Efficiency of a Simple 3-Stage Ideal Gas Cycle: Analyzing Thermal Efficiency η

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SUMMARY

The discussion centers on the thermal efficiency (η) of a simple 3-stage ideal gas cycle, defined by the equation η=1-γ(V2/V1 -1)/(p2/p1-1). The cycle consists of cooling at constant pressure, heating at constant volume, and adiabatic expansion. Key calculations involve the ideal gas law and the relationship between work done and heat added, emphasizing the importance of using correct signs in thermodynamic equations. Participants highlight potential errors in algebraic manipulation and the need for clarity in defining work done by the gas versus work done on the gas.

PREREQUISITES
  • Understanding of ideal gas laws and equations
  • Familiarity with thermodynamic processes (adiabatic, isochoric, isobaric)
  • Knowledge of heat capacities (C_v and C_p) and their relationship (γ)
  • Basic algebraic manipulation skills for thermodynamic equations
NEXT STEPS
  • Study the derivation of thermal efficiency in ideal gas cycles
  • Learn about the implications of adiabatic processes in thermodynamics
  • Explore the relationship between work done and heat added in thermodynamic cycles
  • Investigate common errors in thermodynamic calculations and how to avoid them
USEFUL FOR

Students and professionals in mechanical engineering, thermodynamics researchers, and anyone interested in understanding the efficiency of thermodynamic cycles.

Toby_phys
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A possible ideal-gas cycle operates as follows:

1. From an initial state (##p_1##, ##V_1##) the gas is cooled at constant pressure to (##p_1##, ##V_2##); Let's call the start and end temperature ##T_1## and ##T_2##

2.The gas is heated at constant volume to (##p_2##, ##V_2##);Lets call the start and end temperature ##T_2## and ##T_3##

3.The gas expands adiabatically back to (##p_1##, ##V_1##). Let's call the start and end temperature ##T_3## and ##T_1##
Assuming constant heat capacities, show that the thermal efficiency η is

$$
\eta=1-\gamma\frac{V_2/V_1 -1}{p_2/p_1-1}
$$Efficiencey is defined as: $$\eta=\frac{W}{Q_h}$$ the work done over the heat entered. The heat enters at stage 2 (and some leaves at stage 1 but that doesn't matter). So I need to find the heat entered at stage 2 and the work done.

**Stage 1:**

From the ideal gas equation we get:
$$
p_1V_1=nRT_1, \ \ \ \ p_2V_2=nRT_2 \implies \frac{T_2}{T_1}=\frac{V_2}{V_1}
$$

The work done is just force times distance which is pressure times change in volume:

$$
\Delta W=-p_1\Delta V=-p_1(V_2-V_1)
$$
**Stage 2:**

It doesn't change in volume and so no work is done. However heat is put into the system, increasing the pressure. We need to find this heat.

##\Delta U= Q_h##

For an ideal gas we have:
$$
\Delta U= C_v\Delta T=C_v(T_3-T_2)
$$

Where ##C_v## is heat capacity at constant volume.

**Stage 3:**

Stage 3 is adiabatic so ##\Delta U=\Delta W=C_v(T_1-T_3)##

We also have, using the ideal gas law:
$$
T_3=\frac{p_2V_2}{p_1V_1}T_1
$$Let us sub this into the efficiency:

$$
\eta=\frac{C_v(T_1-T_3)-p_1(V_2-V_1)}{C_v(T_3-T_2)}
$$

If we get ##T_3## and ##T_2## in terms of ##T_1## and sub these in we get:

$$
\eta=-1-\frac{p_1(V_2-V_1)}{C_vT_1(\frac{p_2V_2}{p_1V_1}-\frac{V_2}{V_1})}
$$
And with the ideal gas law, with ##n=1## for simplicity we get ##T_1=\frac{p_1V_1}{R}##

$$
\implies\eta=-1-\frac{R(V_2/V_1-1)}{C_vT_1(\frac{p_2V_2}{p_1V_1}-\frac{V_2}{V_1})}
$$

##R=C_p-C_v## and ##\gamma=C_p/C_v##

$$
\implies\eta=-1-\frac{(\gamma-1)(V_2/V_1-1)}{C_vT_1(\frac{p_2}{p_1}-1)\frac{V_2}{V_1}}
$$

I have no real clue really if this is right or wrong.
 
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Toby_phys said:
Stage 3 is adiabatic so ##\Delta U=\Delta W=C_v(T_1-T_3)##
How did you get this for an adiabatic process?
 
kuruman said:
How did you get this for an adiabatic process?

##dq=0## for adiabatic process I think
 
Toby_phys said:
Assuming constant heat capacities, show that the thermal efficiency η is

$$
\eta=1-\gamma\frac{V_2/V_1 -1}{p_2/p_1-1}
$$
This can't be correct since it yields ##\eta > 1##. Note ##p_2 > p_1## and ##V_2 < V_1##.
Efficiencey is defined as: $$\eta=\frac{W}{Q_h}$$ the work done over the heat entered.
OK. But ##W## represents the work done by the gas. Later in your work, it looks like you calculate the work done on the gas. This can lead to sign errors.

Let us sub this into the efficiency:

$$
\eta=\frac{C_v(T_1-T_3)-p_1(V_2-V_1)}{C_v(T_3-T_2)}
$$

If we get ##T_3## and ##T_2## in terms of ##T_1## and sub these in we get:

$$
\eta=-1-\frac{p_1(V_2-V_1)}{C_vT_1(\frac{p_2V_2}{p_1V_1}-\frac{V_2}{V_1})}
$$
Looks like maybe you made an error in getting the -1 part of the second equation above. Note that the denominator of the first equation does not cancel the first term of the numerator of the first equation to yield -1.

I think the algebra will be simpler if you use the fact that the work done by the gas during the cycle equals the total heat added during the cycle. (WHY?)

The heat added consists of heat added at constant volume and heat added at constant pressure. So you can write the work as the sum of two terms with the first term involving ##C_V## and the second term involving ##C_P##.

You know that the heat , ##Q_h##, is for the constant volume process and therefore involves ##C_V##. So, when you set up the efficiency, you will find that the ratio of ##C_P## to ##C_V## will pop up in the algebra and that will give you the ##\gamma## factor you need.
 
Last edited:

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