Nathaniel Cooper Ph.D.
September 19, 2018
Recall that Internal Energy is the sum of molecular kinetic and potential energy.
An ideal gas has no forces acting between molecules - There is no potential energy since:
\[ \vec{F} = -\frac{dU}{dx} \]
If you were to place an ideal gas in an fixed insulated container and allow it to expand.
In such experiments preformed with low density gases, Temperature does remain constant.
In real gases, molecules do apply forces to each other, so there is some potential energy.
Potential Energy increases with distance.
When real gases expand in an insulated, fixed container, Temperature decreases.
Heat capacity for gases is dependent on the conditions in which the heat is added.
In changing the temperature of an ideal gas:
If volume is held constant, the gas does not do work.
If pressure is held constant, the gas does do work.
So heat is split between internal energy, measured by Temperature in an ideal gas, and work:
\[ Q = \Delta U + W \]
We would expect it would take more heat to change temperature if work is done.
\[ dQ = nC_vdT \\ dU = dQ -dW \\ dW = 0 \\ dU = nC_VdT \]
\[ dQ = nC_PdT \\ dW = pdV \\ pV = nRT \rightarrow pdV = nRdT\\ dU = dQ -dW \\ dU = nC_PdT - nRdT \]
We’ve derived \[ dU = nC_VdT \\ dU = nC_PdT - nRdT \\ nC_PdT = nC_VdT + nRdT \\ \boxed{C_P = C_V + R} \]
\(C_P\) is always higher than \(C_V\) by adding R.
Recall that \(C_V\) for mono- , di- , and polyatomic gases are all factors of R for ideal gases.
What are the corresponding \(C_P\)’s?
monoatomic:
\[ C_v = \frac{3}{2}R \\ C_P = \frac{5}{2}R \]
diatomic:
\[ C_v = \frac{5}{2}R \\ C_P = \frac{7}{2}R \]
polyatomic:
\[ C_v = \frac{7}{2}R \\ C_P = \frac{9}{2}R \]
In some situations, the ratio of the \(C_V\) and \(C_P\) heat capacities are needed.
This ratio is called \(\gamma\)
\[ \gamma = \frac{C_P}{C_V} \]
monoatomic:
\[ \gamma = \frac{\frac{5}{2}R}{\frac{3}{2}R} = \frac{5}{3} = 1.67 \]
diatomic:
\[ \gamma = \frac{\frac{7}{2}R}{\frac{5}{2}R} = \frac{7}{5} = 1.4 \]
polyatomic:
\[ \gamma = \frac{\frac{9}{2}R}{\frac{7}{2}R} = \frac{9}{7} = 1.29 \]
The Adiabatic process is an excellent approximation for real process that occur very rapidly, such that the heat exchange is not significant in that time frame.
Recall that for adiabatic processes:
\[ dU = -W \]
\[ dU = -dW \\ nC_VdT = -pdV \\ nC_VdT = -\frac{-nRT}{V}dV \\ \frac{dT}{T} + \frac{R}{C_V}\frac{dV}{V} =0 \\ \frac{R}{C_V} = \frac{C_P -C_V}{C_V} = \frac{C_P}{C_V} -1 = \gamma -1 \\ \frac{dT}{T} + (\gamma -1) \frac{dV}{V} = 0 \]
\[ \int\frac{dT}{T} + \int(\gamma -1) \frac{dV}{V} = \int0 \\ ln(T) + (\gamma -1)ln(V) = constant \\ ln(T) + ln(V^{\gamma -1}) = constant \\ ln(TV^{\gamma -1}) = constant \\ TV^{\gamma -1} = constant \\ \boxed{T_1V_1^{\gamma -1} = T_2V_2^{\gamma -1}} \\ \boxed{p_1V_1^{\gamma} = p_2V_2^{\gamma}} \]
1.00 liter of ideal, monoatomic gas at a temperature of 300. K expands adaibatically to a final volume of 100. l, What is the final temperature?
\[ T_2 = T_1(\frac{V_1}{V_2})^{\gamma-1} \\ T_2 = 300K(\frac{1.00 l}{100l})^{1.67-1} \\ T_2 = 13.9 K \]
If the initial pressure in the above question in 1.0 ATM, what is the final pressure?
\[ p_2 = p_1(\frac{V_1}{V_2})^{\gamma} \\ T_2 = 1ATM(\frac{1.00 l}{100l})^{1.67} \\ T_2 = 4.6\times 10^{-4} ATM \]
\[ W = nC_V(T_1 - T_2) \]
Apply \(pV = nRT\)
\[ W = \frac{C_V}{R} (p_1V_1 - p_2V_2) = \frac{1}{\gamma-1}(p_1V_1 - p_2V_2) \]
Same gas as the previous two problems. How much work does the gas do?
\[ W = \frac{1}{\gamma-1}(p_1V_1 - p_2V_2) \\ W = \frac{1}{0.67}(1.01\times10^5 Pa * 0.001 m^3 - 48.88 Pa *0.100 m^3)\\ W =144 J \]