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Science

Bernoulli Equation Calculator (Fluid Speed & Pressure)

Enter the fluid density ρ and the pressure P, velocity v and height h at two points along a streamline; the tool applies Bernoulli's equation P + ½ρv² + ρgh = constant to solve for either v₂ or P₂, and reports the dynamic pressure q = ½ρv², the stagnation (total) pressure at each point and the conserved total head. Covers pipe contractions and Venturi meters, Pitot-static tubes, Torricelli's free-jet law and the incompressible-aerofoil pressure-speed relationship. SI units throughout (Pa, m/s, m, kg/m³); g defaults to 9.806 65 m/s² (the SI-exact CODATA 2018 value).

Point 1 (known)
Point 2

Common scenarios (click to load)

Results

Solved variable

Dynamic pressure q₁ = ½ρv₁²

Dynamic pressure q₂ = ½ρv₂²

Stagnation (total) pressure at 1

Stagnation (total) pressure at 2

Conserved total head P + q + ρgh:

Assumptions: steady, incompressible, inviscid flow along a single streamline. Not valid for compressible flow (Mach > 0.3), pumps / turbines or significant friction losses. SI units: pressure Pa, velocity m/s, height m, density kg/m³.

Formula

P₁ + ½ρv₁² + ρgh₁ = P₂ + ½ρv₂² + ρgh₂ v₂ = √( v₁² + 2(P₁ − P₂)/ρ + 2·g·(h₁ − h₂) ) P₂ = P₁ + ½ρ(v₁² − v₂²) + ρg(h₁ − h₂)

Frequently asked

Is aerofoil lift really "just" Bernoulli's effect?

Partly, but it's incomplete. Bernoulli explains *why* a higher-speed flow over the upper surface creates the pressure difference that lifts the wing, but not *why* the upper-surface flow is faster — that requires circulation, the Kutta condition and boundary-layer behaviour, which together are fully described only by Navier–Stokes. Aerospace engineering and NASA's educational material stress that the lift formula L = ½ρv²·S·C_L is *both* a Newtonian momentum result (the wing deflects air downward; reaction force pushes the wing up) and a Bernoulli pressure result — the two are not in opposition.

Why does a tap stream get thinner as it falls — is that Bernoulli?

Yes — it's a classic Bernoulli-plus-continuity example. The water leaves the tap at v₀, then gravity accelerates it to v = √(v₀² + 2gh) after falling h metres. Mass conservation Q = A·v is constant, so A = Q/v must shrink and the stream visibly necks down. If you set "point 1" at the tap exit (v₁ = 1 m/s) and "point 2" 0.2 m below at the same atmospheric pressure, the tool gives v₂ ≈ 2.2 m/s — the cross-section must shrink to v₁/v₂ ≈ 45% of the original.

Why does the calculator sometimes say the solution is imaginary?

It happens when your chosen P₂ (or h₂) is so high that getting from point 1 to point 2 would require *adding* energy, but Bernoulli assumes no external work (no pump, no heating) — so the flow cannot spontaneously accelerate to a real positive v₂. Mathematically v₂² = (...) goes negative and there is no real square root. To fix this: (1) add a pump or fan term (the full energy equation, outside this tool's scope); (2) re-examine the physical setup — the flow may actually be going the other way and you have the points swapped; (3) double-check units, especially pressure (must be in Pa, not mixed Pa / kPa / bar).

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