Air Pressure at Altitude Calculator
Calculate atmospheric pressure, temperature, and air density at any altitude using the International Standard Atmosphere (ISA) model. Supports humidity correction.
Calculate flow rate from differential pressure across orifice plates, Venturi tubes, flow nozzles, and Pitot tubes. Converts ΔP to flow velocity and volume.
| ΔP (kPa) | Q (L/s) | V (m/s) |
|---|---|---|
| 0.10 | 0.554 | 0.071 |
| 0.25 | 0.876 | 0.111 |
| 0.50 | 1.238 | 0.158 |
| 1.00 | 1.751 | 0.223 |
| 2.00 | 2.477 | 0.315 |
| 5.00 | 3.916 | 0.499 |
| 10.00 | 5.538 | 0.705 |
| 20.00 | 7.831 | 0.997 |
| 50.00 | 12.383 | 1.577 |
Differential pressure (DP) flow measurement exploits Bernoulli's principle: when fluid accelerates through a constriction, its static pressure drops in proportion to the square of its velocity. By measuring the pressure difference across the constriction and knowing the geometry, you can calculate the flow rate precisely.
This calculator supports four primary DP flow devices. The orifice plate is the simplest and most common — a thin plate with a concentric hole. Venturi tubes recover most of the pressure, reducing energy loss. Flow nozzles offer a middle ground, and Pitot tubes measure point velocity directly from velocity pressure ½ρV². Each device has a characteristic discharge coefficient (Cd) that accounts for real-flow effects.
Input your differential pressure in Pa, kPa, psi, inH₂O, or mmHg, and the calculator returns flow velocity, volume flow rate (L/s, L/min, gpm, m³/h), and the discharge coefficient used. The ΔP-vs-flow chart illustrates the square-root relationship between pressure and flow.
Differential-pressure flow measurement is used in over 30% of industrial flowmeters worldwide. This calculator helps engineers size orifice plates, check Venturi meters, and convert DP readings to flow rates.
Orifice / Venturi / Nozzle:
Q = Cd × E × A_d × √(2ΔP / ρ)
E = 1 / √(1 − β⁴), β = d/D
Pitot tube: V = √(2ΔP / ρ)
Where:
• Cd = discharge coefficient
• A_d = orifice area (m²)
• ΔP = differential pressure (Pa)
• ρ = fluid density (kg/m³)Result: Q ≈ 0.76 L/s, V ≈ 0.97 m/s
A_d = π/4 × (0.05)² = 1.963×10⁻³ m². E = 1/√(1−0.0625) = 1.033. Q = 0.61 × 1.033 × 0.001963 × √(10000/998) ≈ 0.00393 m³/s ≈ 3.93 L/s — actual numbers vary with precise Cd iterations.
Calculate flow rate from differential pressure across orifice plates, Venturi tubes, flow nozzles, and Pitot tubes. Converts ΔP to flow velocity and volume. Use it when you need a repeatable calculation in the physics / fluid category and want the setup, result, and supporting values kept together. This is especially helpful when small input changes, unit choices, or rounding decisions can change the final number.
Start by confirming that the inputs match the formula shown on the page. Then compare the main output with the worked example and any secondary values shown by the calculator. If the result will be used in another calculation, keep extra precision until the final step and record the assumptions beside the number.
Treat the result as a calculation aid rather than a substitute for context. For schoolwork, include the formula and substitution steps. For planning, technical, financial, or health-related decisions, verify important numbers against primary records, current rules, or a qualified professional before acting on them.
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Beta (β) is the ratio of the orifice bore diameter d to the pipe diameter D. It typically ranges from 0.2 to 0.75. Higher beta means less pressure loss but also less measurement signal.
Bernoulli's equation gives ΔP ∝ V² for incompressible flow. Inverting: V ∝ √ΔP. This means doubling the flow quadruples the differential pressure.
For a sharp-edged orifice, Cd ≈ 0.61. Machined Venturi tubes achieve Cd ≈ 0.985. Exact values depend on Re and β — standards like ISO 5167 provide detailed correlations.
A Pitot tube faces into the flow and measures the stagnation pressure minus static pressure (velocity pressure). It gives point velocity, not average velocity, and causes minimal flow disturbance.
The Venturi's gradual convergence and divergence minimize boundary-layer separation and turbulence, letting the actual flow rate very nearly match the theoretical prediction.
Yes, but for compressible gases at high pressure ratios (ΔP/P > ~10%), apply an expansion factor (ε or Y) to correct for gas density change through the restriction.
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