Bernoulli's equation, P + ½ρV² + ρgz = constant along a streamline, is an energy balance for steady, incompressible, inviscid flow along a streamline. It states that as fluid speed increases, static pressure decreases, and vice versa — a direct consequence of energy conservation. Bernoulli's equation can also be written as total head H = P/(ρg) + V²/(2g) + z = constant, making it useful for pipe and open-channel analysis.
Apply to venturi tubes, nozzles, and flow over airfoils to see the pressure-velocity tradeoff. Always check whether the assumptions hold (steady, incompressible, along one streamline, inviscid). Practice converting between pressure, velocity, and elevation heads using piezometer readings.
Bernoulli's equation is, at its core, a statement about energy conservation applied to a parcel of flowing fluid. Recall from mechanics that the total mechanical energy of an object is the sum of its kinetic energy, potential energy, and any work done by pressure forces. For a small packet of incompressible, inviscid fluid moving steadily along a streamline, those same three energy contributions appear: the static pressure P (energy per unit volume stored in the pressure field), the kinetic energy per unit volume ½ρV² (where ρ is fluid density and V is speed), and the gravitational potential energy per unit volume ρgz (where z is elevation). Bernoulli's equation says their sum is constant along the streamline: P + ½ρV² + ρgz = constant.
The most important practical consequence is the pressure-velocity tradeoff. If you follow a streamline from a wide pipe section to a narrow one, the continuity equation (which you already know) tells you the fluid must speed up in the narrow section to keep the same volume flow rate passing through. Bernoulli's equation then says that if ½ρV² increases, P must decrease — and it does, measurably so. This is the venturi effect, the physical basis for carburetors, aspirators, and venturi meters. The same principle explains why air moving over the curved top of an airplane wing travels faster (and therefore at lower pressure) than air moving under the flat bottom, generating lift.
Bernoulli's equation is also often written in head form by dividing every term by ρg: P/(ρg) + V²/(2g) + z = H, where H is the total head. This form is convenient because each term has units of meters (or feet), representing an equivalent height of fluid. Pressure head, velocity head, and elevation head sum to a constant total head. Engineers use this form when analyzing pipe systems and comparing readings from piezometers and pitot tubes.
Understanding the assumptions is as important as understanding the equation. The flow must be steady (no time variation), incompressible (no density changes — valid for most liquids and low-speed gases), inviscid (no friction — an idealization), and the equation applies along a single streamline only. Real pipe flows violate the inviscid assumption: friction converts mechanical energy to heat, so total head decreases along the pipe. Real fluids also have turbulence and secondary flows. When these effects matter, you extend Bernoulli into the full energy equation by adding a head loss term h_L on one side, which you will do when you study pipe system losses.
The power of Bernoulli's equation is not that it models every real flow accurately — it does not — but that it identifies the right variables and the right tradeoffs. Every more advanced fluid mechanics topic you encounter, from flow measurement to pump selection to aerodynamics, begins by asking whether Bernoulli applies and, if not, what correction terms are needed.