- #1
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.
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.