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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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__TOC__
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\section{Thermodynamics}
=== Specific Heat Relations ===


\subsection{Specific Heat Relations}
For thermally perfect and calorically perfect gases


\noindent For thermally perfect and calorically perfect gases\\
<math display="block">
 
\begin{equation}
\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}
\label{eq:specificheat}
</math>
\end{equation}\\


\noindent From the definition of enthalpy and the equation of state $p=\rho RT$\\
From the definition of enthalpy and the equation of state <math>p=\rho RT</math>


\begin{equation}
<math display="block">
h=e+\frac{p}{\rho}=e+RT
h=e+\frac{p}{\rho}=e+RT
\label{eq:enthalpy}
</math>
\end{equation}\\


\noindent Differentiate Eqn. \ref{eq:enthalpy} with respect to temperature gives\\
Differentiate Eqn. \ref{eq:enthalpy} with respect to temperature gives


\begin{equation}
<math display="block">
\frac{dh}{dT}=\frac{de}{dT}+\frac{d(RT)}{dT}
\frac{dh}{dT}=\frac{de}{dT}+\frac{d(RT)}{dT}
\label{eq:enthalpy:b}
</math>
\end{equation}\\


\noindent Inserting the specific heats gives\\
Inserting the specific heats gives


\begin{equation}
<math display="block">
C_p=C_v+R
C_p=C_v+R
\label{eq:specificheat:b}
</math>
\end{equation}\\


\noindent Dividing Eqn. \ref{eq:specificheat:b} by $C_v$ gives\\
Dividing Eqn. \ref{eq:specificheat:b} by <math>C_v</math> gives


\begin{equation}
<math display="block">
\frac{C_p}{C_v}=1+\frac{R}{C_v}
\frac{C_p}{C_v}=1+\frac{R}{C_v}
\label{eq:specificheat:c}
</math>
\end{equation}\\


\noindent Introducing the ratio of specific heats defined as\\
Introducing the ratio of specific heats defined as


\begin{equation}
<math display="block">
\gamma=\frac{C_p}{C_v}
\gamma=\frac{C_p}{C_v}
\label{eq:gamma}
</math>
\end{equation}\\


\noindent Now, inserting Eqn. \ref{eq:gamma} in Eqn. \ref{eq:specificheat:c} gives\\
Now, inserting Eqn. \ref{eq:gamma} in Eqn. \ref{eq:specificheat:c} gives


\begin{equation}
<math display="block">
C_v=\frac{R}{\gamma-1}
C_v=\frac{R}{\gamma-1}
\label{eq:specificheat:d}
</math>
\end{equation}\\


\noindent In the same way, dividing Eqn. \ref{eq:specificheat:b} with $C_p$ gives\\
In the same way, dividing Eqn. \ref{eq:specificheat:b} with <math>C_p</math> gives


\begin{equation}
<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}
\label{eq:specificheat:e}
</math>
\end{equation}\\


\noindent and thus\\
and thus


\begin{equation}
<math display="block">
C_p=\frac{\gamma R}{\gamma-1}
C_p=\frac{\gamma R}{\gamma-1}
\label{eq:specificheat:f}
</math>
\end{equation}\\


\subsection{Isentropic Relations}
=== Isentropic Relations ===


First law of thermodynamics:\\
First law of thermodynamics:


\begin{equation}
<math display="block">
de=\delta q - \delta w
de=\delta q - \delta w
\label{eq:firstlaw}
</math>
\end{equation}\\


\noindent For a reversible process: $\delta w=pd(1/\rho)$ and $\delta q=Tds$\\
For a reversible process: <math>\delta w=pd(1/\rho)</math> and <math>\delta q=Tds</math>


\begin{equation}
<math display="block">
de=Tds-pd\left(\frac{1}{\rho}\right)
de=Tds-pd\left(\frac{1}{\rho}\right)
\label{eq:firstlaw:b}
</math>
\end{equation}\\


\noindent Enthalpy is defined as: $h=e+p/\rho$ and thus\\
Enthalpy is defined as: <math>h=e+p/\rho</math> and thus


\begin{equation}
<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
\label{eq:dh}
</math>
\end{equation}\\


\noindent Eliminate $de$ in Eqn. \ref{eq:firstlaw:b} using Eqn. \ref{eq:dh}\\
Eliminate $de$ in Eqn. \ref{eq:firstlaw:b} using Eqn. \ref{eq:dh}


\[Tds=dh-\cancel{pd\left(\frac{1}{\rho}\right)}-\left(\frac{1}{\rho}\right)dp+\cancel{pd\left(\frac{1}{\rho}\right)}\]\\
<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>


\[ds=\frac{dh}{T}-\frac{dp}{\rho T}\]\\
<math display="block">
ds=\frac{dh}{T}-\frac{dp}{\rho T}
</math>


\noindent Using $dh=C_p T$ and the equation of state $p=\rho RT$, we get\\
Using <math>dh=C_p T</math> and the equation of state <math>p=\rho RT</math>, we get


\begin{equation}
<math display="block">
ds=C_p\frac{dT}{T}-R\frac{dp}{p}
ds=C_p\frac{dT}{T}-R\frac{dp}{p}
\label{eq:ds}
</math>
\end{equation}\\


\noindent Integrating Eqn. \ref{eq:ds} gives\\
Integrating Eqn. \ref{eq:ds} gives


\begin{equation}
<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)
\label{eq:ds:b}
</math>
\end{equation}\\


\noindent For a calorically perfect gas, $C_p$ is constant (not a function of temperature) and can be moved out from the integral and thus\\
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


\begin{equation}
<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)
\label{eq:ds:c}
</math>
\end{equation}\\


\noindent An alternative form of Eqn. \ref{eq:ds:c} is obtained by using $de=C_v dT$ Eqn. \ref{eq:firstlaw:b}, which gives\\
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


\begin{equation}
<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)
\label{eq:ds:d}
</math>
\end{equation}\\


\noindent Again, for a calorically perfect gas, we get\\
Again, for a calorically perfect gas, we get


\begin{equation}
<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)
\label{eq:ds:e}
</math>
\end{equation}\\


\section*{Isentropic Relations}
=== Isentropic Relations ===


\noindent Adiabatic and reversible processes, i.e., isentropic processes implies $ds=0$ and thus Eqn. \ref{eq:ds:c} reduces to\\
Adiabatic and reversible processes, i.e., isentropic processes implies <math>ds=0</math> and thus Eqn. \ref{eq:ds:c} reduces to


\[\frac{C_p}{R}\ln\left(\frac{T_2}{T_1}\right)=\ln\left(\frac{p_2}{p_1}\right)\]\\
<math display="block">
\frac{C_p}{R}\ln\left(\frac{T_2}{T_1}\right)=\ln\left(\frac{p_2}{p_1}\right)
</math>


\[\frac{C_p}{R}=\frac{\gamma}{\gamma-1}\]\\
<math display="block">
\frac{C_p}{R}=\frac{\gamma}{\gamma-1}
</math>


\[\frac{\gamma}{\gamma-1}\ln\left(\frac{T_2}{T_1}\right)=\ln\left(\frac{p_2}{p_1}\right)\Rightarrow\]\\
<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>


\begin{equation}
<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)}
\label{eq:isentropic:a}
</math>
\end{equation}\\


\noindent In the same way, Eqn. \ref{eq:ds:e} gives\\
In the same way, Eqn. \ref{eq:ds:e} gives


\begin{equation}
<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)}
\label{eq:isentropic:b}
</math>
\end{equation}\\


\noindent Eqn. \ref{eq:isentropic:a} and Eqn. \ref{eq:isentropic:b} constitutes the isentropic relations\\
Eqn. \ref{eq:isentropic:a} and Eqn. \ref{eq:isentropic:b} constitutes the isentropic relations


\begin{equation}
<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)}
\label{eq:isentropic:a}
</math>
\end{equation}


\section{Flow Processes}
=== Flow Processes ===


\[ds=C_v\dfrac{dT}{T}+R\dfrac{d\nu}{\nu}\]
<math display="block">
ds=C_v\dfrac{dT}{T}+R\dfrac{d\nu}{\nu}
</math>


\begin{equation}
<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
\label{eqn:process:dnu}
</math>
\end{equation}


\noindent for an isentropic process ($ds=0$), $d\nu < 0$ for positive values of $dT$.
for an isentropic process (<math>ds=0</math>), <math>d\nu < 0</math> for positive values of <math>dT</math>.


\[ds=C_p\dfrac{dT}{T} - R \dfrac{dp}{p}\]
<math display="block">
ds=C_p\dfrac{dT}{T} - R \dfrac{dp}{p}
</math>


\[dp=-\dfrac{p}{R}ds+C_p\dfrac{p}{RT}dT=-\dfrac{p}{R}ds+C_p\rho dT\]
<math display="block">
dp=-\dfrac{p}{R}ds+C_p\dfrac{p}{RT}dT=-\dfrac{p}{R}ds+C_p\rho dT
</math>


\noindent for an isentropic process ($ds=0$), $dp > 0$ for positive values of $dT$.
for an isentropic process (<math>ds=0</math>), <math>dp > 0</math> for positive values of <math>dT</math>.


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\noindent Since $\nu$ decreases with temperature and pressure increases with temperature for an isentropic process, we can see from Eqn.~\ref{eqn:process:dnu} that $d\nu$ 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 $dv=0$ which implies
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


\[0=\dfrac{\nu}{R}\left(ds-C_v\dfrac{dT}{T}\right) \Rightarrow \dfrac{dT}{ds}=\dfrac{T}{C_v}\]
<math display="block">
0=\dfrac{\nu}{R}\left(ds-C_v\dfrac{dT}{T}\right) \Rightarrow \dfrac{dT}{ds}=\dfrac{T}{C_v}
</math>


\noindent and thus we can see that the slope of an isochore in a $T-s$-diagram is positive and that the slope increases with temperature.
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.


\noindent In analogy, we can see that an isobar ($dp=0$) leads to the following relation
In analogy, we can see that an isobar (<math>dp=0</math>) leads to the following relation


\[0=\dfrac{p}{R}\left(C_p\dfrac{dT}{T}-ds\right) \Rightarrow \dfrac{dT}{ds}=\dfrac{T}{C_p}\]
<math display="block">
0=\dfrac{p}{R}\left(C_p\dfrac{dT}{T}-ds\right) \Rightarrow \dfrac{dT}{ds}=\dfrac{T}{C_p}
</math>


\noindent and consequently isobars will also have a positive slope that increases with temperature in a $T-s$-diagram. Moreover, isobars are less steep than ischores as $C_p > C_v$.  
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

Cp=dhdTCv=dedT

From the definition of enthalpy and the equation of state p=ρRT

h=e+pρ=e+RT

Differentiate Eqn. \ref{eq:enthalpy} with respect to temperature gives

dhdT=dedT+d(RT)dT

Inserting the specific heats gives

Cp=Cv+R

Dividing Eqn. \ref{eq:specificheat:b} by Cv gives

CpCv=1+RCv

Introducing the ratio of specific heats defined as

γ=CpCv

Now, inserting Eqn. \ref{eq:gamma} in Eqn. \ref{eq:specificheat:c} gives

Cv=Rγ1

In the same way, dividing Eqn. \ref{eq:specificheat:b} with Cp gives

1=CvCp+RCp=1γ+RCp

and thus

Cp=γRγ1

Isentropic Relations

First law of thermodynamics:

de=δqδw

For a reversible process: δw=pd(1/ρ) and δq=Tds

de=Tdspd(1ρ)

Enthalpy is defined as: h=e+p/ρ and thus

dh=de+pd(1ρ)+(1ρ)dp

Eliminate $de$ in Eqn. \ref{eq:firstlaw:b} using Eqn. \ref{eq:dh}

Tds=dhpd(1ρ)(1ρ)dp+pd(1ρ)

ds=dhTdpρT

Using dh=CpT and the equation of state p=ρRT, we get

ds=CpdTTRdpp

Integrating Eqn. \ref{eq:ds} gives

s2s1=12CpdTTRln(p2p1)

For a calorically perfect gas, Cp is constant (not a function of temperature) and can be moved out from the integral and thus

s2s1=Cpln(T2T1)Rln(p2p1)

An alternative form of Eqn. \ref{eq:ds:c} is obtained by using de=CvdT Eqn. \ref{eq:firstlaw:b}, which gives

s2s1=12CvdTTRln(ρ2ρ1)

Again, for a calorically perfect gas, we get

s2s1=Cvln(T2T1)Rln(ρ2ρ1)

Isentropic Relations

Adiabatic and reversible processes, i.e., isentropic processes implies ds=0 and thus Eqn. \ref{eq:ds:c} reduces to

CpRln(T2T1)=ln(p2p1)

CpR=γγ1

γγ1ln(T2T1)=ln(p2p1)

p2p1=(T2T1)γ/(γ1)

In the same way, Eqn. \ref{eq:ds:e} gives

ρ2ρ1=(T2T1)1/(γ1)

Eqn. \ref{eq:isentropic:a} and Eqn. \ref{eq:isentropic:b} constitutes the isentropic relations

p2p1=(ρ2ρ1)γ=(T2T1)γ/(γ1)

Flow Processes

ds=CvdTT+Rdνν

dν=νRdsCvνRTdT=νRdsCvpdT

for an isentropic process (ds=0), dν<0 for positive values of dT.

ds=CpdTTRdpp

dp=pRds+CppRTdT=pRds+CpρdT

for an isentropic process (ds=0), dp>0 for positive values of dT.


Since ν decreases with temperature and pressure increases with temperature for an isentropic process, we can see from Eqn.~\ref{eqn:process:dnu} that dν 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 dv=0 which implies

0=νR(dsCvdTT)dTds=TCv

and thus we can see that the slope of an isochore in a Ts-diagram is positive and that the slope increases with temperature.

In analogy, we can see that an isobar (dp=0) leads to the following relation

0=pR(CpdTTds)dTds=TCp

and consequently isobars will also have a positive slope that increases with temperature in a Ts-diagram. Moreover, isobars are less steep than ischores as Cp>Cv.