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Fluid Dynamics (Bernoulli) Calculator

Apply Bernoulli's equation to calculate pressure or velocity changes in an ideal fluid between two points at different heights.

About this calculator

This calculator applies Bernoulli's equation — the statement that pressure, kinetic energy, and gravitational potential energy per unit volume sum to a constant along a streamline in an ideal fluid — to two points at possibly different heights, velocities, and pressures. Because Bernoulli's equation alone has more unknowns than equations, the tool reports several conditional results rather than one answer: the pressure at point 2 if velocity stays the same (useful for elevation changes in a pipe of constant diameter), and two velocity-at-point-2 scenarios — one holding pressure constant, and one assuming point 2 is open to atmosphere (zero gauge pressure), which reduces to a Torricelli-like efflux velocity for tank-draining problems. It also breaks down point 1's total energy per unit volume into its three components — static pressure, dynamic pressure (one-half density times velocity squared), and hydrostatic pressure (density times gravity times height) — so you can see which term dominates.

The chart shows how pressure trades off against height at a fixed velocity, visualizing the hydrostatic term in isolation. Keep in mind Bernoulli's equation assumes an ideal fluid: incompressible, non-viscous, and in steady, non-turbulent flow along a single streamline with no pumps or turbines between the two points. Real pipe flow includes friction losses that this calculator doesn't model, so treat results as an upper-bound, ideal-case estimate, not a substitute for a head-loss calculation in real piping systems.

Inputs

Pa
m/s
ft
ft
kg/m³

Results

P₂ (same velocity)

150,375 Pa

v₂ (same pressure)

10.1 m/s

v₂ (P₂ = 0 gauge)17.46 m/s
Total Energy per Volume152,375 Pa
Dynamic Pressure (½ρv²)2,000 Pa
Hydrostatic Pressure (ρgh)49,050 Pa
How to Use This Calculator
  1. Enter Pressure at Point 1 (P₁), Velocity at Point 1 (v₁), and Height at Point 1 (h₁).
  2. Set Height at Point 2 (h₂) and Fluid Density.
  3. Review P₂ (same velocity) (Pa) and v₂ (same pressure) (m/s).
  4. Use v₂ (P₂ = 0 gauge) (m/s) and Total Energy per Volume (Pa) to inform your decision.
  5. Use the chart to visualize the results and explore different scenarios by adjusting inputs.

How the result changes with Pressure at Point 1 (P₁)

Pressure at Point 1 (P₁)P₂ (same velocity)v₂ (same pressure)
50,66399,713 Pa10.1 m/s
75,994125,044 Pa10.1 m/s
151,988201,038 Pa10.1 m/s
253,313302,363 Pa10.1 m/s

What each input means

Pressure at Point 1 (P₁)
Static pressure at point 1 in pascals. Atmospheric pressure ≈ 101,325 Pa.
Velocity at Point 1 (v₁)
Flow velocity at point 1 in meters per second.
Height at Point 1 (h₁)
Elevation of point 1 above the reference level.
Height at Point 2 (h₂)
Elevation of point 2 above the reference level.
Fluid Density
Density of the fluid. Water ≈ 1000 kg/m³, air ≈ 1.225 kg/m³, mercury ≈ 13,546 kg/m³.

How this is calculated

Worked example, using the default values

  1. Identify Input Parameters
    4 parameters
    Pressure at Point 1 (P₁) = 101325, Velocity at Point 1 (v₁) = 2, Height at Point 1 (h₁) = 5, Height at Point 2 (h₂) = 0 = 5 input(s) provided
  2. Calculate P₂
    P₂
    150375 = 150375
  3. Calculate v₂
    v₂
    10.104 = 10.104
  4. Calculate v₂
    v₂
    17.457 = 17.457
  5. Calculate Total Energy per Volume
    Total Energy per Volume
    152375 = 152375

Engine last updated . Checked against 1 independently-derived test — how we verify calculators. Built by Paul Gunder, a software engineer, not a licensed financial, medical, or legal professional.

Frequently Asked Questions

Why does the calculator give several different results instead of one answer for point 2?

Bernoulli's equation alone has more unknowns (pressure, velocity, and height at point 2) than equations to solve them with, so a unique answer requires an assumption about which quantity stays fixed. The calculator reports pressure2SameV (assuming velocity is unchanged, useful for a constant-diameter pipe with an elevation change) and two velocity scenarios — one holding pressure constant and one assuming point 2 is open to atmosphere — rather than picking one assumption for you.

What does the 'v₂ (P₂ = 0 gauge)' result represent?

It's the velocity at point 2 if that point is open to atmospheric pressure (zero gauge pressure), computed from the full Bernoulli balance of point 1's pressure, velocity, and height difference. This is the classic Torricelli-type scenario — for example, fluid exiting a tank into open air — where the exit velocity depends on the driving pressure and elevation head rather than a fixed downstream pressure.

What do the dynamic, static, and hydrostatic pressure components tell you?

These three values decompose point 1's total energy per unit volume into its parts: static pressure is the input pressure directly, dynamic pressure (½ρv²) represents kinetic energy from the fluid's motion, and hydrostatic pressure (ρgh) represents potential energy from elevation. Comparing their magnitudes shows which effect dominates the flow at that point — for example, at low velocity in a tall tank, hydrostatic pressure will dwarf the dynamic term.

Why might real-world results differ from what this calculator predicts?

Bernoulli's equation assumes an ideal fluid — incompressible, non-viscous, and flowing steadily along a single streamline with no pumps, turbines, or friction losses between the two points. Real piping systems lose energy to wall friction, fittings, and turbulence, so actual pressures and velocities will be somewhat lower than this frictionless, ideal-case calculation predicts, especially over longer runs of pipe.

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