Calculate the total mechanical energy constant along a fluid streamline. Essential for hydraulics, aerodynamics, and fluid dynamics analysis.
ISO 8601 • Fluid Mechanics • 2024
Pascals (absolute)
flow velocity
elevation above reference
1.225 air (STP), 1000 water
Bernoulli's principle states that the total mechanical energy of a flowing fluid—consisting of pressure energy, kinetic energy, and potential energy—remains constant along a streamline in frictionless, incompressible flow. Mathematically, E = P + ½ρv² + ρgh = constant. This elegant relationship reveals a profound trade-off: when fluid accelerates (v increases), pressure must decrease to maintain constant total energy. This counterintuitive phenomenon explains phenomena from aircraft lift to the behavior of water jets and explains why fast-moving fluids exert less pressure than slow-moving ones. Bernoulli's equation is valid for inviscid (frictionless), incompressible, steady-state flow along a single streamline.
The three components of Bernoulli's constant represent different forms of mechanical energy. Pressure energy (P) is work per unit volume done by pressure forces. Kinetic energy (½ρv²) represents motion energy proportional to density and velocity squared. Potential energy (ρgh) represents gravitational energy based on elevation. These three terms must sum to the same value at any point along a streamline. In real applications, friction losses (viscous effects) cause the Bernoulli constant to decrease slightly as fluid flows, requiring the extended Bernoulli equation with loss terms. Modern fluid dynamics uses Bernoulli's equation as a foundation for understanding aerodynamic lift, pump design, fluid flow measurement, and countless engineering applications. The principle fails for compressible flows (high-speed gases), turbulent flows with significant energy dissipation, and non-streamline conditions.
Measure Pressure: Obtain the static pressure at a point along the streamline in Pascals (Pa). Use a pressure transducer or gauge. Ensure you're measuring absolute pressure, not gauge pressure (gauge + 101325 Pa = absolute for sea level).
Determine Flow Velocity: Calculate or measure the velocity at that point in m/s. For pipe flow, velocity = flow rate / cross-sectional area. Use pitot tubes or velocity meters for direct measurement.
Record Elevation: Measure or establish the height of the point above a reference level (usually ground or pump inlet) in meters. This represents gravitational potential energy contribution.
Identify Fluid Density: Use the correct fluid density in kg/m³. Air at sea level: 1.225 kg/m³. Water at 20°C: 1000 kg/m³. Density varies with temperature and pressure, which affects energy calculations.
Apply Formula: Calculate E = P + ½ρv² + ρgh. The result is total mechanical energy per unit volume (J/m³ or Pa). Verify this constant at other points on the same streamline for consistency.
Bernoulli's equation assumes: (1) Inviscid flow (no friction), (2) Incompressible flow (constant density), (3) Steady flow (no time variations), (4) Flow along a streamline. Violations invalidate the constant energy principle.
Scenario: Air flows at 25 m/s at 5 meters elevation in a wind tunnel with absolute pressure 101325 Pa. Calculate the Bernoulli constant.
Interpretation: This Bernoulli constant (101766.8 Pa ≈ 1.0049 bar) remains the same at all other points along this streamline. If the fluid slows to 10 m/s, pressure must increase. If it rises to 10m, pressure must decrease—always maintaining the constant total energy.
Bernoulli's equation enforces energy conservation. If kinetic energy (½ρv²) increases, the pressure term must decrease to keep total energy constant. This trade-off is fundamental to fluid mechanics and explains lift, jet phenomena, and pressure drop in pipes.
Wing design accelerates air over the upper surface, reducing pressure per Bernoulli's principle. Lower upper pressure compared to lower surface creates net upward force (lift). This pressure difference generates the lift force that supports flight.
Bernoulli's equation requires absolute pressure. Gauge pressure is relative to atmospheric. For sea level: absolute = gauge + 101325 Pa. Using gauge pressure directly produces incorrect results. Always convert to absolute pressure first.
Bernoulli fails for: viscous flows (friction reduces energy), compressible flows (high-speed gases), turbulent flows with energy dissipation, or shock waves. Real-world flows often require extensions of Bernoulli with loss terms.
No—Bernoulli's equation applies along a single streamline. Between streamlines, energy may differ due to turbulence or discontinuities. Each streamline has its own constant.
Density appears in both kinetic and potential energy terms (½ρv², ρgh). Denser fluids have higher energy for the same velocity and height. Water (1000 kg/m³) produces much larger energy terms than air (1.225 kg/m³).
Static pressure (P) is measured in a moving fluid at rest. Total pressure includes static plus dynamic pressure from motion (½ρv²). Bernoulli constant = static pressure + dynamic pressure + potential energy.
Yes—engineers use it to design pump systems, size pipes, calculate nozzle flows, and analyze aircraft aerodynamics. However, real applications add friction loss terms to the basic equation for accuracy.
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