Thermodynamic processes: Difference between revisions
Created page with "Category:Compressible flow Category:Thermodynamics __TOC__ \section{Thermodynamics} \subsection{Specific Heat Relations} \noindent For thermally perfect and calorically perfect gases\\ \begin{equation} \begin{aligned} &C_p=\frac{dh}{dT}\\ &C_v=\frac{de}{dT} \end{aligned} \label{eq:specificheat} \end{equation}\\ \noindent From the definition of enthalpy and the equation of state $p=\rho RT$\\ \begin{equation} h=e+\frac{p}{\rho}=e+RT \label{eq:enthalpy} \end..." |
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=== Specific Heat Relations === | |||
For thermally perfect and calorically perfect gases | |||
<math display="block"> | |||
\begin{aligned} | \begin{aligned} | ||
&C_p=\frac{dh}{dT}\\ | &C_p=\frac{dh}{dT}\\ | ||
&C_v=\frac{de}{dT} | &C_v=\frac{de}{dT} | ||
\end{aligned} | \end{aligned} | ||
</math> | |||
From the definition of enthalpy and the equation of state <math>p=\rho RT</math> | |||
<math display="block"> | |||
h=e+\frac{p}{\rho}=e+RT | h=e+\frac{p}{\rho}=e+RT | ||
</math> | |||
Differentiate Eqn. \ref{eq:enthalpy} with respect to temperature gives | |||
<math display="block"> | |||
\frac{dh}{dT}=\frac{de}{dT}+\frac{d(RT)}{dT} | \frac{dh}{dT}=\frac{de}{dT}+\frac{d(RT)}{dT} | ||
</math> | |||
Inserting the specific heats gives | |||
<math display="block"> | |||
C_p=C_v+R | C_p=C_v+R | ||
</math> | |||
Dividing Eqn. \ref{eq:specificheat:b} by <math>C_v</math> gives | |||
<math display="block"> | |||
\frac{C_p}{C_v}=1+\frac{R}{C_v} | \frac{C_p}{C_v}=1+\frac{R}{C_v} | ||
</math> | |||
Introducing the ratio of specific heats defined as | |||
<math display="block"> | |||
\gamma=\frac{C_p}{C_v} | \gamma=\frac{C_p}{C_v} | ||
</math> | |||
Now, inserting Eqn. \ref{eq:gamma} in Eqn. \ref{eq:specificheat:c} gives | |||
<math display="block"> | |||
C_v=\frac{R}{\gamma-1} | C_v=\frac{R}{\gamma-1} | ||
</math> | |||
In the same way, dividing Eqn. \ref{eq:specificheat:b} with <math>C_p</math> gives | |||
<math display="block"> | |||
1=\frac{C_v}{C_p}+\frac{R}{C_p}=\frac{1}{\gamma}+\frac{R}{C_p} | 1=\frac{C_v}{C_p}+\frac{R}{C_p}=\frac{1}{\gamma}+\frac{R}{C_p} | ||
</math> | |||
and thus | |||
<math display="block"> | |||
C_p=\frac{\gamma R}{\gamma-1} | C_p=\frac{\gamma R}{\gamma-1} | ||
</math> | |||
=== Isentropic Relations === | |||
First law of thermodynamics: | First law of thermodynamics: | ||
<math display="block"> | |||
de=\delta q - \delta w | de=\delta q - \delta w | ||
</math> | |||
For a reversible process: <math>\delta w=pd(1/\rho)</math> and <math>\delta q=Tds</math> | |||
<math display="block"> | |||
de=Tds-pd\left(\frac{1}{\rho}\right) | de=Tds-pd\left(\frac{1}{\rho}\right) | ||
</math> | |||
Enthalpy is defined as: <math>h=e+p/\rho</math> and thus | |||
<math display="block"> | |||
dh=de+pd\left(\frac{1}{\rho}\right)+\left(\frac{1}{\rho}\right)dp | dh=de+pd\left(\frac{1}{\rho}\right)+\left(\frac{1}{\rho}\right)dp | ||
</math> | |||
Eliminate $de$ in Eqn. \ref{eq:firstlaw:b} using Eqn. \ref{eq:dh} | |||
<math display="block"> | |||
Tds=dh-\cancel{pd\left(\frac{1}{\rho}\right)}-\left(\frac{1}{\rho}\right)dp+\cancel{pd\left(\frac{1}{\rho}\right)} | |||
</math> | |||
<math display="block"> | |||
ds=\frac{dh}{T}-\frac{dp}{\rho T} | |||
</math> | |||
Using <math>dh=C_p T</math> and the equation of state <math>p=\rho RT</math>, we get | |||
<math display="block"> | |||
ds=C_p\frac{dT}{T}-R\frac{dp}{p} | ds=C_p\frac{dT}{T}-R\frac{dp}{p} | ||
</math> | |||
Integrating Eqn. \ref{eq:ds} gives | |||
<math display="block"> | |||
s_2-s_1=\int_1^2 C_p\frac{dT}{T}-R\ln\left(\frac{p_2}{p_1}\right) | s_2-s_1=\int_1^2 C_p\frac{dT}{T}-R\ln\left(\frac{p_2}{p_1}\right) | ||
</math> | |||
For a calorically perfect gas, <math>C_p</math> is constant (not a function of temperature) and can be moved out from the integral and thus | |||
<math display="block"> | |||
s_2-s_1=C_p\ln\left(\frac{T_2}{T_1}\right)-R\ln\left(\frac{p_2}{p_1}\right) | s_2-s_1=C_p\ln\left(\frac{T_2}{T_1}\right)-R\ln\left(\frac{p_2}{p_1}\right) | ||
</math> | |||
An alternative form of Eqn. \ref{eq:ds:c} is obtained by using <math>de=C_v dT</math> Eqn. \ref{eq:firstlaw:b}, which gives | |||
<math display="block"> | |||
s_2-s_1=\int_1^2 C_v\frac{dT}{T}-R\ln\left(\frac{\rho_2}{\rho_1}\right) | s_2-s_1=\int_1^2 C_v\frac{dT}{T}-R\ln\left(\frac{\rho_2}{\rho_1}\right) | ||
</math> | |||
Again, for a calorically perfect gas, we get | |||
<math display="block"> | |||
s_2-s_1=C_v\ln\left(\frac{T_2}{T_1}\right)-R\ln\left(\frac{\rho_2}{\rho_1}\right) | s_2-s_1=C_v\ln\left(\frac{T_2}{T_1}\right)-R\ln\left(\frac{\rho_2}{\rho_1}\right) | ||
</math> | |||
=== Isentropic Relations === | |||
Adiabatic and reversible processes, i.e., isentropic processes implies <math>ds=0</math> and thus Eqn. \ref{eq:ds:c} reduces to | |||
<math display="block"> | |||
\frac{C_p}{R}\ln\left(\frac{T_2}{T_1}\right)=\ln\left(\frac{p_2}{p_1}\right) | |||
</math> | |||
<math display="block"> | |||
\frac{C_p}{R}=\frac{\gamma}{\gamma-1} | |||
</math> | |||
<math display="block"> | |||
\frac{\gamma}{\gamma-1}\ln\left(\frac{T_2}{T_1}\right)=\ln\left(\frac{p_2}{p_1}\right)\Rightarrow | |||
</math> | |||
<math display="block"> | |||
\frac{p_2}{p_1}=\left(\frac{T_2}{T_1}\right)^{\gamma/(\gamma-1)} | \frac{p_2}{p_1}=\left(\frac{T_2}{T_1}\right)^{\gamma/(\gamma-1)} | ||
</math> | |||
In the same way, Eqn. \ref{eq:ds:e} gives | |||
<math display="block"> | |||
\frac{\rho_2}{\rho_1}=\left(\frac{T_2}{T_1}\right)^{1/(\gamma-1)} | \frac{\rho_2}{\rho_1}=\left(\frac{T_2}{T_1}\right)^{1/(\gamma-1)} | ||
</math> | |||
Eqn. \ref{eq:isentropic:a} and Eqn. \ref{eq:isentropic:b} constitutes the isentropic relations | |||
<math display="block"> | |||
\frac{p_2}{p_1}=\left(\frac{\rho_2}{\rho_1}\right)^{\gamma}=\left(\frac{T_2}{T_1}\right)^{\gamma/(\gamma-1)} | \frac{p_2}{p_1}=\left(\frac{\rho_2}{\rho_1}\right)^{\gamma}=\left(\frac{T_2}{T_1}\right)^{\gamma/(\gamma-1)} | ||
</math> | |||
=== Flow Processes === | |||
<math display="block"> | |||
ds=C_v\dfrac{dT}{T}+R\dfrac{d\nu}{\nu} | |||
</math> | |||
<math display="block"> | |||
d\nu=\dfrac{\nu}{R}ds-C_v\dfrac{\nu}{RT}dT=\dfrac{\nu}{R}ds-\dfrac{C_v}{p}dT | d\nu=\dfrac{\nu}{R}ds-C_v\dfrac{\nu}{RT}dT=\dfrac{\nu}{R}ds-\dfrac{C_v}{p}dT | ||
</math> | |||
for an isentropic process (<math>ds=0</math>), <math>d\nu < 0</math> for positive values of <math>dT</math>. | |||
<math display="block"> | |||
ds=C_p\dfrac{dT}{T} - R \dfrac{dp}{p} | |||
</math> | |||
<math display="block"> | |||
dp=-\dfrac{p}{R}ds+C_p\dfrac{p}{RT}dT=-\dfrac{p}{R}ds+C_p\rho dT | |||
</math> | |||
for an isentropic process (<math>ds=0</math>), <math>dp > 0</math> for positive values of <math>dT</math>. | |||
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Since <math>\nu</math> decreases with temperature and pressure increases with temperature for an isentropic process, we can see from Eqn.~\ref{eqn:process:dnu} that <math>d\nu</math> will be greater at lower temperatures and thus isochores (lines of constant specific volume) will be closely spaced at low temperatures and more sparse at higher temperatures. For an isochore <math>dv=0</math> which implies | |||
<math display="block"> | |||
0=\dfrac{\nu}{R}\left(ds-C_v\dfrac{dT}{T}\right) \Rightarrow \dfrac{dT}{ds}=\dfrac{T}{C_v} | |||
</math> | |||
and thus we can see that the slope of an isochore in a <math>T-s</math>-diagram is positive and that the slope increases with temperature. | |||
In analogy, we can see that an isobar (<math>dp=0</math>) leads to the following relation | |||
<math display="block"> | |||
0=\dfrac{p}{R}\left(C_p\dfrac{dT}{T}-ds\right) \Rightarrow \dfrac{dT}{ds}=\dfrac{T}{C_p} | |||
</math> | |||
and consequently isobars will also have a positive slope that increases with temperature in a <math>T-s</math>-diagram. Moreover, isobars are less steep than ischores as <math>C_p > C_v</math>. | |||
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Revision as of 17:12, 16 March 2026
Specific Heat Relations
For thermally perfect and calorically perfect gases
From the definition of enthalpy and the equation of state
Differentiate Eqn. \ref{eq:enthalpy} with respect to temperature gives
Inserting the specific heats gives
Dividing Eqn. \ref{eq:specificheat:b} by gives
Introducing the ratio of specific heats defined as
Now, inserting Eqn. \ref{eq:gamma} in Eqn. \ref{eq:specificheat:c} gives
In the same way, dividing Eqn. \ref{eq:specificheat:b} with gives
and thus
Isentropic Relations
First law of thermodynamics:
For a reversible process: and
Enthalpy is defined as: and thus
Eliminate $de$ in Eqn. \ref{eq:firstlaw:b} using Eqn. \ref{eq:dh}
Using and the equation of state , we get
Integrating Eqn. \ref{eq:ds} gives
For a calorically perfect gas, is constant (not a function of temperature) and can be moved out from the integral and thus
An alternative form of Eqn. \ref{eq:ds:c} is obtained by using Eqn. \ref{eq:firstlaw:b}, which gives
Again, for a calorically perfect gas, we get
Isentropic Relations
Adiabatic and reversible processes, i.e., isentropic processes implies and thus Eqn. \ref{eq:ds:c} reduces to
In the same way, Eqn. \ref{eq:ds:e} gives
Eqn. \ref{eq:isentropic:a} and Eqn. \ref{eq:isentropic:b} constitutes the isentropic relations
Flow Processes
for an isentropic process (), for positive values of .
for an isentropic process (), for positive values of .
Since decreases with temperature and pressure increases with temperature for an isentropic process, we can see from Eqn.~\ref{eqn:process:dnu} that will be greater at lower temperatures and thus isochores (lines of constant specific volume) will be closely spaced at low temperatures and more sparse at higher temperatures. For an isochore which implies
and thus we can see that the slope of an isochore in a -diagram is positive and that the slope increases with temperature.
In analogy, we can see that an isobar () leads to the following relation
and consequently isobars will also have a positive slope that increases with temperature in a -diagram. Moreover, isobars are less steep than ischores as .