User talk:Paul Wormer/scratchbook: Difference between revisions

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===Proof that entropy is a state variable===
===Proof that entropy is a state variable===
After equation [[#(1)|(1)]] has been proven, the entropy ''S''  has been shown to be a state variable. The standard proof, as given now, is physical and by means of the construct of [[Carnot cycle]]s and is derived from the Clausius/Kelvin formulation of the second law given in the introduction.
After equation [[#(1)|(1)]] has been proven, the entropy ''S''  has been shown to be a state variable. The standard proof, as given now, is physical and by means of [[Carnot cycle]]s and is derived from the Clausius/Kelvin formulation of the second law given in the introduction.
{{Image|Entropy.png|right|350px|Fig. 1 Carnot engine (E) moves to or from condensor (C) heat from or to infinite heat reservoir (R).}}
{{Image|Entropy.png|right|350px|Fig. 1.  ''T'' > ''T''<sub>0</sub>. (I): Carnot engine E moves heat from  heat reservoir R to condensor C and needs input of work DW<sub>in</sub>. (II): E generates work DW<sub>out</sub> from the heat flow from C to R. }} An alternative, more mathematical proof, postulates the existence of a state variable ''S'' with certain properties and derives the existence of [[thermodynamical temperature]] and the second law from these properties.


In figure 1  a two finite heat baths C ("condensors") of constant volume with variable temperature ''T'' are shown. They are connected to an infinite heat reservoir R through reversible Carnot engines E. Because R is infinite its temperature ''T''<sub>0</sub> is constant, addition or extraction of heat does not change ''T''<sub>0</sub>.  It is assumed that always ''T'' &ge; ''T''<sub>0</sub>. The Carnot engines cycle and per cycle either generate work ''DW''<sub>out</sub> when heat is transported from high temperature to low temperature (path II), or need work  ''DW''<sub>in</sub> when heat is transported from low to high temperature (path I).
In figure 1  a finite heat bath C ("condensor") of constant volume and variable temperature ''T'' is shown. It is connected to an infinite heat reservoir R through a reversible Carnot engine E. Because R is infinite its temperature ''T''<sub>0</sub> is constant, addition or extraction of heat does not change ''T''<sub>0</sub>.  It is assumed that always ''T'' &ge; ''T''<sub>0</sub>.  One may think of the system E-plus-C as a ship and the heat reservoir R as the sea. The following argument then deals with an attempt of extracting energy from the sea in order to move the ship, i.e., with an attempt to let E perform net outgoing work.
 
A Carnot engine performs reversible cycles and per cycle either generates work ''DW''<sub>out</sub> when heat is transported from high temperature to low temperature (path II), or needs work  ''DW''<sub>in</sub> when heat is transported from low to high temperature (path I).  


The definition of [[thermodynamical temperature]]  is such that for path II,
The definition of [[thermodynamical temperature]]  is such that for path II,
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\frac{DW_\mathrm{out}}{DQ} = \frac{T-T_0}{T},
\frac{DW_\mathrm{out}}{DQ} = \frac{T-T_0}{T},
</math>
</math>
while for path I it holds by definition that
while for path I  
:<math>
:<math>
\frac{DW_\mathrm{in}}{DQ_0} = \frac{T-T_0}{T_0}.
\frac{DW_\mathrm{in}}{DQ_0} = \frac{T-T_0}{T_0}.
</math>
</math>
The first law of thermodynamics states that both I and II, respectively, it holds that
 
The first law of thermodynamics states for both I and II, respectively,
:<math>
:<math>
DW_\mathrm{in} = DQ- DQ_0\quad\hbox{and}\quad DW_\mathrm{out} = DQ- DQ_0
-DW_\mathrm{in} -DQ_0 + DQ=0\quad\hbox{and}\quad DW_\mathrm{out} + DQ_0-DQ=0
</math>
</math>
For I,
{{Image|Cycle entropy.png|right|150px|Fig. 2. Two paths in the state space of the "condensor" C.}}
For path I,
:<math>
:<math>
\begin{align}
\begin{align}
\frac{DW_\mathrm{in}}{DQ_0} &= \frac{DQ- DQ_0}{DQ_0} = \frac{DQ}{DQ_0} -1 \\
\frac{DW_\mathrm{in}}{DQ_0} &= \frac{DQ- DQ_0}{DQ_0} = \frac{DQ}{DQ_0} -1 \\
&=\frac{T-T_0}{T_0} =  \frac{T}{T_0} - 1 \\
&=\frac{T-T_0}{T_0} =  \frac{T}{T_0} - 1 \;
&\Longrightarrow DQ_0 = T_0 \left(\frac{DQ}{T}\right)
\Longrightarrow DQ_0 = T_0 \left(\frac{DQ}{T}\right)
\end{align}
\end{align}
</math>
</math>
For II,
 
For II we find the same result,
:<math>
:<math>
\begin{align}
\begin{align}
\frac{DW_\mathrm{out}}{DQ} &= \frac{DQ- DQ_0}{DQ} = 1- \frac{DQ_0}{DQ} \\
\frac{DW_\mathrm{out}}{DQ} &= \frac{DQ- DQ_0}{DQ} = 1- \frac{DQ_0}{DQ} \\
&=\frac{T-T_0}{T} =  1- \frac{T_0}{T} \\
&=\frac{T-T_0}{T} =  1- \frac{T_0}{T}  
&\Longrightarrow DQ_0 = T_0 \left(\frac{DQ}{T}\right)
\;\Longrightarrow DQ_0 = T_0 \left(\frac{DQ}{T}\right)
\end{align}
\end{align}
</math>
</math>
In figure 2 the state diagram of the "condensor" C is shown. Along path I the Carnot engine needs input of work to transport heat from the reservoir R to C and the absorption of heat raises the temperature and pressure of C. Integration of ''DW''<sub>in</sub> = ''DQ'' &minus; ''DQ''<sub>0</sub> along path I gives
:<math>
W_\mathrm{in} = Q_\mathrm{in} - T_0 {\int\limits_1\limits^2}_{{\!\!}^{(I)}} \frac{DQ}{T} \quad\hbox{with}\quad  Q_\mathrm{in} \equiv  {\int\limits_1\limits^2}_{{\!\!}^{(I)}} DQ.
</math>
Along path II the Carnot engine delivers work while transporting heat from C to R. Integration of ''DW''<sub>out</sub> = ''DQ'' &minus; ''DQ''<sub>0</sub> along path I gives
:<math>
W_\mathrm{out} = Q_\mathrm{out} - T_0 {\int\limits_2\limits^1}_{{\!\!}^{(II)}} \frac{DQ}{T}
\quad\hbox{with}\quad  Q_\mathrm{out} \equiv  {\int\limits_2\limits^1}_{{\!\!}^{(II)}} DQ
</math>
Assume now that the  amount of heat ''Q''<sub>out</sub> extracted (along path II) from C and the heat ''Q''<sub>in</sub> delivered (along I) to C are the same in absolute value, or in other words, that upon a full cycle in the state diagram of figure 2 the condensor C does not gain or lose heat. That is,
:<math>
Q_\mathrm{in} + Q_\mathrm{out} = 0, \,
</math>
and hence
:<math>
W_\mathrm{in} + W_\mathrm{out} =  - T_0 {\int\limits_1\limits^2}_{{\!\!}^{(I)}} \frac{DQ}{T}
- T_0 {\int\limits_2\limits^1}_{{\!\!}^{(II)}} \frac{DQ}{T}.
</math>
If the total net work ''W''<sub>in</sub> + ''W''<sub>out</sub> performed in a full cycle is positive (outgoing), work is done by  heat obtained from R, which is not possible because of the Clausius/Kelvin principle.  If the total net work ''W''<sub>in</sub> + ''W''<sub>out</sub> is negative, then by inverting all reversible processes, i.e., by swapping path I and II (going backwards in figure 2), the net work becomes positive (outgoing). Again the Clausius/Kelvin principle is violated. The conclusion is that the net work is zero and that
:<math>
T_0 {\int\limits_1\limits^2}_{{\!\!}^{(I)}} \frac{DQ}{T} +
T_0 {\int\limits_2\limits^1}_{{\!\!}^{(II)}} \frac{DQ}{T} = 0
\;\Longrightarrow\;  {\int\limits_1\limits^2}_{{\!\!}^{(I)}} \frac{DQ}{T} =  {\int\limits_1\limits^2}_{{\!\!}^{(II)}} \frac{DQ}{T}.
</math>
From this independence of path it is concluded that
:<math>
dS \equiv \frac{DQ}{T}
</math>
is a state (local) variable.

Revision as of 10:25, 28 October 2009

The second law of thermodynamics, as formulated in the middle of the 19th century by William Thomson (Lord Kelvin) and Rudolf Clausius, states that it is impossible to gain mechanical energy by letting heat flow from a cold to a warm object. The law states, on the contrary, that mechanical energy (work) is needed to transport heat from a low- to a high-temperature heat bath.

If the second law would be invalid, there would be no energy crisis. For example, it would be possible—as already pointed out by Lord Kelvin—to fuel ships by energy extracted from sea water. After all, the oceans contain immense amounts of internal energy. If it would be possible to extract a small portion of this energy—whereby a slight cooling of the sea water would occur—and to use this energy to move the ship (a form of work), then the seas could be sailed without any net consumption of energy. It would not violate the first law of thermodynamics, because the the ship's rotating propellers do heat the water and in total the energy of the supersystem "ship-plus-ocean" would be conserved, in agreement with the first law. Unfortunately, it is not possible, because a ship is warmer than the sea water that it moves in (or at least the ship is not colder) and hence no work can be extracted from the water by the ship.

Entropy

Clausius was able to give a mathematical expression of the second law. In order to be able do that, he needed the concept of entropy. Following his footsteps entropy will be introduced in this subsection.

The state of a thermodynamical system is characterized by a number of (dependent) variables, such as pressure p, temperature T, amount of substance, volume V, etc. In general a system has a number of energy contacts with its surroundings. For instance, the prototype thermodynamical system, a gas-filled cylinder with piston, can perform work DW = pdV on its surroundings, where dV stands for a small increment of the volume V of the cylinder, p is the pressure inside the cylinder and DW stands for a small amount of work. This small amount is indicated by D, and not by d, because DW is not necessarily a differential of a function. However, when we divide by p the quantity DW/p becomes equal to the differential of the state function V. State functions are local, they dependent on the actual values of the parameters, and not on the path along which the state was reached. Mathematically this means that integration from point 1 to point 2 along path I is equal to integration along another path II

The amount of work (divided by p) performed along path I is equal to the amount of work (divided by p) along path II, which proves that the fraction DW/p is a state variable.

Absorption of a small amount of heat DQ is another energy contact of the system with its surroundings. In a completely analogous manner, the following result can be shown for DQ (divided by T) absorbed by the system along two different paths:

(1)



Hence the quantity dS defined by

is the differential of a state variable S, the entropy of the system. Before proving equation (1) from the second law, it is emphasized that this definition of entropy only fixes entropy differences:

Note further that entropy has the dimension energy per degree temperature (joule per degree kelvin) and recalling the first law of thermodynamics (the differential dU of the internal energy satisfies dU = DQ + DW), it follows that

(For convenience sake only a single work term was considered here, namely DW = pdV). The internal energy is an extensive quantity, that is, when the system is halved, U is halved too. The temperature T is an intensive property, independent of the size of the system. The entropy S, then, is also extensive. In that sense the entropy resembles the volume of the system. An important difference between V and S is that the former is a state variable with a concrete meaning, whereas the latter is introduced by analogy and therefore is not easily visualized.

Proof that entropy is a state variable

After equation (1) has been proven, the entropy S has been shown to be a state variable. The standard proof, as given now, is physical and by means of Carnot cycles and is derived from the Clausius/Kelvin formulation of the second law given in the introduction.

PD Image
Fig. 1. T > T0. (I): Carnot engine E moves heat from heat reservoir R to condensor C and needs input of work DWin. (II): E generates work DWout from the heat flow from C to R.

An alternative, more mathematical proof, postulates the existence of a state variable S with certain properties and derives the existence of thermodynamical temperature and the second law from these properties.

In figure 1 a finite heat bath C ("condensor") of constant volume and variable temperature T is shown. It is connected to an infinite heat reservoir R through a reversible Carnot engine E. Because R is infinite its temperature T0 is constant, addition or extraction of heat does not change T0. It is assumed that always TT0. One may think of the system E-plus-C as a ship and the heat reservoir R as the sea. The following argument then deals with an attempt of extracting energy from the sea in order to move the ship, i.e., with an attempt to let E perform net outgoing work.

A Carnot engine performs reversible cycles and per cycle either generates work DWout when heat is transported from high temperature to low temperature (path II), or needs work DWin when heat is transported from low to high temperature (path I).

The definition of thermodynamical temperature is such that for path II,

while for path I

The first law of thermodynamics states for both I and II, respectively,

PD Image
Fig. 2. Two paths in the state space of the "condensor" C.

For path I,

For II we find the same result,

In figure 2 the state diagram of the "condensor" C is shown. Along path I the Carnot engine needs input of work to transport heat from the reservoir R to C and the absorption of heat raises the temperature and pressure of C. Integration of DWin = DQDQ0 along path I gives

Along path II the Carnot engine delivers work while transporting heat from C to R. Integration of DWout = DQDQ0 along path I gives

Assume now that the amount of heat Qout extracted (along path II) from C and the heat Qin delivered (along I) to C are the same in absolute value, or in other words, that upon a full cycle in the state diagram of figure 2 the condensor C does not gain or lose heat. That is,

and hence

If the total net work Win + Wout performed in a full cycle is positive (outgoing), work is done by heat obtained from R, which is not possible because of the Clausius/Kelvin principle. If the total net work Win + Wout is negative, then by inverting all reversible processes, i.e., by swapping path I and II (going backwards in figure 2), the net work becomes positive (outgoing). Again the Clausius/Kelvin principle is violated. The conclusion is that the net work is zero and that

From this independence of path it is concluded that

is a state (local) variable.