Modeling air temperature and pressure in an open system (decompressing tank)

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SUMMARY

This discussion focuses on modeling the temperature and pressure changes in an open system involving a tank with a volume of 1320 gallons and a 3-inch diameter exit pipe. The tank is initially at 400°F and 100 psig, and the challenge is to accurately model the decompression process as the tank is allowed to vent. Key concepts include the Joule–Thomson effect and the use of differential equations to describe the mass flow rate out of the tank, which is influenced by pressure and density over time.

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  • Understanding of the Joule–Thomson effect
  • Familiarity with differential equations
  • Knowledge of mass flow rate calculations
  • Basic principles of thermodynamics and gas behavior
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I am trying to determine how to accurately model an open system which includes:

A tank: Volume = 1320 gallons
An exit pipe from tank: Diameter = 3 inches

The tank is compressed from atmospheric conditions to a final pressure of 100 psig. Then the tank is allowed to decompress by opening a valve at the exit (blow down test).

The air in the tank is initially at 400 F and 100 psig.

The temperature in the tank decreases as pressure decreases. How do I model the temperature change in the tank as well as pressure.

Keep in mind choke conditions at the pipe exit. Assume isentropic behavior and perfect insulation. Ignore frictional losses of the exit pipe and bends.

Hope you guys can help me with this. Thanks!


FYI: The problem I am having is that, we known, PV=mRT but the pressure changes with the temperature, but the mass also changes due to decompression (open system).
 
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Joule–Thomson effect on Wikipedia along with the equations
 
There are a couple of different ways to approach the problem, the more accurate of which utilize differential equations. You basically need to look at the mass flow rate out of the tank as a function of pressure, which in turn is a function of time. It isn't straightforward, but it can be done.

The basic form of the relationship would be something like this:
\frac{d}{dt}m(t)=-m_{dot}

Where m.dot is the flow rate out of the orifice, and dependent on p(t) and rho(t).

m_{dot}(t)=C*A*\sqrt{2*\rho(t)*(P_{ambient}-P_{tank}(t))}
 
Oops also noticed this thread is almost a year old and was never followed-up on by the OP. Thanks emerhawk.
 
Yes it has been almost a year since I received a response. If other ideas/ methods keep rolling in, I appreciate them. Thank you.
 
I have encountered a vertically oriented hydraulic cylinder that is designed to actuate and slice heavy cabling into sections with a blade. The cylinder is quite small (around 1.5 inches in diameter) and has an equally small stroke. The cylinder is single acting (i.e. it is pressurized from the bottom, and vented to atmosphere with a spring return, roughly 200lbs of force on the spring). The system operates at roughly 2500 psi. Interestingly, the cylinder has a pin that passes through its...

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