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		<id>http://www.sklogwiki.org/SklogWiki/index.php?title=Cole_equation_of_state&amp;diff=14819</id>
		<title>Cole equation of state</title>
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		<updated>2015-12-05T12:16:25Z</updated>

		<summary type="html">&lt;p&gt;103.15.217.222: space inserted between &amp;#039;the&amp;#039; and &amp;#039;EOS&amp;#039; for friendly reading&lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;The &#039;&#039;&#039;Cole equation of state&#039;&#039;&#039;&lt;br /&gt;
&amp;lt;ref&amp;gt;[http://www.archive.org/details/underwaterexplos00cole Robert H Cole &amp;quot;Underwater explosions&amp;quot;, Princeton University Press, Princeton (1948)]&amp;lt;/ref&amp;gt;&amp;lt;ref&amp;gt;G. K. Batchelor &amp;quot;An introduction to ﬂuid mechanics&amp;quot;, Cambridge University Press (1974) ISBN  0521663962&amp;lt;/ref&amp;gt;&amp;lt;ref&amp;gt;[http://www.archive.org/details/supersonicflowsh00cour Richard Courant &amp;quot;Supersonic flow and shock waves a manual on the mathematical theory of non-linear wave motion&amp;quot;, Courant Institute of Mathematical Sciences, New York University, New York (1944)]&amp;lt;/ref&amp;gt;&lt;br /&gt;
is the adiabatic version of the [[stiffened equation of state]] for liquids. (See &#039;&#039;Derivation&#039;&#039;, below.)&lt;br /&gt;
It has the form&lt;br /&gt;
&lt;br /&gt;
:&amp;lt;math&amp;gt;p = B \left[ \left( \frac{\rho}{\rho_0} \right)^\gamma  -1 \right]&amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
In it, &amp;lt;math&amp;gt;\rho_0&amp;lt;/math&amp;gt; is a reference density around which the density varies,&lt;br /&gt;
&amp;lt;math&amp;gt;\gamma&amp;lt;/math&amp;gt; is the [[Heat capacity#Adiabatic index | adiabatic index]],  and &amp;lt;math&amp;gt;B&amp;lt;/math&amp;gt; is a pressure parameter.&lt;br /&gt;
&lt;br /&gt;
Usually, the equation is used to model a nearly incompressible system. In this case,&lt;br /&gt;
the exponent is often set to a value of 7, and &amp;lt;math&amp;gt;B&amp;lt;/math&amp;gt; is large, in the following&lt;br /&gt;
sense. The fluctuations of the density are related to the speed of sound as&lt;br /&gt;
&lt;br /&gt;
:&amp;lt;math&amp;gt;\frac{\delta \rho}{\rho} = \frac{v^2}{c^2} ,&amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
where &amp;lt;math&amp;gt;v&amp;lt;/math&amp;gt; is the largest velocity, and &amp;lt;math&amp;gt;c&amp;lt;/math&amp;gt; is the speed of&lt;br /&gt;
sound (the ratio &amp;lt;math&amp;gt;v/c&amp;lt;/math&amp;gt; is [[Mach&#039;s number]]). The [[speed of sound]] can&lt;br /&gt;
be seen to be&lt;br /&gt;
&lt;br /&gt;
:&amp;lt;math&amp;gt;c^2 = \frac{\gamma B}{\rho_0}. &amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
Therefore, if &amp;lt;math&amp;gt;B=100 \rho_0 v^2 / \gamma&amp;lt;/math&amp;gt;, the relative density fluctuations&lt;br /&gt;
will be about 0.01.&lt;br /&gt;
&lt;br /&gt;
If the fluctuations in the density are indeed small, the&lt;br /&gt;
[[Equations of state | equation of state]] may be approximated by the simpler:&lt;br /&gt;
&lt;br /&gt;
:&amp;lt;math&amp;gt;p = B \gamma \left[&lt;br /&gt;
\frac{\rho-\rho_0}{\rho_0}&lt;br /&gt;
 \right]&amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
It is quite common that the name &amp;quot;[[Tait equation of state]]&amp;quot; is improperly used for this EOS. This perhaps stems for the classic text by Cole calling this equation a &amp;quot;modified Tait equation&amp;quot; (p. 39).&lt;br /&gt;
&lt;br /&gt;
==Derivation==&lt;br /&gt;
&lt;br /&gt;
Let us write the stiffened EOS as&lt;br /&gt;
&lt;br /&gt;
:&amp;lt;math&amp;gt;p+ p^* = (\gamma -1) e \rho = (\gamma -1) E / V ,&amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
where &#039;&#039;E&#039;&#039; is the internal energy. In an adiabatic process, the work is the only responsible of a change in internal energy. Hence the&lt;br /&gt;
first law reads&lt;br /&gt;
&lt;br /&gt;
:&amp;lt;math&amp;gt;  dW= -p dV  = dE .&amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
Taking differences on the EOS,&lt;br /&gt;
&lt;br /&gt;
:&amp;lt;math&amp;gt;   dE = \frac{1}{\gamma-1} [(p+p^*) dV + V dp ] , &amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
so that the first law can be simplified to&lt;br /&gt;
&lt;br /&gt;
:&amp;lt;math&amp;gt;   - (\gamma p + p^*)  dV  = V dp.&amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
This equation can be solved in the standard way, with the result&lt;br /&gt;
&lt;br /&gt;
:&amp;lt;math&amp;gt;   ( p + p^* / \gamma)  V^\gamma   = C ,&amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
where &#039;&#039;C&#039;&#039; is a constant of integration. This derivation closely follows the standard derivation of the adiabatic law&lt;br /&gt;
of an ideal gas, and it reduces to it if &amp;lt;math&amp;gt;   p^*  =0 &amp;lt;/math&amp;gt;.&lt;br /&gt;
&lt;br /&gt;
If the values of the thermodynamic variables are known at some reference state, we may write&lt;br /&gt;
&lt;br /&gt;
:&amp;lt;math&amp;gt;   ( p + p^* / \gamma)  V^\gamma   =   ( p_0 + p^* / \gamma)  V_0^\gamma , &amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
which can be written as&lt;br /&gt;
&lt;br /&gt;
:&amp;lt;math&amp;gt;   p      =  p_0 +  ( p_0 + p^* / \gamma) ( (V_0/V)^\gamma - 1 )  . &amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
Going back to densities, instead of volumes,&lt;br /&gt;
&lt;br /&gt;
:&amp;lt;math&amp;gt;   p      =  p_0 +  ( p_0 + p^* / \gamma)  ( (\rho/\rho_0)^\gamma - 1) . &amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
Comparing with the Cole EOS, we can readily identify&lt;br /&gt;
&lt;br /&gt;
:&amp;lt;math&amp;gt; B = p^* / \gamma  &amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
Moreover, the Cole EOS differs slightly, as it should read (as indeed does in e.g. the book by Courant)&lt;br /&gt;
&lt;br /&gt;
:&amp;lt;math&amp;gt;p = A \left( \frac{\rho}{\rho_0} \right)^\gamma  - B ,&amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
with&lt;br /&gt;
&lt;br /&gt;
:&amp;lt;math&amp;gt; A = p^* / \gamma  + p_0 . &amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
This difference is negligible for liquids but for an ideal gas &amp;lt;math&amp;gt;p^*=0&amp;lt;/math&amp;gt; and there is a huge&lt;br /&gt;
difference, &#039;&#039;B&#039;&#039; being zero and &#039;&#039;A&#039;&#039; being equal to the reference pressure.&lt;br /&gt;
&lt;br /&gt;
Now, the speed of sound is given by&lt;br /&gt;
&lt;br /&gt;
:&amp;lt;math&amp;gt;   c^2=\frac{dp}{d\rho}  &amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
with the derivative taken along an adiabatic line. This is precisely our case, and we readily obtain&lt;br /&gt;
&lt;br /&gt;
:&amp;lt;math&amp;gt;   c^2=  ( p_0 + p^* / \gamma) \gamma /\rho_0 . &amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
From this expression a value of &amp;lt;math&amp;gt;p^*&amp;lt;/math&amp;gt; can be deduced. For water, &amp;lt;math&amp;gt;p^*\approx 23000&amp;lt;/math&amp;gt; bar,&lt;br /&gt;
from which &amp;lt;math&amp;gt;B\approx 3000&amp;lt;/math&amp;gt; bar. If the speed of sound is used in the EOS one obtains the rather&lt;br /&gt;
elegant expression&lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
:&amp;lt;math&amp;gt;   p      =  p_0 +  ( \rho_0 c^2 / \gamma)  ( (\rho/\rho_0)^\gamma - 1) . &amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
==References==&lt;br /&gt;
&amp;lt;references/&amp;gt;&lt;br /&gt;
[[category: equations of state]]&lt;/div&gt;</summary>
		<author><name>103.15.217.222</name></author>
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