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Physics · Ch 2 — Mechanical Properties of Fluids

Equation of Continuity

2.8

Equation of Continuity

Consider the steady flow of an incompressible fluid through a flow tube whose cross-sectional area varies along its length. In a steady flow, the velocity of a fluid particle at any given point stays constant over time, though it can certainly vary from one point to another along the tube. Consider two sections of such a flow tube, A1A_1 and A2A_2, where A1A_1 has a larger cross-sectional area than A2A_2; let v1v_1 and v2v_2 be the fluid's speeds at sections A1A_1 and A2A_2 respectively. A fluid particle necessarily has to move faster through the narrower section A2A_2 (where there is less space available) in order to let the particles behind it keep up, and correspondingly slows down again on entering a wider section, where more space becomes available. Since the fluid is incompressible, it cannot simply be squeezed to fit into a narrow region — it must instead speed up there, and slow down in a wider region, to keep the same amount of fluid moving through every cross-section in a given time.

Consider a tube of flow — recalling that all fluid confined to a given flow tube must pass through every cross-section that cuts across the tube, and can neither leave the tube nor enter it from outside. Since matter is neither created nor destroyed anywhere within the region of the tube enclosed between two sections A1A_1 (at a point A) and A2A_2 (at a point B), the mass of fluid contained within this enclosed region must stay constant over time — meaning that whatever mass m of fluid enters through section A1A_1 in a given time, an equal mass m must leave through section A2A_2 in that same time.

Let the fluid crossing section A1A_1 (at point A) have speed v1v_1; in a time interval Δt\Delta t, the mass of fluid entering the tube through this section is ρA1v1Δt\rho A_1 v_1 \Delta t. Similarly, let the fluid crossing section A2A_2 (at point B) have speed v2v_2; in the same time interval Δt\Delta t, the mass of fluid leaving the tube through this section is ρA2v2Δt\rho A_2 v_2 \Delta t. Since the fluid is incompressible, the mass entering at A must equal the mass leaving at B:

ρA1v1Δt=ρA2v2Δt— (2.39)\rho A_1 v_1 \Delta t = \rho A_2 v_2 \Delta t \qquad \text{--- (2.39)}

A1v1=A2v2,i.e.Av=constant— (2.40)\boxed{A_1 v_1 = A_2 v_2}, \quad \text{i.e.} \quad Av = \text{constant} \qquad \text{--- (2.40)} …

Figure 2.33Fig. 2.33: Steady flow fluid — a flow tube with sections EFGH (area A₁, advance v₁Δt at point A) and PQRS (area A₂, advance v₂Δt at point B)
Fig. 2.33 — Fig. 2.33: Steady flow fluid — a flow tube with sections EFGH (area A₁, advance v₁Δt at point A) and PQRS (area A₂, advance v₂Δt at point B)

Drawn by us to help you understand the concept clearly, and verified to make sure it's accurate. For exams, practice from your textbook's own diagram.

What this figure shows. A flow tube, bounded by streamlines, is shown with a wider cross-section A1A_1 (marked by a cross-section EFGH at point A, where fluid enters with speed v1v_1) and a narrower cross-section A2A_2 further along (marked by a cross-section PQRS at point B, where fluid leaves with speed v2v_2). This is the exact geometry used to derive the equation of continuity by equating the mass of fluid entering the tube at A1A_1 during a small time interval Δt\Delta t to the mass leaving at $A …