Physics • Fluid Mechanics • Hydrodynamics

Bernoulli's Principle Calculator

Calculate pressure, velocity, and height differences in fluid flow using Bernoulli's equation — with Venturi meter, Torricelli's theorem, and pipe flow analysis.

Fluid Density Presets
Select Calculation Mode

P₁ + ½ρv₁² + ρgh₁ = P₂ + ½ρv₂² + ρgh₂
Enter 5 of the 6 unknowns. Select the variable to solve for.

Solve For
kg/m³
m/s²
Pa
m/s
m
Pa
m/s
m
Step-by-Step Working

What is Bernoulli's Principle?

Bernoulli's Principle states that for an ideal (non-viscous, incompressible) fluid in steady flow, the total mechanical energy per unit volume remains constant along a streamline. This means that where fluid speed increases, pressure decreases, and vice versa. It is derived from the law of conservation of energy applied to fluid flow.

Core Fluid Mechanics Formulas

Bernoulli's Equation — NCERT / JEE Standard
P + ½ρv² + ρgh = constant
P₁ + ½ρv₁² + ρgh₁ = P₂ + ½ρv₂² + ρgh₂
Continuity Equation (Mass Conservation)
A₁v₁ = A₂v₂ = Q  [volume flow rate, m³/s]
Venturi Meter — Flow Rate
Q = A₁A₂ × sqrt(2ΔP / (ρ(A₁² − A₂²)))
Torricelli's Theorem — Speed of Efflux
v = sqrt(2gh)  [h = height of fluid above the orifice]
Dynamic Pressure
q = ½ρv²  [Pascals; converts kinetic energy to pressure form]
SymbolQuantityUnitNotes
PStatic pressurePa (N/m²)Force per unit area by fluid
ρFluid densitykg/m³Water = 1000; Air = 1.225
vFlow velocitym/sMagnitude of fluid velocity
hHeight above datummPotential energy term
gGravitational accelerationm/s²9.8 m/s² on Earth
QVolume flow ratem³/sQ = Av (constant for incompressible flow)
ACross-sectional areaLarger area → slower flow
ΔPPressure differencePaMeasured by manometer in Venturi meter

Key Concepts & Real-World Applications

The Three Energy Terms

Bernoulli's equation is fundamentally an energy conservation equation for fluid flow. Each term has units of pressure (Pa = J/m³):

Energy Density Terms
P               → Static pressure (pressure energy per unit volume)
½ρv²       → Dynamic pressure (kinetic energy per unit volume)
ρgh        → Hydrostatic pressure (potential energy per unit volume)
Aircraft Wing (Aerofoil)

Air flows faster over the curved upper surface of a wing than the flat lower surface. By Bernoulli, higher velocity means lower pressure on top. The pressure difference creates lift force upward.

Venturi Meter

A pipe narrows at the throat (smaller A). By continuity, v increases; by Bernoulli, P decreases. The pressure difference ΔP is measured by a manometer and used to calculate flow rate Q.

Atomizer / Spray Bottle

Fast-moving air across the top of a tube creates low pressure. Liquid rises up the tube and is carried away as a spray. Used in perfume bottles, carburettors, and paint sprayers.

Bunsen Burner

Gas flows rapidly through a narrow nozzle, creating low pressure. This draws air through the side holes by Bernoulli suction. The air-gas mixture creates a clean, hot flame.

Magnus Effect (Spinning Ball)

A spinning ball drags air with it. On one side, ball and air move together (faster); on the other, they oppose (slower). The pressure difference causes lateral deflection — used in swing bowling and free kicks.

Blood Flow in Arteries

At an arterial constriction (stenosis), blood velocity increases and pressure drops. The reduced pressure can cause arterial walls to collapse inward, a real medical concern. Bernoulli's principle helps model this.

Assumptions and Limitations

Bernoulli's equation is valid under specific conditions: (1) Steady flow (velocity at any point doesn't change with time). (2) Incompressible fluid (constant density; valid for liquids and low-speed gases). (3) Non-viscous fluid (no friction losses). (4) Flow along a streamline. Real fluids (water, oil, air at high speed) deviate from ideal Bernoulli behaviour due to viscosity, turbulence, and compressibility.

Solved Examples (NCERT / JEE Level)

Example 01 — Pressure Drop in a Constricted Pipe
Water flows through a horizontal pipe. At point 1 (radius 10 cm), the velocity is 2 m/s and pressure is 2 × 105 Pa. Find the pressure at point 2 where the radius narrows to 5 cm. (ρ = 1000 kg/m³)
By continuity: A₁v₁ = A₂v₂
A₁ = π(0.10)² = 0.03142 m²
A₂ = π(0.05)² = 0.007854 m²
v₂ = A₁v₁ / A₂ = 0.03142 × 2 / 0.007854 = 8 m/s

Bernoulli (horizontal, h₁ = h₂ = 0):
P₂ = P₁ + ½ρ(v₁² − v₂²)
P₂ = 2 × 10&sup5; + ½ × 1000 × (4 − 64)
P₂ = 200000 + 500 × (−60)
P₂ = 200000 − 30000
P₂ = 1.70 × 10&sup5; Pa  |  Pressure drops by 30 kPa where velocity quadruples
Example 02 — Torricelli's Theorem
A large tank holds water with a water level 3.2 m above a small hole at the bottom. Calculate the speed of water emerging from the hole and the time to fall 1 m below the hole. Take g = 10 m/s².
Torricelli's theorem: v = sqrt(2gh)
v = sqrt(2 × 10 × 3.2)
v = sqrt(64)
v = 8 m/s

The water emerges horizontally. Time to fall 1 m:
1 = ½ × 10 × t²
t² = 0.2 → t = 0.447 s

Horizontal distance = v × t = 8 × 0.447 = 3.58 m
Speed of efflux = 8 m/s  |  Horizontal throw distance = 3.58 m in 0.447 s
Example 03 — Venturi Meter Flow Rate
A Venturi meter has inlet diameter 8 cm and throat diameter 4 cm. The pressure difference is 5000 Pa. Find the volume flow rate for water (ρ = 1000 kg/m³).
A₁ = π(0.04)² = 5.027 × 10−3
A₂ = π(0.02)² = 1.257 × 10−3

Q = A₁A₂ × sqrt(2ΔP / (ρ(A₁² − A₂²)))
A₁² = 2.527 × 10−5; A₂² = 1.580 × 10−6
A₁² − A₂² = 2.369 × 10−5
2ΔP / (ρ × ΔA²) = 10000 / (1000 × 2.369 × 10−5) = 421.9
Q = 5.027 × 10−3 × 1.257 × 10−3 × sqrt(421.9)
Q = 6.319 × 10−6 × 20.54 = 1.298 × 10−4 m³/s
Q = 1.30 × 10−4 m³/s = 0.130 L/s = 7.8 L/min

Frequently Asked Questions (FAQs)

Why does pressure decrease when fluid velocity increases? +
This is a consequence of energy conservation. The total energy per unit volume of a fluid (P + ½ρv² + ρgh) must remain constant along a streamline. When velocity (kinetic energy) increases, pressure (pressure potential energy) must decrease to keep the total constant. A familiar analogy: a garden hose — when you partially block the opening (reducing area), water speeds up and you can feel the reduced pressure near the constriction.
What is the continuity equation and why does it matter in Bernoulli problems? +
The continuity equation A₁v₁ = A₂v₂ comes from the conservation of mass. For an incompressible fluid in a pipe, the volume flow rate Q (m³/s) is constant. A narrower pipe (smaller A) forces higher velocity v. The continuity equation is almost always used together with Bernoulli's equation in JEE problems — continuity gives v₂ in terms of v₁, which is then substituted into Bernoulli to find pressures.
What is Torricelli's theorem and how is it derived? +
Torricelli's theorem gives the speed of efflux (outflow) from a hole in a tank: v = sqrt(2gh), where h is the height of the fluid surface above the hole. It is derived by applying Bernoulli's equation between the tank surface (point 1: P = P₀, v ≈ 0, height h) and the hole (point 2: P = P₀, v = efflux speed, height 0). The atmospheric pressures cancel, giving ½ρv² = ρgh, so v = sqrt(2gh). This is analogous to free-fall — the fluid exits at the same speed as an object dropped from height h.
How does a Venturi meter measure flow rate? +
A Venturi meter is inserted into a pipe and has a gradually narrowing throat section. By the continuity equation, fluid speeds up at the throat. By Bernoulli's equation, pressure drops. A manometer measures the pressure difference ΔP between the inlet and throat. Since both the geometry (A₁, A₂) and fluid density (ρ) are known, the flow rate Q can be calculated precisely from Q = A₁A₂ × sqrt(2ΔP / (ρ(A₁² − A₂²))). Venturi meters are widely used in water treatment plants, oil pipelines, and HVAC systems.
Can Bernoulli's equation be applied to air? Does it explain how airplanes fly? +
Yes, Bernoulli's equation applies to air at low speeds (below ~0.3 Mach, where compressibility effects are negligible). The aerofoil (wing) is shaped so air must travel a longer path over the curved upper surface, causing it to speed up relative to the lower surface. By Bernoulli, the faster air on top has lower pressure, creating a net upward lift force. However, the full explanation of aircraft lift also involves the Kutta condition and circulation theory (angle of attack), which go beyond simple Bernoulli in modern aerodynamics.