Small pipe break for an ideal gas

AI Thread Summary
The discussion focuses on calculating the flow rate of an ideal gas through a small break in a large tube, where the internal pressure (p1) is significantly higher than the external pressure (p2). The process is identified as adiabatic and isentropic, leading to the assumption that changes in enthalpy and kinetic energy are related. The size of the break is crucial for determining flow rate, and the density can be calculated using the system's total state. Participants emphasize the importance of understanding the nature of gas expansion—whether isothermal or adiabatic—and the relevance of the compressible flow version of Bernoulli's equation. The conversation ultimately seeks to clarify the correct approach to solving the problem.
eXorikos
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Homework Statement


A large tube filled with an ideal gas at pressure p1 and temperature T1 has a small break in it towards an envirronement at p2, with p1 much larger than p2. What is the flow rate through the hole to the outside of the tube.

Homework Equations


pv=rT
Δh+Δc2/2=δq-δl
h1 + c12 = h2 + c22/2

The Attempt at a Solution


The proces is adiabatic and isentropic so Δh+Δc2/2=0
Since it is a large tube it can be presumed that c1=0. Since p2 is much lower than p1 we can presume h2 = 0.

Am I on the right track here?
 
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Is this the exact wording of the problem statement?
 
Yes. Do you need size of the break?
 
eXorikos said:
Yes. Do you need size of the break?
Sure. If the size of the break is zero, then the flow rate is zero.
 
Since the whole exercise is symbolic, let's assume size A which is small. Than the equation I mentioned would give the velocity, we have A and I can find the density using the total state of the system.

Is this correct?
 
eXorikos said:
Since the whole exercise is symbolic, let's assume size A which is small. Than the equation I mentioned would give the velocity, we have A and I can find the density using the total state of the system.

Is this correct?
What makes you think that h2 can be taken as zero? Are you familiar with the compressible flow version of the Bernoulli equation? Do you think that the gas in the tank approaching the exit hole will be experiencing something close to (a) isothermal expansion or (b) adiabatic expansion? Do you think that the gas flow will be close to reversible expansion or no?
 
Good points. Than I have no idea on how to approach this problem.

Can you point me into a direction?
 
My leading questions were to get you pointed in the right direction. Here's another hint: for the flow approaching the exit hole in the tank,
$$dh=-vdv$$
 
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