Work and heat transferred in ideal engine

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The discussion focuses on calculating work and heat transferred in an ideal engine operating with one mole of ideal gas through various thermodynamic processes: adiabatic expansion, isothermal compression, and isochoric heating. The initial calculations show that work done during adiabatic expansion is equal to C_V(T1 - T2), while work during isothermal compression is expressed in terms of volume changes. A key point is the efficiency of the engine, derived as η = 1 - (T2 ln(T1/T2))/(T1 - T2). The conversation reveals a correction regarding the terminology used, clarifying that the work done in adiabatic expansion is indeed zero, leading to a resolution of earlier confusion. The thread concludes with a confirmation of the calculations and the efficiency formula.
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[SOLVED] Work and heat transferred in ideal engine

Homework Statement



System is ideal engine containing one mole of ideal gas.

System in initial state P1, V1, T1.
System undergoes free expansion along adiabat to P2, V2, T2.
System undergoes isothermal compression to P3, V3, T3.
System is heated along isochore back to P1, V1, T1.

Give the work and heat for each path in terms of T1, T2, and C_{P}, C_{V} and \gamma. Show that the efficiency of the engine is:

\eta = 1 - \frac{T_{2} ln(T_{1}/T_{2})}{T_{1} - T_{2}}

Homework Equations



From the above we see that V3 = V1 and T3 = T2.
Convention used is dU = dW + dQ

PV = nRT
W = -\int P dV
T_{1}V_{1}^{\gamma - 1} = T_{2}V_{2}^{\gamma - 1}
C_{P} - C_{V} = nR

The Attempt at a Solution



For the first adiabatic path:

Q = 0
W = C_{V}(T_{1} - T_{2})

For the third, isochoral path:

W = 0 since the volume is constant
Q = C_{V}(T_{1} - T_{2})

For the second, isothermal path, well: internal energy is constant, therefore:

W = -Q
W = -\int _{V2} ^{V1} \frac{nRT_{2}}{V} dV<br /> = (C_{P} - C_{V})T_{2} [ln(V_{2}) - ln(V_{1})] = (C_{P} - C_{V})T_{2} ln\left(\frac{V_{2}}{V_{1}}\right)

This is where this gets awkward and I'd appreciate someone checking what I've done. Because I have W in terms of V but I want it in terms of T, I used:

T_{1}V_{1}^{\gamma - 1} = T_{2}V_{2}^{\gamma - 1}
and took the \gamma - 1 root, giving:

T_{1}^{\frac{1}{\gamma - 1}}V_{1} = T_{2}^{\frac{1}{\gamma - 1}}V_{2}

Substituting into by expression for W:

W = (C_{P} - C_{V})T_{2} ln\left(\left(\frac{T_{1}}{T_{2}}\right)^\frac{1}{\gamma - 1}\right)<br /> = (C_{P} - C_{V})T_{2} \frac{ln(T_{1}/T_{2})}{\gamma - 1}

This seems an extreme solution. It also seems wrong since evaluating \eta = \frac{W}{Q} does not give the desired equality. Any obvious errors?

Cheers,

El Hombre
 
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Won't the work done in the free expansion from (P1, V1, T1) to (P2, V2, T2) be 0 by definition? So, while the pressure and the volumes change, the temperature won't.
 
siddharth said:
Won't the work done in the free expansion from (P1, V1, T1) to (P2, V2, T2) be 0 by definition? So, while the pressure and the volumes change, the temperature won't.

Apologies, that should have been 'adiabatic expansion' not 'free expansion'. Turned out my solution was correct: I had stupidly used the net heat instead of the heat in when evaluating the efficiency though, so I thought, as I had expected, my method was wrong. All's well that ends well.

Thanks anyway...

El Hombre
 
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