\documentclass[12pt]{article} %\usepackage{mathptmx} \usepackage{helvet} \usepackage{graphicx} %\usepackage{ngerman} \usepackage[latin1]{inputenc} \usepackage{amsmath} \usepackage{amssymb} \usepackage{amsthm} \usepackage{bm} \usepackage{bbm} \usepackage{a4wide} \newcommand{\tx}[1]{ \mathrm{#1} } \newcommand{\nc}[2]{ #1_\mathrm{#2} } \newcommand{\kb}{ \nc{k}{B} } \newcommand{\diff}[1]{ \, \mathrm{d} #1 \, } \newcommand{\diffm}[2]{ \, \mathrm{d} \mathbf{#1}_{#2} \, } \newcommand{\dr}{ \, \mathrm{d} \mathbf{r}_1 \ldots \mathrm{d} \mathbf{r}_N \, } \newcommand{\var}{ \, \mathrm{var} } \newcommand{\mean}[1]{ \left\langle #1 \right\rangle } \newcommand{\Nq}{ \overline{N} } \newcommand{\pd}[3]{ \left(\frac{\partial #1}{\partial #2} \right)_{#3} } \newcommand{\N}{ \overline{N} } \begin{document} \centerline{\textbf{Lösungen zum Übungsblatt 10} } \vspace{0,5cm} Johannes Dörr, Jan Schumann-Bischoff \hfill Übungsgruppe 2, Jürgen Lampe\\ \mbox{}\hrulefill\\ \vspace {1cm} \textbf{Problem 1: Thermodynamic Relations and Clausius-Clapeyron equation:} \\ \textbf{Tasks:} \begin{itemize} \item[a)] Show the following thermodynamic relation: \begin{equation} \pd{T}{p}{S} = \frac{T}{C_p}\pd{V}{T}{p} \label{eq:relation1} \end{equation} \item[b)] Show the following thermodynamic relation: \begin{equation} \pd{V}{p}{S} = \pd{V}{p}{T} + \frac{T}{C_p} \pd{V}{T}{p}^2 \label{eq:relation2} \end{equation} \end{itemize} \textbf{Methods:}\\ \begin{itemize} \item[a)] We'll show the Maxwell-relation (\textsl{proof 1}): \begin{equation} \pd{T}{p}{S} = \pd{V}{S}{P} \label{eq:maxwell1} \end{equation} and after a few transformations we'll insert it in the definition of the spesific heat by a constant pressure: \begin{equation} C_p := T \pd{S}{T}{p} \label{eq:def_pressure} \end{equation} \item[b)] We concider the functions $f(u,v)$ and $g(u,v)$ and want to prove the following assertions: \begin{itemize} \item[\textsl{2)}] The Jacobians can be simplified as followed \begin{equation} \frac{\partial (f,g)}{\partial (u,g)} = \pd{f}{u}{g} \quad \frac{\partial (f,g)}{\partial (f,v)} = \pd{g}{v}{f} \label{eq:jacobi1} \end{equation} \item[\textsl{3)}] \begin{equation} \pd{S}{p}{T} = -\pd{V}{T}{p} \label{eq:maxwell2} \end{equation} \item[\textsl{4)}] \begin{equation} \pd{f}{u}{v} = -\frac{\pd{f}{v}{u}}{\pd{u}{v}{f}} \label{eq:jacobi2} \end{equation} \item[\textsl{5)}] \begin{equation} \frac{C_p}{C_V} = \frac{\kappa_T}{\kappa_S} \label{eq:cpv} \end{equation} \end{itemize} \end{itemize} \textbf{Results:}\\ \textbf{Appendix:}\\ a) If we multiply \eqref{eq:def_pressure} with $\partial V$ we obtain: \begin{align} \partial V C_p &= T \partial V \pd{S}{T}{p} \notag \\ \Rightarrow \pd{V}{S}{p} &= \frac{T}{C_p} \pd{V}{T}{p} \notag \end{align} With the Maxwell-relation \eqref{eq:maxwell1} prooved in \textsl{proof 1} we obtain our relation \eqref{eq:relation1}: \begin{displaymath} \pd{T}{p}{S} = \frac{T}{C_p}\pd{V}{T}{p} \end{displaymath} \underline{\textsl{proof 1}}: We start with the differential of the enthalpy $H(S,p)$: \begin{displaymath} \diff{H} = T\diff{S} + V \diff{p} \end{displaymath} with the obvios equations: \begin{displaymath} T=\pd{H}{S}{p} \qquad \qquad V=\pd{H}{p}{S} \end{displaymath} Now we use the permutability of differentations: \begin{displaymath} \pd{T}{p}{S} = \frac{\partial^2 H}{\partial p \, \partial S} = \frac{\partial^2 H}{\partial S \, \partial p} = \pd{V}{S}{p} \qed \end{displaymath} b) We start with the definition of the specific heat by a constant temperature and use the relations \eqref{eq:jacobi1}: \begin{align} C_V &:= T \pd{S}{T}{V} = T \cdot \frac{\partial (S,V)}{\partial (T,V)} \notag \\ &= T \cdot \frac{\partial (S,V)}{\partial (T,p)} \frac{\partial (T,p)}{\partial (T,V)} \notag \\ &= T \pd{p}{V}{T}\frac{\partial (S,V)}{\partial (T,p)} \notag \\ &= T \pd{p}{V}{T} \left[ \pd{S}{T}{p}\pd{V}{p}{T} - \pd{S}{p}{T}\pd{V}{T}{p} \right] \notag \\ &= T\pd{S}{T}{p} - T\pd{p}{V}{T}\pd{S}{p}{T}\pd{V}{T}{p} \notag \end{align} With the Maxwell-relation \eqref{eq:maxwell2}, $\alpha := \frac{1}{V} \pd{V}{T}{p}$ and the definition of the isothermal compressibility $\kappa_T := -\frac{1}{V} \pd{V}{p}{T}$ we obtain: \begin{align} C_V &= C_p + T\frac{\pd{V}{T}{p}^2}{\pd{V}{p}{T}} \notag \\ \Rightarrow C_p - C_V &= \frac{T\alpha^2}{\kappa_T} \notag \end{align} With \eqref{eq:cpv} we obtain: \begin{align} \kappa_S &= \kappa_T - \frac{TV\alpha^2}{C_p} \notag \\ \Rightarrow -\frac{1}{V}\pd{V}{p}{S} &= -\frac{1}{V}\pd{V}{p}{T} - \frac{TV\pd{V}{T}{p}^2}{V^2C_p} \notag \\ \Rightarrow \pd{V}{p}{S} &= \pd{V}{p}{T} + \frac{T}{C_p}\pd{V}{T}{p}^2 \notag \end{align} \underline{\textsl{proof 2:}} We also concider the functions $f(u,v)$ and $g(u,v)$. The Jacobian is defined by: \begin{displaymath} \frac{\partial (f,g)}{\partial (u,v)} = \pd{f}{u}{v}\pd{g}{v}{u} - \pd{f}{v}{u}\pd{g}{u}{v} \end{displaymath} Now we set $g=v$. $\pd{v}{u}{v}=0$ and $\pd{g}{v}{u}=1$ is trivial and we obtain: \begin{displaymath} \frac{\partial (f,v)}{\partial (u,v)} = \pd{f}{u}{v} \end{displaymath} With the same argumentation you can find with $f=u$: \begin{displaymath} \frac{\partial (u,g)}{\partial (u,v)} = \pd{g}{v}{u} \quad \qed \end{displaymath} \underline{\textsl{proof 3:}} We concider the potential of the free enthalpy $G(T,p)$ \begin{displaymath} \diff{G} = -S\diff{T} + V \diff{p} \end{displaymath} and find the relations: \begin{displaymath} S=-\pd{G}{T}{p} \qquad \qquad V=\pd{G}{p}{T} \end{displaymath} With the same argumentation as in \textsl{proof 1} we obtain the Maxwell-relation: \begin{displaymath} -\pd{S}{p}{T} = \frac{\partial^2 G}{\partial p \partial T}=\frac{\partial^2 G}{\partial T \partial p} = \pd{V}{T}{p} \qquad \qquad \qed \end{displaymath} \underline{\textsl{proof 4:}} With the use of \textsl{proof 2} we obtain: \begin{displaymath} \pd{f}{u}{v} = \frac{\partial (f,v)}{\partial (u,v)} = \frac{\partial (f,v)}{\partial (f,u)}\frac{\partial (f,u)}{\partial (u,v)} = -\frac{\pd{f}{v}{u}}{\pd{u}{v}{f}} \qquad \qed \end{displaymath} \underline{\textsl{proof 5:}} We start with the entropy $S(V,T)$ and \eqref{eq:jacobi2}: \begin{align} \pd{S}{V}{T} &= \pd{T}{V}{S}\cdot \frac{\pd{S}{V}{T}}{\pd{T}{V}{S}} \notag \\ &= -\pd{T}{V}{S}\pd{S}{T}{V} \notag \\ \Rightarrow -\pd{S}{p}{T} \pd{p}{V}{T} &= \pd{T}{V}{S}\pd{S}{T}{V} \notag \\ \Rightarrow -\frac{\pd{S}{p}{T}}{\pd{T}{p}{S}} \pd{p}{V}{T} &= \pd{T}{V}{S}\pd{p}{T}{S}\pd{S}{T}{V} \notag \\ \Rightarrow \pd{S}{T}{p} \pd{p}{V}{T} &= \pd{p}{V}{S} \pd{S}{T}{V} \notag \\ \Rightarrow -\frac{T}{V}\pd{S}{T}{p} \pd{V}{p}{S} &= -\frac{T}{V}\pd{S}{T}{V} \pd{V}{p}{T} \notag \end{align} With the definitions of the specific heat and the compressibility we obtain: \begin{displaymath} C_p\kappa_S = C_V\kappa_T \qquad \qed \end{displaymath} \newpage \textbf{Problem 2: Solar Cells and Geothermal Energy} \begin{itemize} \item[(a)] The solar constant specifies the average energy, that reaches the surface of the earth averaged per square meter per second, is $1.367\tx{kJm}^{-2}\tx{s}^{-1}$. Since about one third of the arriving energy is reflected, only $I = 0.96\tx{kJm}^{-2}\tx{s}^{-1} \approx 1\tx{kJm}^{-2}\tx{s}^{-1}$ actually reach the surface. Knowing that the radiation's temperature is $T_2 = 6000\tx{K}$ and estimating $T_1 = 290\tx{K}$ on earth, we obtain the Carnot efficiency: \begin{align*} \eta_{\tx{C}} &= \frac{T_2 - T_1}{T_2} = 0.95 \ \ . \end{align*} This means that the maximum power $P_{\tx{max}}$, a $1\tx{m}^2$ solar cell can obtain hypothetically, is \begin{align*} P_{\tx{max}} = \eta_{\tx{C}} I \cdot 1\tx{m}^2 = 0.91\tx{kJs}^{-1} = 910\tx{W} \ \ . \end{align*} This calculation ignores, that the solar cell's temperature probably will increase to higher values than $290\tx{K}$. \item[(b)] We assume a real efficiency $\eta_{\tx{r}} = 0.05$ of a solar cell. This leads to: \begin{align*} P_{\tx{r}} = \eta_{\tx{r}} I \cdot 1\tx{m}^2 = 48\tx{W} \ \ . \end{align*} We regard a cell, that does its job for $30$ years, $5$ hours a day. The "produced" electrical energy during this time is \begin{align*} E = \underbrace{30 \cdot 365 \cdot 5 \cdot 60 \cdot 60}_{=: \ t \ [\tx{s}]} \cdot 48 \tx{W} = 9461 \cdot 10^6 \tx{J} = 2628 \tx{kWh}\ \ , \end{align*} since $[\tx{kWh}] = 1000 \cdot [\tx{W}] \cdot 60^2$. We can compute the adequate price $p$ of the solar cell as follows, assuming $0.15\$/\tx{kWh}$: \begin{align*} p = 2628 \tx{kWh} \cdot 0.15\$ / \tx{kWh} = 394.2\$ \ \ . \end{align*} After $30$ years, the solar cell is profitable. \item[(c)] With \begin{align*} \diff{Q} = c \cdot \diff{T} \ \ , \end{align*} where $c = 1000 \tx{J}\tx{kg}^{-1}\tx{K}^{-1} \cdot 10^{14}\tx{kg}$ is the specific heat of the rock, we get the change of energy during a change of temperature. To compute the energy $\diff{W}$, the power plant "produces", we need its efficiency. Similar to task (a), the efficiency is computed by: \begin{align*} \eta_{\tx{C}} = \eta_{\tx{C}}(T) &= \frac{T - T_W}{T} \ \ \ \ \ (T_W=20°C=293\tx{K}) \ \ , \end{align*} with the difference, that one of both temperatures ($T$) is not a constant. Now we get: \begin{align*} \diff{W} = c \cdot \eta_{\tx{C}}(T) \diff{T} \ \ . \end{align*} The total amount of energy is: \begin{align*} W &= \int \diff{W} = c \cdot \int\limits_{T_i}^{T_f} \eta_{\tx{C}}(T) \diff{T} \\ &= c \cdot \int\limits_{T_i}^{T_f} \frac{T - T_W}{T} \diff{T} = c \cdot \int\limits_{T_i}^{T_f} \left(1 - \frac{T_W}{T} \right) \diff{T} \\ &= c \cdot \left[T - T_W \cdot \ln T \right]_{T_i}^{T_f} \\ &= c \cdot (T_f - T_W \cdot \ln T_f - T_i + T_W \cdot \ln T_i) \\ &= -2.49 \cdot 10^{19} \ \tx{J} \\ &= -6.91 \cdot 10^{12} \ \tx{kWh} \ \ , \end{align*} with $T_i = 600°C = 873K$ and $T_f = 110°C = 383K$. The negative value indicates, that the energy leaves the system (the power plant). \end{itemize} \end{document}