INGENIA

FLD-02

Continuity equation

A₁ v₁ = A₂ v₂. Volume flux is conserved for steady incompressible flow.

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FluidsContinuity

Governing equation

A1v1=A2v2A_1 v_1=A_2 v_2

where

A_1
Area 1 ()
v_1
Speed 1 (m/s)
A_2
Area 2 ()
Q
Discharge (m³/s)
v_2
Speed 2 (m/s)

Lecture brief

Historical brief

Bernoulli, Navier–Stokes, Reynolds (1883) and Stokes drag made continuum flow a dimensionless craft. The sheets compute head, drag, Re and a pedagogical NS snapshot. This sheet (FLD-02 — Continuity equation) is the form associated with Continuity. Working symbols: A1A_1, v1v_1, A2A_2 \rightarrow QQ, v2v_2. Mass conservation in a stream tube. Compressible flow uses ρ A v instead.

Purpose

Purpose: compute QQ, v2v_2 from A1A_1, v1v_1, A2A_2 in Fluid physics via A1v1=A2v2A_1 v_1=A_2 v_2 A₁ v₁ = A₂ v₂. Volume flux is conserved for steady incompressible flow. Use it when a real fluid physics question must be answered in SI before a code check.

Live realistic example

In symbols

Live case. Given A1=0.050m2A_1 = 0.050\,\mathrm{m^{2}}, v1=2.000m/sv_1 = 2.000\,\mathrm{m/s}, A2=0.020m2A_2 = 0.020\,\mathrm{m^{2}}, the governing relation A1v1=A2v2A_1 v_1=A_2 v_2 yields Q=0.1000m3/sQ = 0.1000\,\mathrm{m^{3}/s}, v2=5.000m/sv_2 = 5.000\,\mathrm{m/s}. A narrowing pipe, two area disks, a speeding core. Move a slider: the numbers are this situation, not a canned story.

Calculator

Inputs

Outputs

  • Discharge Q0.1000 m³/s
  • Speed 2 v_25.000 m/s
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FLD-02 · pipe
00:0 / 00:08

Narration of this film

A narrowing pipe, two area disks, a speeding core.

Mass conservation in a stream tube. Compressible flow uses ρ A v instead.

Reading speed

Watch on YouTube