Thermodynamic Problem: Ideal Gas Expansion and Work Calculation

In summary: In the next question they've put final pressure equal to pext.In summary, the final pressure of the gas can be wrong in the calculation of the work done.
  • #1
mooncrater
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Homework Statement


Two moles of an ideal mono atomic gas (C2=12. 55 JK-1mol-1) expands irreversibly and adiabatically from an initial pressure of 10 atm against a constant external pressure of 1 atm until the temperature drops from the initial value of 325 K to a final temperature of 275 K. Calculate the work done by the gas and its final volume.

Homework Equations


W=-Pext[Vf-Vi]---(1)
PV=nRT -----(2)

The Attempt at a Solution


work done can be found easily
W=-pext (ΔV)
=-1255 J
And V 1 can be found by the ideal gas equation.
BUT, there are two ways to find V2 : that is by ideal gas equation and by the work equation ( by putting the value of V 1 in it ).
Both these method give different values of final volume. Which method is wrong here? And why?
 
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  • #2
Nope that is not the work done by the gas, because the pressure of the gas does not remain constant and equal to pext as you assume. Use the given fact that the expansion is adiabatic to calculate the work from the 1st law.
 
  • #3
BUT for an IRREVERSIBLE process there is a same formula W=-Pext[ΔV] for both irreversible isothermic and irreversible adiabatic processes. From what I know you must be talking about the formula used in the reversible adiabatic process.
 
  • #4
I am not sure if this formula is correct for all irreversible adiabatic processes. Well if your book mentions clearly that this is the case then i guess you should use it to get the final volume, now that i think of it it is unclear what the final pressure of the gas is , so you just can't use the ideal gas eq.
 
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  • #5
Actually, your result for the work done is correct. Since the process is adiabatic, the change in internal energy is equal to minus the work done on the surroundings:
$$ΔU=(2)(12.55)(275-325)=-1255 J$$
The work done on the surroundings is, as you correctly calculated, ##W=P_{ext}(V_f-V_i)=1255 J##. (I assume you are using the sign convention where the work done by the surroundings on the system is W, while I am using the sign convention where the work done by the system on the surroundings is W).

So, there is no inconsistency. The work you calculated from each of the two equations matches.

Chet
 
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  • #6
Delta² said:
I am not sure if this formula is correct for all irreversible adiabatic processes.
Not only is this equation correct for all irreversible adiabatic processes. It is correct for all processes.

Chet

Edit: Actually, what I meant to say is the dW=PextdV for all processes. For reversible processes, Pext=P, where P is the equilibrium pressure of the gas.
 
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  • #7
Chestermiller said:
Not only is this equation correct for all irreversible adiabatic processes. It is correct for all processes.

Chet

Ok maybe i am going to sound dumb but why is this. Is it just the definition of work on the boundary and that the fact that external pressure remains constant?
 
  • #8
Chestermiller said:
The work you calculated from each of the two equations matches.
Yes it matches BUT the problem I am facing is with the final volume(as I said in the question). Do I have to use this work method or the ideal gas equation to find it cause they both are giving different values of final volume.
 
  • #9
When you use the ideal gas equation what final pressure of gas you use ? do you use [itex]p_f=p_{ext}=1atm[/itex]? I think the problem doesn't imply that the final pressure of gas equals [itex]p_{ext}[/itex]
 
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  • #10
Yeah... it never said that final pressure is equal to pext... but many a times we use ideal gas equation inside this work equation to get temperatures. And there we consider pext
as the final pressure of the gas. Like:
W=Pext[V2-V1]
Which is many times written as:
W=P2[nR T2/P2 -nRT1 /P1]
Which I have seen and used in many questions.
 
  • #11
i just don't think in this case the final pressure is 1atm.

Because if it is then if you use it in conjuction with the ideal gas equation (and we know the ideal gas equation is correct no doubt about that) you get different value for the final volume than that of the value you get from the equation for work. So either the final pressure is not 1atm, or the equation for work is not correct. But Chet strongly agrees that your equation for work is correct, which leave us only one option that the final pressure is not 1atm.
 
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  • #12
You are right. It is the final pressure that can be wrong here as no other thing can be wrong. But why?
I am uploading pics of this question and the next one in which they've put final pressure equal to the external pressure.
RA7M0a8TYaCeJR38WQeBJ3U5.jpg
b16TEAe5QE1KdNTA62FD7LhM.jpg
 
  • #13
yes in the example (33) it says among others "until it is in equilibrium with a constant external pressure". This statement essentialy means that [itex]P_f=P_{ext}[/itex]. In the example (32) there is no such statement, it just says "till the temperature drop to 275K".
 
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  • #14
Okay...! Now it's clear to me... in the example 32 the pressure may lie between anything from 10 atm to 1 atm... whereas in the 33 rd example it is given that the equilibrium pressure is equal to external pressure therefore in that we can say that external pressure = final pressure but not for the 32nd example. Now I get it. Thanks for your guidance :).
 
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  • #15
Delta² said:
Ok maybe i am going to sound dumb but why is this. Is it just the definition of work on the boundary and that the fact that external pressure remains constant?
It's not what I would call the definition. It's just the force exerted by the gas on the surroundings times the displacement. That's what we always call the mechanical work. dW = PextdV=(F/A)(Adx)
 
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  • #16
Delta² said:
When you use the ideal gas equation what final pressure of gas you use ? do you use [itex]p_f=p_{ext}=1atm[/itex]? I think the problem doesn't imply that the final pressure of gas equals [itex]p_{ext}[/itex]
Good point. During the time that the expansion is occurring, the external force per unit area is held at 1 atm. After the piston is stopped, if the gas volume does not correspond to the volume that would be obtained from the ideal gas law at 1 atm and the final specified temperature, then the gas will re-equilibrate at a different final pressure, corresponding to the final volume and the specified final temperature.

Chet
 
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  • #17
mooncrater said:
Yeah... it never said that final pressure is equal to pext... but many a times we use ideal gas equation inside this work equation to get temperatures. And there we consider pext
as the final pressure of the gas. Like:
W=Pext[V2-V1]
Which is many times written as:
W=P2[nR T2/P2 -nRT1 /P1]
Which I have seen and used in many questions.
Yes. This is what you get when the gas is allowed to expand all the way to the point where its final equilibrium pressure equals the constant pressure imposed during the irreversible expansion.

Chet
 
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What is thermodynamics?

Thermodynamics is the branch of physics that deals with the relationships between heat, work, temperature, and energy. It studies the behavior of systems that involve the transfer of energy as heat and work.

What is an ideal gas?

An ideal gas is a theoretical gas composed of a large number of randomly moving point particles that do not interact with each other. It follows the ideal gas law, which relates the pressure, volume, temperature, and number of moles of an ideal gas.

What is an expansion in thermodynamics?

An expansion in thermodynamics is when a system changes in volume due to a change in its internal energy. This can occur through various processes, such as isothermal, adiabatic, or isobaric expansions.

How do you calculate work in thermodynamics?

The work done by a thermodynamic system is equal to the force applied multiplied by the distance moved in the direction of the force. In an ideal gas expansion, the work can be calculated using the formula W = -PΔV, where P is the external pressure and ΔV is the change in volume.

What is the first law of thermodynamics?

The first law of thermodynamics, also known as the law of conservation of energy, states that energy cannot be created or destroyed, only transferred or converted from one form to another. This law is the basis for understanding energy flow in thermodynamic systems.

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