 0.64 of the orifice area. Combined with velocity losses, this gives Cd ≈ 0.61. A well-rounded orifice avoids contraction and achieves Cd ≈ 0.98.
The vena contracta is the point where the flow cross-section is smallest — downstream of the orifice where streamlines are most converged. For a sharp-edged orifice, it occurs at about 0.5 diameters downstream and has an area about 0.64× the orifice.
Yes — at low Reynolds numbers (<10,000), Cd decreases because viscous effects become more significant. Above Re ≈ 100,000, Cd is essentially constant for a given geometry. Most tabulated values assume turbulent flow.
Cd = Cv × Cc. Cv is the velocity coefficient (actual velocity / theoretical velocity, accounts for friction). Cc is the contraction coefficient (vena contracta area / orifice area). For a sharp orifice, Cv ≈ 0.97 and Cc ≈ 0.64, giving Cd ≈ 0.62.
Measure the actual flow rate (volume collected over time, or flow meter) and divide by the theoretical rate Q = A√(2gH). The ratio is Cd. Multiple measurements at different heads improve accuracy.