## Bernoulli’s law

Up to now the focus has been fluids at rest. This section deals with fluids that are in motion in a steady fashion such that the fluid velocity at each given point in space is not changing with time. Any flow pattern that is steady in this sense may be seen in terms of a set of streamlines, the trajectories of imaginary particles suspended in the fluid and carried along with it. In steady flow, the fluid is in motion but the streamlines are fixed. Where the streamlines crowd together, the fluid velocity is relatively high; where they open out, the fluid becomes relatively stagnant.

When Euler and Bernoulli were laying the foundations of hydrodynamics, they treated the fluid as an idealized inviscid substance in which, as in a fluid at rest in equilibrium, the shear stresses associated with viscosity are zero and the pressure *p* is isotropic. They arrived at a simple law relating the variation of *p* along a streamline to the variation of *v* (the principle is credited to Bernoulli, but Euler seems to have arrived at it first), which serves to explain many of the phenomena that real fluids in steady motion display. To the inevitable question of when and why it is justifiable to neglect viscosity, there is no single answer. Some answers will be provided later in this article, but other matters will be taken up first.

Consider a small element of fluid of mass *m*, which—apart from the force on it due to gravity—is acted on only by a pressure *p*. The latter is isotropic and does not vary with time but may vary from point to point in space. It is a well-known consequence of Newton’s laws of motion that, when a particle of mass *m* moves under the influence of its weight *m**g* and an additional force *F* from a point P where its speed is *v*_{P} and its height is *z*_{P} to a point Q where its speed is *v*_{Q} and its height is *z*_{Q}, the work done by the additional force is equal to the increase in kinetic and potential energy of the particle—*i.e.,* that

In the case of the fluid element under consideration, *F* may be related in a simple fashion to the gradient of the pressure, and one finds

If the variations of fluid density along the streamline from P to Q are negligibly small, the factor ρ^{−1} may be taken outside the integral on the right-hand side of (131), which thereupon reduces to ρ^{−1}(*p*_{Q} - *p*_{P}). Then (130) and (131) can be combined to obtain

Since this applies for any two points that can be visited by a single element of fluid, one can immediately deduce Bernoulli’s (or Euler’s) important result that along each streamline in the steady flow of an inviscid fluid the quantityis constant.

Under what circumstances are variations in the density negligibly small? When they are very small compared with the density itself—*i.e.,* whenwhere the symbol Δ is used to represent the extent of the change along a streamline of the quantity that follows it, and where *V*_{s} is the speed of sound (see below Compressible flow in gases). This condition is satisfied for all the flow problems having to do with water that are discussed below. If the fluid is air, it is adequately satisfied provided that the largest excursion in *z* is on the order of metres rather than kilometres and provided that the fluid velocity is everywhere less than about 100 metres per second.

Bernoulli’s law indicates that, if an inviscid fluid is flowing along a pipe of varying cross section, then the pressure is relatively low at constrictions where the velocity is high and relatively high where the pipe opens out and the fluid stagnates. Many people find this situation paradoxical when they first encounter it. Surely, they say, a constriction should increase the local pressure rather than diminish it? The paradox evaporates as one learns to think of the pressure changes along the pipe as cause and the velocity changes as effect, instead of the other way around; it is only because the pressure falls at a constriction that the pressure gradient upstream of the constriction has the right sign to make the fluid accelerate.

Paradoxical or not, predictions based on Bernoulli’s law are well-verified by experiment. Try holding two sheets of paper so that they hang vertically two centimetres or so apart and blow downward so that there is a current of air between them. The sheets will be drawn together by the reduction in pressure associated with this current. Ships are drawn together for much the same reason if they are moving through the water in the same direction at the same speed with a small distance between them. In this case, the current results from the displacement of water by each ship’s bow, which has to flow backward to fill the space created as the stern moves forward, and the current between the ships, to which they both contribute, is stronger than the current moving past their outer sides. As another simple experiment, listen to the hissing sound made by a tap that is almost, but not quite, turned off. What happens in this case is that the flow is so constricted and the velocity within the constriction so high that the pressure in the constriction is actually negative. Assisted by the dissolved gases that are normally present, the water cavitates as it passes through, and the noise that is heard is the sound of tiny bubbles collapsing as the water slows down and the pressure rises again on the other side.

Two practical devices that are used by hydraulic engineers to monitor the flow of liquids though pipes are based on Bernoulli’s law. One is the venturi tube, a short length with a constriction in it of standard shape (see Figure 5A), which may be inserted into the pipe proper. If the velocity at point P, where the tube has a cross-sectional area *A*_{P}, is *v*_{P} and the velocity in the constriction, where the area is *A*_{Q}, is *v*_{Q}, the continuity condition—the condition that the mass flowing through the pipe per unit time has to be the same at all points along its length—suggests that ρ_{P}*A*_{P}*v*_{P} = ρ_{Q}*A*_{Q}*v*_{Q}, or that *A*_{P}*v*_{P} = *A*_{Q}*v*_{Q} if the difference between ρ_{P} and ρ_{Q} is negligible. Then Bernoulli’s law indicates

Thus one should be able to find *v*_{P}, and hence the quantity *Q* (= *A*_{P}*v*_{P}) that engineers refer to as the rate of discharge, by measuring the difference of level *h* of the fluid in the two side tubes shown in the diagram. At low velocities the pressure difference (*p*_{P} - *p*_{Q}) is greatly affected by viscosity (see below Viscosity), and equation (135) is unreliable in consequence. The venturi tube is normally used, however, when the velocity is large enough for the flow to be turbulent (see below Turbulence). In such a circumstance, equation (135) predicts values for *Q* that agree with values measured by more direct means to within a few parts percent, even though the flow pattern is not really steady at all.

The other device is the pitot tube, which is illustrated in Figure 5B. The fluid streamlines divide as they approach the blunt end of this tube, and at the point marked Q in the diagram there is complete stagnation, since the fluid at this point is moving neither up nor down nor to the right. It follows immediately from Bernoulli’s law that

As with the venturi tube, one should therefore be able to find *v*_{P} from the level difference *h*.

One other simple result deserves mention here. It concerns a jet of fluid emerging through a hole in the wall of a vessel filled with liquid under pressure. Observation of jets shows that after emerging they narrow slightly before settling down to a more or less uniform cross section known as the vena contracta. They do so because the streamlines are converging on the hole inside the vessel and are obliged to continue converging for a short while outside. It was Torricelli who first suggested that, if the pressure excess inside the vessel is generated by a head of liquid *h*, then the velocity *v* at the vena contracta is the velocity that a free particle would reach on falling through a height *h*—*i.e.,* that

This result is an immediate consequence, for an inviscid fluid, of the principle of energy conservation that Bernoulli’s law enshrines.

In the following section, Bernoulli’s law is used in an indirect way to establish a formula for the speed at which disturbances travel over the surface of shallow water. The explanation of several interesting phenomena having to do with water waves is buried in this formula. Analogous phenomena dealing with sound waves in gases are discussed below in Compressible flow in gases, where an alternative form of Bernoulli’s law is introduced. This form of the law is restricted to gases in steady flow but is not restricted to flow velocities that are much less than the speed of sound. The complication that viscosity represents is again ignored throughout these two sections.