Calculate Bernoulli's Equation Calculator

Enter your engineering parameters below to compute verified physical and mathematical metrics.

Static pressure at station 1 in Kilopascals (e.g. 200 kPa).
Fluid velocity at station 1 in meters/second (e.g. 2.0 m/s).
Datum elevation height at station 1 in meters (e.g. 0.0 m).
Fluid velocity at station 2 in meters/second (e.g. 5.0 m/s).
Datum elevation height at station 2 in meters (e.g. 2.0 m).
Incompressible fluid density in kg/m³ (e.g. Water = 1,000 kg/m³).

Calculation Results

Primary Metric Output --
Metric Breakdown 1 --
Metric Breakdown 2 --
Metric Breakdown 3 --
Metric Breakdown 4 --
Metric Breakdown 5 --
Mathematical Standard --

Calculated using verified physical methodology: Bernoulli's Principle: P_2 = P_1 + \1 / 2\rho(v_1^2 - v_2^2) + \rho g(z_1 - z_2)

*Note: Results represent standard engineering estimates. Validate with structural codes (AISC, Eurocode) or laboratory test measurements for mission-critical applications.

Quick Summary

The Bernoulli's Equation Calculator applies the conservation of energy principle for frictionless, incompressible streamline flow ($P_1 + \1 / 2\rho v_1^2 + \rho g z_1 = P_2 + \1 / 2\rho v_2^2 + \rho g z_2$), computing downstream static pressure ($P_2$) across SI and Imperial units.

Formula Explanation

Bernoulli's Principle: P_2 = P_1 + \1 / 2\rho(v_1^2 - v_2^2) + \rho g(z_1 - z_2)
Total Head: H = \P / \rho g + \v^2 / 2g + z = \text{constant}

How It Works

The Bernoulli's Equation Calculator balances static pressure energy ($P$), dynamic kinetic energy density ($\1 / 2\rho v^2$), and gravitational potential energy density ($\rho g z$) between two points on a fluid streamline. It computes the resulting downstream static pressure ($P_2$) as fluid velocity and pipe elevation change.

Step-by-Step Worked Example

Practical Problem: Water ($\rho = 1,000\text{ kg/m}^3$) enters a Venturi nozzle at $P_1 = 200\text{ kPa}$, $v_1 = 2.0\text{ m/s}$, $z_1 = 0\text{ m}$. It accelerates to $v_2 = 5.0\text{ m/s}$ while rising to an elevation $z_2 = 2.0\text{ m}$. Calculate downstream pressure $P_2$.

  1. Step 1: Identify Input Variables: $P_1 = 200,000\text{ Pa}$, $v_1 = 2.0\text{ m/s}$, $z_1 = 0\text{ m}$, $v_2 = 5.0\text{ m/s}$, $z_2 = 2.0\text{ m}$, $\rho = 1,000\text{ kg/m}^3$.
  2. Step 2: Calculate Dynamic Pressure Change: $\Delta P_{dyn} = \1 / 2 \rho (v_1^2 - v_2^2) = 0.5 \times 1,000 \times (4 - 25) = -10,500\text{ Pa}$ ($-10.50\text{ kPa}$).
  3. Step 3: Calculate Hydrostatic Elevation Head Pressure Change: $\Delta P_{elev} = \rho g (z_1 - z_2) = 1,000 \times 9.80665 \times (0 - 2) = -19,613.30\text{ Pa}$ ($-19.61\text{ kPa}$).
  4. Step 4: Execute Bernoulli Equation Addition: $P_2 = 200,000 - 10,500 - 19,613.30 = 169,886.70\text{ Pa}$.
  5. Step 5: Convert and Interpret Metric Outputs: Downstream Pressure $P_2 = 169.89\text{ kPa}$. Pressure drop: $30.11\text{ kPa}$. Imperial Pressure: $169.89 \times 0.145038 = 24.64\text{ PSI}$. Downstream Bar Pressure: $1.699\text{ Bar}$.

Real-World Calculation Examples

Scenario 1: Horizontal Venturi Flow Meter

Parameters: $P_1 = 300\text{ kPa}$, $v_1 = 1.0\text{ m/s}$, $z_1 = 0$, $v_2 = 4.0\text{ m/s}$, $z_2 = 0$, $\rho = 1,000\text{ kg/m}^3$

Result: $P_2 = 292.50\text{ kPa}$ (42.42 PSI). Flow nozzle pressure drop.

Scenario 2: Vertical Water Riser Pipe

Parameters: $P_1 = 400\text{ kPa}$, $v_1 = 2.0\text{ m/s}$, $z_1 = 0$, $v_2 = 2.0\text{ m/s}$, $z_2 = 10\text{ m}$, $\rho = 1,000\text{ kg/m}^3$

Result: $P_2 = 301.93\text{ kPa}$ (43.79 PSI). Hydrostatic elevation head pressure loss.

Scenario 3: Aircraft Wing Aerodynamic Lift

Parameters: $P_1 = 101.3\text{ kPa}$, $v_1 = 50\text{ m/s}$ (lower), $z_1 = 0$, $v_2 = 60\text{ m/s}$ (upper), $z_2 = 0$, $\rho = 1.225\text{ kg/m}^3$

Result: $P_2 = 100.63\text{ kPa}$. Pressure difference $\Delta P = 0.67\text{ kPa}$ producing upward lift.

Scenario 4: Fire Hose Spray Nozzle

Parameters: $P_1 = 500\text{ kPa}$, $v_1 = 3.0\text{ m/s}$, $z_1 = 0$, $v_2 = 25.0\text{ m/s}$, $z_2 = 0$, $\rho = 1,000\text{ kg/m}^3$

Result: $P_2 = 192.00\text{ kPa}$ (27.85 PSI). High-velocity nozzle kinetic energy conversion.

Key Benefits of Using This Calculator

Complete Energy Head Balance

Evaluates static pressure, dynamic velocity head, and elevation head simultaneously.

Multi-Pressure Unit Conversion

Outputs static pressure in kPa, Pascals, Bar, and Imperial PSI.

Venturi & Nozzle Flow Analysis

Ideal tool for analyzing Venturi meters, spray nozzles, and piping contraction pressure drops.

100% Free Client-Side Engine

Fast interactive calculations running locally in your browser with zero data transmission.

Frequently Asked Questions (FAQ)

What is Bernoulli's Principle?

Bernoulli's Principle states that an increase in fluid velocity occurs simultaneously with a decrease in static pressure or fluid potential energy.

What assumptions are required for Bernoulli's equation?

Bernoulli's equation assumes steady, incompressible, frictionless (inviscid) flow along a single fluid streamline.

What is static pressure vs dynamic pressure?

Static pressure (P) is fluid thermodynamic pressure; dynamic pressure (0.5 * rho * v²) is kinetic energy per unit volume due to fluid motion.

What is total stagnation pressure?

Stagnation pressure P_total = P_static + 0.5 * rho * v² (the pressure when fluid velocity is brought to rest frictionlessly).

How does a Venturi meter measure flow rate?

A Venturi tube narrows pipe area to increase fluid velocity, measuring the resulting static pressure drop to deduce flow rate.

Why does pressure drop when pipe diameter narrows?

Continuity forces fluid velocity to increase in narrow sections; to conserve total energy, static pressure must drop.

How does elevation change affect fluid pressure?

Climbing upward by elevation z decreases static pressure by rho * g * z (hydrostatic head loss).

What is hydraulic head H?

Total hydraulic head H = P / (rho*g) + v² / (2g) + z, expressing total fluid energy in equivalent meters of liquid column.

Can Bernoulli's equation be applied to real pipe systems with friction?

Real piping requires the extended energy equation: P1/rho*g + v1²/2g + z1 = P2/rho*g + v2²/2g + z2 + h_loss (adding friction head loss h_loss).

How convert kPa to PSI?

Multiply kPa by 0.145038 to obtain PSI (e.g. 100 kPa = 14.50 PSI).