Efficiency of an imaginary ideal-gas engine cycle

In summary, the student attempted to solve an equation for the thermal efficiency of an engine performing the Joule cycle, but was not successful. Instead, they used the adiabatic condition and found the work done. They then used the equation for efficiency to determine the temperatures in terms of P and V.
  • #1
Jacobpm64
239
0

Homework Statement


The figure represents a simplified PV diagram of the Joule ideal-gas cycle. All processes are quasi-static, and [tex] C_P[/tex] is constant. Prove that the thermal efficiency of an engine performing this cycle is
[tex] \eta = 1 - \gamma \frac{\frac{V_{1}}{V_{2}} - 1}{\frac{P_{3}}{P_{2}} - 1}[/tex]
http://img134.imageshack.us/img134/4534/thermo3eo8.jpg
http://g.imageshack.us/img134/thermo3eo8.jpg/1/

Homework Equations


[tex] PV = RT [/tex]
[tex] \gamma = \frac{C_P}{C_V} [/tex]
[tex] dE = dq + dw [/tex] (should have strokes through the d's on dq and dw, but I don't know how to latex inexact differentials)
[tex] \eta = \frac{|W|}{|q_{in}|} [/tex]
On adiabatic processes,
[tex] TV^{\gamma - 1} = [/tex] constant
[tex] PV^{\gamma} = [/tex] constant


The Attempt at a Solution


First of all, [tex] \eta = \frac{|W|}{|q_{in}|} [/tex]

1->2
We have [tex] dP = 0 [/tex] and [tex] P = constant [/tex]
[tex] W = \int^{V_{2}}_{V_{1}} dV [/tex]
[tex] W = -P_{2} (V_{2} - V_{1}) [/tex]
Since this is an ideal gas, we know:
[tex] dq = C_{P} dT [/tex]
Therefore,
[tex] q = C_{P} (T_{2} - T{1}) [/tex]


2->3
We have [tex] dV = 0 [/tex] and [tex] dw = 0 [/tex] since the process is isochoric.
Therefore,
[tex] dE = dq [/tex]
Since this is an ideal gas [tex] dE = C_{V} dT [/tex]
Therefore,
[tex]dq = C_{V} dT [/tex]
[tex] q = C_{V} (T_{3} - T{2}) [/tex]
By hypothesis,
[tex] w = 0 [/tex]

3->1
This is an adiabatic process, so [tex] dq = 0 [/tex]
Therefore,
[tex] dE = dw [/tex]
Since this is an ideal gas [tex] dE = C_{V} dT [/tex]
Therefore,
[tex] W = \int^{T_{1}}_{T_{3}} C_{V} dT [/tex]
[tex] W = C_{V} (T_{1} - T_{3}) [/tex]
Also, by hypothesis,
[tex] q = 0 [/tex]

Plugging all this into the equation for [tex] \eta [/tex], we get:
[tex] \eta = \frac{P_{2} (V_{2} - V_{1} ) - C_{V} (T_{1} - T_{3})}{C_{P} (T_{2} - T_{1}) + C_{V} (T_{3} - T_{2})} [/tex]

Now, I don't know how to manipulate this to get it in the form that the problem asked for.

Any help would be greatly appreciated. Thanks.
 
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  • #2
Your solution does not provide a solution for T1.

The key here is the adiabatic condition:

[tex]PV^\gamma = K[/tex]

Try applying the adiabatic condition to find the work done from 3 to 1.

AM
 
  • #3
Sorry to revive a dead thread but I still can't figure it out.
 
  • #4
belalegosi said:
Sorry to revive a dead thread but I still can't figure it out.

Sorry to do likewise but I'm in the same boat.
 
  • #5
You'll need to show how far you got with solving the problem before you can receive help. That's our forum policy, and the reason why belalegosi got no help last March.
 
  • #6
In looking at this again, there is a much easier approach than the one taken by the original poster. You do not need to use the adiabatic condition at all. You don't have to calculate the work done either. Just the heat flows. Use the expression for efficiency in terms of Qin and Qout only.

Qin and Qout can be determined as the OP has done. That will give you an expression for efficiency involving T1, T2 and T3. Then use the ideal gas equation to work out expressions for the temperatures in terms of P and V.

AM
 
  • #7
Jacobpm64 said:
1
Plugging all this into the equation for [tex] \eta [/tex], we get:
[tex] \eta = \frac{P_{2} (V_{2} - V_{1} ) - C_{V} (T_{1} - T_{3})}{C_{P} (T_{2} - T_{1}) + C_{V} (T_{3} - T_{2})} [/tex]

.


You need only the absorbed heat in the denominator, Cv(T3-T2).

PV =RT and R = Cp-Cv.

ehild
 
  • #8
Jacobpm64 said:
Plugging all this into the equation for [tex] \eta [/tex], we get:
[tex] \eta = \frac{P_{2} (V_{2} - V_{1} ) - C_{V} (T_{1} - T_{3})}{C_{P} (T_{2} - T_{1}) + C_{V} (T_{3} - T_{2})} [/tex]
As ehild has pointed out, the denominator is Qin which does not include [itex]Q_{1-2}[/itex]. The latter represents the heat flow out of the system.

To find the efficiency, use [tex]\eta = W/Q_{in} = \frac{Q_{in} - Q_{out}}{Q_{in}} = 1 - \frac{Q_{out}}{Q_{in}}[/tex]

In this case [itex]Q_{in}[/itex] is the heat flow from 2-3 and [itex]Q_{out}[/itex] is the heat flow from 1 to 2. Using the ideal gas law to put T1/T2 in terms of V1/V2 and T3/T2 in terms of P3/P2.

AM
 
Last edited:

What is the efficiency of an imaginary ideal-gas engine cycle?

The efficiency of an imaginary ideal-gas engine cycle is defined as the ratio of the work output to the heat input. It is a measure of how well the engine converts heat energy into mechanical work.

How is the efficiency of an imaginary ideal-gas engine cycle calculated?

The efficiency of an imaginary ideal-gas engine cycle can be calculated using the Carnot efficiency formula, which is (T1-T2)/T1, where T1 is the temperature of the heat source and T2 is the temperature of the heat sink.

What factors affect the efficiency of an imaginary ideal-gas engine cycle?

The efficiency of an imaginary ideal-gas engine cycle is affected by several factors, including the temperature of the heat source and heat sink, the compression ratio, and the type of gas used in the cycle.

Is the efficiency of an imaginary ideal-gas engine cycle always the same?

No, the efficiency of an imaginary ideal-gas engine cycle can vary depending on the specific conditions of the cycle. It is also limited by the Carnot efficiency, which is the maximum efficiency that can be achieved for a given temperature difference between the heat source and sink.

How does the efficiency of an imaginary ideal-gas engine cycle compare to real-world engines?

The efficiency of an imaginary ideal-gas engine cycle is a theoretical concept and is often used as a benchmark for comparing the efficiency of real-world engines. However, due to various limitations and inefficiencies, real-world engines typically have lower efficiencies than the theoretical maximum of an imaginary ideal-gas engine cycle.

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