Bernoulli Equation Calculator
Solve for any unknown in the Bernoulli equation given pressure, velocity, and elevation at two points
This free online bernoulli equation calculator provides instant results with no signup required. All calculations run directly in your browser — your data is never sent to a server. Supports both metric (SI) and imperial units with built-in unit selection dropdowns on every input field, so you can work in whatever units your problem provides. Designed for engineering students and professionals working through coursework, design projects, or quick reference calculations.
Bernoulli Equation Calculator
P₁ + ½ρv₁² + ρgz₁ = P₂ + ½ρv₂² + ρgz₂
v2 — Point 2
14.2023 m/s
Bernoulli Equation
P₁ + ½ρv₁² + ρgz₁ = P₂ + ½ρv₂² + ρgz₂
How to Use This Calculator
Enter your input values
Fill in all required input fields for the Bernoulli Equation Calculator. Most fields include unit selectors so you can work in your preferred unit system — metric or imperial, whichever matches your problem.
Review your inputs
Double-check that all values are correct and that you have selected the right units for each field. Incorrect units are the most common source of calculation errors and can produce results that are off by factors of 2, 10, or more.
Read the results
The Bernoulli Equation Calculator instantly computes the output and displays results with units clearly labeled. All calculations happen in your browser — no loading time and no data sent to a server.
Explore parameter sensitivity
Try adjusting individual input values to see how the output changes. This is a quick and effective way to develop intuition about how different parameters influence the result and to identify which inputs have the largest effect.
Formula Reference
Bernoulli's Equation
P₁ + ½ρV₁² + ρgz₁ = P₂ + ½ρV₂² + ρgz₂
Variables: P = pressure, ρ = fluid density, V = velocity, g = gravitational acceleration, z = elevation
When to Use This Calculator
- •Use the Bernoulli Equation Calculator when solving homework or exam problems that require quick numerical verification of your hand calculations — instant feedback helps identify arithmetic errors before they propagate.
- •Use it during the early design phase to rapidly iterate on parameters and narrow down feasible configurations before committing time to detailed finite element simulations or full design packages.
- •Use it when reviewing a colleague's calculation or checking a vendor's data sheet for plausibility — a quick sanity check can prevent costly downstream errors.
- •Use it to generate reference data for a technical report or presentation without manual computation, ensuring consistent, reproducible numbers throughout the document.
- •Use it in the field when a quick estimate is needed and a full engineering software package is not available.
About This Calculator
The Bernoulli Equation Calculator is a precision engineering calculation tool designed for students, engineers, and technical professionals. Solve for any unknown in the Bernoulli equation given pressure, velocity, and elevation at two points All calculations are performed using established engineering formulas from the relevant scientific literature and standards. Inputs support both metric (SI) and imperial unit systems, with unit conversion handled automatically — simply select your preferred unit from the dropdown next to each field. Results are computed instantly in the browser without sending data to a server, ensuring both speed and privacy. This calculator is intended as a supplementary tool for learning and design exploration; always verify results against authoritative references for safety-critical applications.
The Theory Behind It
Bernoulli's equation expresses conservation of mechanical energy for an incompressible, steady, inviscid, and irrotational flow along a streamline: P + ½ρV² + ρgz = constant, where P is static pressure, ρ is density, V is velocity, g is gravitational acceleration, and z is elevation above a reference datum. The three terms represent pressure energy per unit volume, kinetic energy per unit volume, and potential energy per unit volume. The sum is the total mechanical energy per unit volume, which is constant along a streamline in an ideal fluid with no friction, no heat transfer, and no shaft work. Applying Bernoulli's equation between two points 1 and 2 on the same streamline: P₁ + ½ρV₁² + ρgz₁ = P₂ + ½ρV₂² + ρgz₂. This allows solving for any unknown (pressure, velocity, or elevation) given the other five values. The equation is exact for ideal flow and is a good approximation for real flow at high Re (low viscous effects) and over short distances where friction losses are small. For real flow with friction, head loss h_L is added to the downstream side: P₁/ρg + V₁²/(2g) + z₁ = P₂/ρg + V₂²/(2g) + z₂ + h_L. This form is sometimes called the energy equation and is used in hydraulics for pipe networks and open channels. Bernoulli's equation is one of the most widely applied results in fluid mechanics and is the basis for airspeed indicators (pitot tubes), Venturi flow meters, airfoil lift analysis, and siphon flow.
Real-World Applications
- •Pitot tube airspeed measurement: a pitot tube facing the flow measures stagnation pressure (P + ½ρV²); a static port measures P. The difference is ½ρV², from which velocity is computed: V = √(2·ΔP/ρ). This is the principle behind aircraft airspeed indicators.
- •Venturi flow meter: a Venturi or orifice plate creates a pressure drop at a constriction in a pipe. Bernoulli's equation relates the pressure difference to the velocity at the throat, and from that to the volumetric flow rate.
- •Tank drainage (Torricelli's law): water draining from a tank through a hole in the bottom accelerates to V = √(2gh), where h is the head above the hole. This is Bernoulli's equation applied between the free surface and the hole exit.
- •Airfoil lift analysis: above a wing, air speeds up relative to below, so pressure above is lower than below (Bernoulli). The pressure difference times wing area gives the lift force. This explanation is slightly simplified but captures the essential physics.
- •Water fountain and jet trajectories: the initial velocity of a water jet from a fountain nozzle comes from the pressure head (Bernoulli converting pressure to velocity). Subsequent projectile motion sets the trajectory and height.
Frequently Asked Questions
What is Bernoulli's equation?
P + ½ρV² + ρgz = constant along a streamline in steady, incompressible, inviscid, irrotational flow. It is conservation of mechanical energy per unit volume. Each term has units of pressure: P is pressure energy per volume, ½ρV² is kinetic energy per volume, ρgz is potential energy per volume. The sum is constant, so pressure and velocity trade off along the streamline.
What are the assumptions of Bernoulli's equation?
Four key assumptions: (1) steady flow (not changing with time); (2) incompressible (density constant — valid for liquids and low-Mach-number gases < 0.3); (3) inviscid (no friction); (4) along a streamline (not across different streamlines in general). Real flows violate these to some degree, introducing errors. The equation is exact for ideal flow and a good approximation when viscous losses are small over the distance of interest.
When does Bernoulli's equation fail?
For flows with significant friction (long pipes, rough surfaces), the pressure drop exceeds what Bernoulli predicts — use Darcy-Weisbach for friction losses. For compressible flow (high-speed gas, Mach > 0.3), density changes invalidate the incompressible assumption. For unsteady flows (accelerating or decelerating), an unsteady term must be added. For flows with shaft work (pumps, turbines), energy is added or removed along the path and Bernoulli's equation must include those terms.
How is Bernoulli used to measure velocity?
A pitot tube measures stagnation pressure P_stag = P + ½ρV² (flow is brought to rest at the tube opening). A static port measures the free-stream static pressure P. The difference ΔP = P_stag − P = ½ρV² gives V = √(2ΔP/ρ). This is how aircraft airspeed indicators work. For reliable readings, the static port must be in a location where the flow is approximately undisturbed.
How do I include friction losses?
The modified Bernoulli (or 'energy') equation adds a head loss term: h₁ + V₁²/(2g) + z₁ = h₂ + V₂²/(2g) + z₂ + h_L, where h_L is the total head loss from friction (from Darcy-Weisbach for pipes) and minor losses (fittings, valves, entrances, exits). This form is standard in hydraulics for pipe network analysis and open-channel flow.
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