Enter the velocity of flow (m/s) and the density (kg/m^3) into the calculator to determine the Pressure From Velocity. 

Velocity To Pressure Calculator

Enter one value to calculate the other

Pressure From Velocity Formula

The following formula is used to calculate dynamic pressure from velocity.

$ P = V^2 * d / 2 $

  • P is the dynamic pressure (pascals, Pa)
  • v is the fluid velocity (m/s)
  • ρ (rho) is the fluid density (kg/m³)

This equation derives from the kinetic energy per unit volume of a moving fluid. It is one component of Bernoulli’s equation, which describes the conservation of energy in fluid flow: total pressure = static pressure + dynamic pressure. The dynamic pressure term captures how much of the total pressure budget comes from the fluid’s motion rather than its resting state.

Static, Dynamic, and Total Pressure

In any flowing fluid, three pressure components exist simultaneously. Static pressure acts equally in all directions and is the pressure you would measure if you moved with the fluid. Dynamic pressure is the additional pressure produced by the fluid’s velocity. Total pressure (also called stagnation pressure) is the sum of these two. Bernoulli’s equation expresses this relationship: P_total = P_static + (1/2)ρv². A pitot tube exploits this principle by measuring total pressure at a forward-facing opening and static pressure at side ports, with the difference yielding the dynamic (velocity) pressure directly.

This distinction matters in engineering because instruments rarely measure velocity directly in a pipe or duct. Instead, a differential pressure sensor reads the gap between total and static pressure, and the velocity is back-calculated. HVAC engineers size ducts this way, aerodynamicists derive airspeed from it, and process engineers monitor flow rates in chemical plants using the same underlying relationship.

Air Velocity to Dynamic Pressure Reference

The following table uses standard sea-level air density of 1.225 kg/m³ (15 °C, 101.325 kPa). For altitudes above sea level or temperatures significantly different from 15 °C, the density drops and so does the resulting dynamic pressure at the same velocity.

Air Velocity to Dynamic Pressure (ρ = 1.225 kg/m³)
Velocity (m/s)Velocity (ft/min)Pressure (Pa)Pressure (in. w.g.)Pressure (psi)
598415.30.0610.0022
101,96961.30.2460.0089
152,953137.80.5530.0200
203,937245.00.9840.0355
254,921382.81.5380.0555
305,906551.32.2140.0799
407,874980.03.9360.1421
509,8431,531.36.1500.2220
7514,7643,445.313.8380.4996
10019,6856,125.024.6010.8884
15029,52813,781.355.3521.9989
20039,37024,500.098.4033.5536
1 in. w.g. = 248.84 Pa. Assumes dry air at sea level, 15 °C.

Water Velocity to Dynamic Pressure Reference

Water is roughly 800 times denser than air, so dynamic pressures are dramatically higher at the same velocity. The table below uses a density of 998 kg/m³ (fresh water at 20 °C). These values are relevant to pipe sizing, pump selection, and erosion velocity limits in plumbing and process systems.

Water Velocity to Dynamic Pressure (ρ = 998 kg/m³, 20 °C)
Velocity (m/s)Pressure (Pa)Pressure (kPa)Pressure (psi)
0.5124.80.1250.018
1.0499.00.4990.072
1.51,122.81.1230.163
2.01,996.01.9960.290
3.04,491.04.4910.651
4.07,984.07.9841.158
5.012,475.012.4751.809
7.528,068.828.0694.071
10.049,900.049.9007.236
15.0112,275.0112.27516.281
Fresh water at 20 °C. P = 0.5 × 998 × v².

Common Fluid Densities for Pressure Calculations

Choosing the correct density is the most common source of error when converting velocity to pressure. The table below gives standard reference densities for fluids frequently encountered in engineering. Temperature and pressure both shift density: gases are especially sensitive (air density drops about 17% between 15 °C and 60 °C at the same altitude), while liquids change by only a few percent over normal working ranges.

Reference Densities of Common Fluids
FluidTemp (°C)Density (kg/m³)Notes
Air (sea level)151.225ISA standard atmosphere
Air (sea level)401.127Hot day conditions
Air (1,500 m altitude)151.056Approx. Denver, CO elevation
Fresh water20998Most piping calcs
Seawater151,025Average ocean salinity
Diesel fuel20832Typical No. 2 diesel
Hydraulic oil (ISO 32)40860Common hydraulic system oil
Gasoline20737Varies by blend
Ethanol20789Pure (200-proof)
Natural gas150.72Approximate, varies by composition
Steam (1 atm)1000.598Saturated at atmospheric pressure

Where Velocity-to-Pressure Conversion Is Used

HVAC duct design is one of the largest application areas. Engineers measure velocity pressure with a pitot tube traverse across a duct cross-section, convert each reading to a local velocity, and then average those velocities to find total airflow in cubic feet per minute (CFM) or cubic meters per hour. Duct friction loss charts are indexed by velocity, but the field measurement comes from a pressure differential, so the conversion happens constantly on every commissioning job.

In aerospace, pitot-static systems on aircraft feed dynamic pressure into airspeed indicators. At low speeds the incompressible form of the equation applies directly. Above roughly Mach 0.3, compressibility corrections become necessary, and the relationship between measured pressure and true airspeed grows more complex. For subsonic commercial flight, indicated airspeed is essentially a calibrated dynamic-pressure reading.

Hydraulic and process piping engineers use the same formula when calculating minor losses through fittings. Every loss coefficient (K-factor) for elbows, tees, valves, and reducers is multiplied by the velocity pressure to yield the pressure drop across that fitting. A system with 50 fittings requires 50 individual velocity-pressure products, making a reliable conversion tool essential for accurate system curves.

Wind engineering applies velocity-to-pressure conversion to estimate wind loads on structures. Building codes such as ASCE 7 define reference wind speeds and then convert them to velocity pressures (often denoted q_z) that serve as the basis for structural load calculations on walls, roofs, and cladding.

Compressibility Limits

The standard formula P = (1/2)ρv² assumes the fluid is incompressible, meaning its density does not change as it accelerates or decelerates. This holds well for all liquids and for gases at Mach numbers below about 0.3 (roughly 100 m/s or 370 km/h in air at sea level). Beyond that threshold, air density itself changes measurably across the flow, and the simple equation underestimates the actual stagnation pressure. Corrections use isentropic relations that account for the ratio of specific heats. For practical HVAC and low-speed industrial work, the incompressible formula is accurate to within 2% of the true value.

velocity to pressure calculator