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Integral continuity for a compressing duct

Short answer

The integral continuity equation states time rate of mass stored plus net outflow equals zero. Mass flow is 1.2*0.020*20=0.48 kg/s; outlet velocity = 0.48/(1.5*0.010)=32 m/s.

State the integral form of the continuity equation for a control volume. Air flows steadily through a duct. At the inlet the area is 0.020 m², density 1.2 kg/m³ and velocity 20 m/s. At the outlet the area is 0.010 m² and the density is 1.5 kg/m³. Find the mass flow rate and the outlet velocity.

Integral form

For a fixed control volume (CV) with control surface (CS):

∂∂t∫CVρ dV+∫CSρ (V⃗⋅n^) dA=0\frac{\partial}{\partial t}\int_{CV}\rho\,dV+\int_{CS}\rho\,(\vec V\cdot\hat n)\,dA=0

The first term is the rate of change of mass stored in the CV; the second is the net mass outflow through the surface. For steady flow the first term is zero, so total mass inflow equals total outflow. For one inlet and one outlet:

ρ1A1V1=ρ2A2V2=m˙\rho_1A_1V_1=\rho_2A_2V_2=\dot m

The integral form is the basis of the finite volume method, since it is applied to each cell. The differential form follows by applying the divergence theorem to a very small volume.

Numerical

Mass flow rate:

m˙=ρ1A1V1=1.2×0.020×20=0.48 kg/s\dot m=\rho_1A_1V_1=1.2\times0.020\times20=0.48\ \text{kg/s}

Outlet velocity:

V2=m˙ρ2A2=0.481.5×0.010=32 m/sV_2=\frac{\dot m}{\rho_2A_2}=\frac{0.48}{1.5\times0.010}=32\ \text{m/s}

Check: halving the area doubles the velocity, while the 1.25 times higher density reduces it by a factor of 1.25, giving a net factor of 1.6: V2=V1×ρ1A1ρ2A2=20×0.0240.015=32V_2=V_1\times\dfrac{\rho_1A_1}{\rho_2A_2}=20\times\dfrac{0.024}{0.015}=32 m/s.

Answer: m˙=0.48\dot m=0.48 kg/s; V2=32V_2=32 m/s.

✓ Answer checked by Claude Opus 5.5 (high effort)

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