The Equation of Continuity — Question 3

Section 14-8 · Physics pages 2196–2197

Question 3 A gas can gain volume flow without gaining mass flow A steady gas stream enters a duct at density ρ1 = 2.0 kg/m3, area A1 = 0.010 m2 and mean speed v1 = 12 m/s. It exits at density ρ2 = 1.2 kg/m3 and area A2 = 0.0060 m2. Density and speed are uniform across each section; there is no leak. 1 2 Gas duct schematic; density is specified separately at each section. (a) Find mass flow, exit speed and both volume flow rates. (b) What exit speed would the incompressible formula predict, and why is that wrong here? Does continuity alone explain the density change?
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Question 3 - Solution A gas can gain volume flow without gaining mass flow 1 2 (a) Derivation and calculation ˙m = ρ1A1v1 = (2.0)(.0100)(12) = .240 kg/s . v2 = ˙m ρ2A2 = .240 1.20(.00600) = 33.3333 m/s . Q1 = A1v1 = .120 m3/s , Q2 = ˙m/ρ2 = .200 m3/s . (b) Result and interpretation Ignoring the density change would give v2,wrong = A1v1/A2 = .120/.00600 = 20.0 m/s. ρ1Q1 = ρ2Q2, Q2/Q1 = ρ1/ρ2 = 5/3. Mass flow is conserved while volume flow grows. Continuity alone does not supply the thermodynamics responsible for the density change. Physical check The correct exit mass flow is 1.20(.00600)(33.3333) = .240 kg/s.

Question 3

A gas can gain volume flow without gaining mass flow

A steady gas stream enters a duct at density ρ1=2.0kg/m3\rho_1=2.0\,\mathrm{kg/m^3}, area A1=0.010m2A_1=0.010\,\mathrm{m^2} and mean speed v1=12m/sv_1=12\,\mathrm{m/s}. It exits at density ρ2=1.2kg/m3\rho_2=1.2\,\mathrm{kg/m^3} and area A2=0.0060m2A_2=0.0060\,\mathrm{m^2}. Density and speed are uniform across each section; there is no leak.

Diagram shown in the original SVG worksheet.

  1. Find mass flow, exit speed and both volume flow rates.

  2. What exit speed would the incompressible formula predict, and why is that wrong here? Does continuity alone explain the density change?

Question 3 - Solution

A gas can gain volume flow without gaining mass flow

Diagram shown in the original SVG worksheet.

(a) Derivation and calculation

ṁ=ρ1A1v1=(2.0)(.0100)(12)=.240kg/s.\boxed{\dot m=\rho_1A_1v_1=(2.0)(.0100)(12)=.240\,\mathrm{kg/s}}.v2=ṁρ2A2=.2401.20(.00600)=33.3333m/s.\boxed{v_2=\frac{\dot m}{\rho_2A_2}=\frac{.240}{1.20(.00600)}=33.3333\,\mathrm{m/s}}.Q1=A1v1=.120m3/s,Q2=ṁ/ρ2=.200m3/s.\boxed{Q_1=A_1v_1=.120\,\mathrm{m^3/s}},\quad\boxed{Q_2=\dot m/\rho_2=.200\,\mathrm{m^3/s}}.

(b) Result and interpretation

Ignoring the density change would givev2,wrong=A1v1/A2=.120/.00600=20.0m/s.v_{2,\mathrm{wrong}}=A_1v_1/A_2=.120/.00600=20.0\,\mathrm{m/s}.ρ1Q1=ρ2Q2,Q2/Q1=ρ1/ρ2=5/3.\rho_1Q_1=\rho_2Q_2,\qquad Q_2/Q_1=\rho_1/\rho_2=5/3.Mass flow is conserved while volume flow grows. Continuity alone does not supply the thermodynamics responsible for the density change.

Physical check

The correct exit mass flow is 1.20(.00600)(33.3333)=.240kg/s1.20(.00600)(33.3333)=.240\,\mathrm{kg/s}.