Calculating Work in Isothermal Processes of Carnot Cycle

In summary: That is, it shows that the product of entropy change and temperature change is a function of state, so that the entropy change is a function of state. The fact that this function of state has the expression \frac{Q}{T} is a consequence of the Second Law.[The last paragraph is my impression of what is going on. I am not an expert in this area. Corrections are welcome.]In summary, the conversation discussed the Carnot Cycle and calculating work done in isothermal processes. The equations for isothermal work were given and it was explained how to calculate work in adiabatic processes. The question of why the ratio of volumes in isothermal processes is equal to the ratio in adiabatic processes was also
  • #1
Abigale
56
0
Hallo,

I read about thr Carnot-Cycle and got a problem.

A->B: isothermal
B->C: adiabatic
C->D: isothermal
D->A: adiabatic


I want to understand how to calculate the work done in the isothermal processes.
I have read:

[itex]
W_{AB}= T_{H}Nk\ln{(\frac{V_{A}}{V_{\text{B}}})}\\

W_{CD}= -T_{n}Nk\ln{(\frac{V_{A}}{V_{\text{B}}})}
[/itex]

But if i callculate i get:
[itex]
W_{CD}= -T_{n}Nk\ln{(\frac{V_{D}}{V_{C}})}
[/itex]

So the question is, why is:
[itex]
(\frac{V_{A}}{V_{\text{B}}}) = (\frac{V_{D}}{V_{C}})
[/itex] ?

Thx
Abbigale :wink:
 
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  • #3
Abigale said:
Hallo,

I read about thr Carnot-Cycle and got a problem.

A->B: isothermal
B->C: adiabatic
C->D: isothermal
D->A: adiabatic


I want to understand how to calculate the work done in the isothermal processes.
I have read:

[itex]
W_{AB}= T_{H}Nk\ln{(\frac{V_{A}}{V_{\text{B}}})}\\

W_{CD}= -T_{n}Nk\ln{(\frac{V_{A}}{V_{\text{B}}})}
[/itex]

But if i callculate i get:
[itex]
W_{CD}= -T_{n}Nk\ln{(\frac{V_{D}}{V_{C}})}
[/itex]

So the question is, why is:
[itex]
(\frac{V_{A}}{V_{\text{B}}}) = (\frac{V_{D}}{V_{C}})
[/itex] ?
Abigale,

From the first law we know that ΔU + W = Q where W is the work done BY the gas. But since ΔU = 0 in one complete cycle, W = Q = heat flow in from hot register - heat flow out to cold register = |Qh| - |Qc|. Heat flow occurs only from A-B and C-D, so the difference in these heat flows is the work done for the entire cycle. That means the work done in the adiabatic parts nets out to 0.

The efficiency is:

[tex]\eta = 1 - \frac{|Q_c|}{|Q_h|} = 1 - \frac{T_cNk\ln\left(\frac{V_D}{V_C}\right)}{T_hNk\ln\left(\frac{V_A}{V_B}\right)}[/tex]

But we also know that for a Carnot cycle:

ΔS = Qh/Th + Qc/Th = 0 so |Qc/Qh| = Tc/Th

This necessarily means that [itex](\frac{V_{A}}{V_{\text{B}}}) = (\frac{V_{D}}{V_{C}})
[/itex]

AM
 
  • #4
Hey,
but is it possible to schow the Relation, just by looking at the pv-diagram?
 
  • #5
Abigale said:
Hey,
but is it possible to show the Relation, just by looking at the pv-diagram?
Yes, if the PV graph showed the scale.

AM
 
  • #6
The equations you give for isothermal work are for an ideal gas.

Since we're dealing with an ideal gas we can use the adiabatic equations for an ideal gas, for BC and DA.

So [itex]p_B V_B^{\gamma} = p_C V_C^{\gamma}[/itex]

and [itex]p_A V_A^{\gamma} = p_D V_D^{\gamma} [/itex]

dividing: [itex] \frac{p_B}{p_A} \frac{V_B^{\gamma}}{V_A^{\gamma}} = \frac{p_C}{p_D} \frac{V_C^{\gamma}} {V_D^{\gamma}}[/itex]

But for the isothermals: [itex]\frac{p_B}{p_A} = \frac{V_A}{V_B}[/itex] and [itex]\frac{p_C}{p_D} = \frac{V_D}{V_C}.[/itex]

We can now eliminate the pressure ratios from the previous equation, giving...

[itex] \frac{V_B^{\gamma - 1}}{V_A^{\gamma - 1}} = \frac{V_C^{\gamma - 1}} {V_D^{\gamma - 1}}[/itex]

So [itex] \frac{V_B}{V_A} = \frac{V_C} {V_D}[/itex]
 
  • #7
Philip Wood said:
The equations you give for isothermal work are for an ideal gas.

Since we're dealing with an ideal gas we can use the adiabatic equations for an ideal gas, for BC and DA.

So [itex]p_B V_B^{\gamma} = p_C V_C^{\gamma}[/itex]

and [itex]p_A V_A^{\gamma} = p_D V_D^{\gamma} [/itex]

dividing: [itex] \frac{p_B}{p_A} \frac{V_B^{\gamma}}{V_A^{\gamma}} = \frac{p_C}{p_D} \frac{V_C^{\gamma}} {V_D^{\gamma}}[/itex]

But for the isothermals: [itex]\frac{p_B}{p_A} = \frac{V_A}{V_B}[/itex] and [itex]\frac{p_C}{p_D} = \frac{V_D}{V_C}.[/itex]

We can now eliminate the pressure ratios from the previous equation, giving...

[itex] \frac{V_B^{\gamma - 1}}{V_A^{\gamma - 1}} = \frac{V_C^{\gamma - 1}} {V_D^{\gamma - 1}}[/itex]

So [itex] \frac{V_B}{V_A} = \frac{V_C} {V_D}[/itex]
It might be easier to use the adiabatic condition in terms of temperature and volume:

[itex]TV^{\gamma - 1} = K[/itex] from which it is apparent that adiabatic paths between the same two temperatures result in the same proportional changes in volume.

AM
 
  • #8
Much neater – if you can remember TVγ-1 = K. [Though, I suppose TVanything = K would suffice!]

We've got to be careful of the logic here. OP's argument leads to [itex]\left| \frac{Q_{AB}}{Q_{CD}} \right| = \frac{T_{AB}}{T_{CD}}[/itex]. The temperatures which appear in this equation are (in my interpretation of the above argument) ideal gas scale temperatures, effectively defined by pV = nRT. But the Second Law leads to a definition of thermodynamic temperature based on Carnot cycles for any working substance (not just an ideal gas) that is essentially [itex]\frac{T_{AB}}{T_{CD}} = \left| \frac{Q_{AB}}{Q_{CD}} \right| [/itex]. Hence the OP's argument shows the equivalence of the thermodynamic scale and the ideal gas scale.
 
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