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2.3 Thermodynamic Relations

Chalmers University of Technology
Department of Mechanical Engineering
Division of Fluid Dynamics

Specific Heat Relations

For thermally perfect and calorically perfect gases

Cp=dhdTCv=dedT\begin{aligned} &C_p=\frac{dh}{dT}\\ &C_v=\frac{de}{dT} \end{aligned}

From the definition of enthalpy and the equation of state p=ρRTp=\rho RT

h=e+pρ=e+RTh=e+\frac{p}{\rho}=e+RT

Differentiate Eqn. (2.9) with respect to temperature gives

dhdT=dedT+d(RT)dT\frac{dh}{dT}=\frac{de}{dT}+\frac{d(RT)}{dT}

Inserting the specific heats gives

Cp=Cv+RC_p=C_v+R

Dividing Eqn. (2.11) by CvC_v gives

CpCv=1+RCv\frac{C_p}{C_v}=1+\frac{R}{C_v}

Introducing the ratio of specific heats defined as

γ=CpCv\gamma=\frac{C_p}{C_v}

Now, inserting Eqn. (2.13) in Eqn. (2.12) gives

Cv=Rγ1C_v=\frac{R}{\gamma-1}

In the same way, dividing Eqn. (2.11) with CpC_p gives

1=CvCp+RCp=1γ+RCp1=\frac{C_v}{C_p}+\frac{R}{C_p}=\frac{1}{\gamma}+\frac{R}{C_p}

and thus

Cp=γRγ1C_p=\frac{\gamma R}{\gamma-1}

Isentropic Relations

First law of thermodynamics:

de=δqδwde=\delta q - \delta w

For a reversible process: δw=pd(1/ρ)\delta w=pd(1/\rho) and δq=Tds\delta q=Tds

de=Tdspd(1ρ)de=Tds-pd\left(\frac{1}{\rho}\right)

Enthalpy is defined as: h=e+p/ρh=e+p/\rho and thus

dh=de+pd(1ρ)+(1ρ)dpdh=de+pd\left(\frac{1}{\rho}\right)+\left(\frac{1}{\rho}\right)dp

Eliminate dede in Eqn. (2.18) using Eqn. (2.19)

Tds=dhpd(1ρ)(1ρ)dp+pd(1ρ)Tds=dh-\cancel{pd\left(\frac{1}{\rho}\right)}-\left(\frac{1}{\rho}\right)dp+\cancel{pd\left(\frac{1}{\rho}\right)}
ds=dhTdpρTds=\frac{dh}{T}-\frac{dp}{\rho T}

Using dh=CpTdh=C_p T and the equation of state p=ρRTp=\rho RT, we get

ds=CpdTTRdppds=C_p\frac{dT}{T}-R\frac{dp}{p}

Integrating Eqn. (2.22) gives

s2s1=12CpdTTRln(p2p1)s_2-s_1=\int_1^2 C_p\frac{dT}{T}-R\ln\left(\frac{p_2}{p_1}\right)

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

s2s1=Cpln(T2T1)Rln(p2p1)s_2-s_1=C_p\ln\left(\frac{T_2}{T_1}\right)-R\ln\left(\frac{p_2}{p_1}\right)

An alternative form of Eqn. (2.24) is obtained by using de=CvdTde=C_v dT Eqn. (2.18), which gives

s2s1=12CvdTTRln(ρ2ρ1)s_2-s_1=\int_1^2 C_v\frac{dT}{T}-R\ln\left(\frac{\rho_2}{\rho_1}\right)

Again, for a calorically perfect gas, we get\

s2s1=Cvln(T2T1)Rln(ρ2ρ1)s_2-s_1=C_v\ln\left(\frac{T_2}{T_1}\right)-R\ln\left(\frac{\rho_2}{\rho_1}\right)

Isentropic Relations:

Adiabatic and reversible processes, i.e., isentropic processes implies ds=0ds=0 and thus Eqn. (2.24) reduces to

CpRln(T2T1)=ln(p2p1)\frac{C_p}{R}\ln\left(\frac{T_2}{T_1}\right)=\ln\left(\frac{p_2}{p_1}\right)
CpR=γγ1\frac{C_p}{R}=\frac{\gamma}{\gamma-1}
γγ1ln(T2T1)=ln(p2p1)\frac{\gamma}{\gamma-1}\ln\left(\frac{T_2}{T_1}\right)=\ln\left(\frac{p_2}{p_1}\right)\Rightarrow
p2p1=(T2T1)γ/(γ1)\frac{p_2}{p_1}=\left(\frac{T_2}{T_1}\right)^{\gamma/(\gamma-1)}

In the same way, Eqn. (2.26) gives

ρ2ρ1=(T2T1)1/(γ1)\frac{\rho_2}{\rho_1}=\left(\frac{T_2}{T_1}\right)^{1/(\gamma-1)}

Eqn. (2.30) and Eqn. (2.31) constitutes the isentropic relations

p2p1=(ρ2ρ1)γ=(T2T1)γ/(γ1)\frac{p_2}{p_1}=\left(\frac{\rho_2}{\rho_1}\right)^{\gamma}=\left(\frac{T_2}{T_1}\right)^{\gamma/(\gamma-1)}