Find Mass Flow Rate and the Exit Flow Area

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Northbysouth
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Homework Statement


Air enters aone-inlet, one-exit contreol volume at 6 bar, 500K and 30m/s through a flow area of 28cm3. At the exit the pressure is 3 bar, the temperature is 456.5 K and the velocity is 300 m/s. The air behaves as an ideal gas. For steady state operation determine

a) the mass flow rate, in kg/s
b) the exit flow area, in cm3


Homework Equations



m' = dm/dt = ρvA

The Attempt at a Solution



I have the area of the cross section, A, and the velocity at both ends, but I'm not sure about the ρ.

Can I use:

ρ = p/RT to find the air density?
 
on Phys.org
I've managed to find the mass flow rate, using the density equation given above, I found the air density and then plugged this number into m' =ρvA

m' = (4.1803 kg/m3)(30 m/s)(28cm2)

m' = 0.351 kg/s

Does the mass flow rate stay constant? Can I rework these equations to find the Exit flow area?
 
Northbysouth said:
Does the mass flow rate stay constant?
Mass is a a conserved quantity. In steady state, the mass within the volume is neither increasing nor decreasing, so the mass flow rate in must equal the mass flow rate out.