Physics Asked by Foad on December 6, 2020
I’m trying to write the heat transfer equation in an arbitrary fluid (compressible and viscous). Consider an adiabatic system where the only heat generated is due to the internal friction/viscosity. In a fluid, the dissipation function is:
$$Phi_v= check{tau}:check{nabla}^Tcheck{nu} tag{1}$$
$boldsymbol{tau}$ is defined as
$$check{tau}=check{sigma}-Pcheck{I} tag{2}$$
Where $boldsymbol{sigma}$ is the Cauchy stress tensor and $P$ is the hydrostatic pressure.
Assuming that conduction and radiation are negligible, and convection is the only form of heat transfer, I think I can write the conservation of heat as:
$$frac{partial}{partial t}left( q right)
+check{nabla}left( q , check{nu}^T right)=
check{tau}: check{nabla}^T check{nu} tag{3}$$
Now what I do not understand is which one represent heat: enthalpy $h$ or internal energy $e$? For example I’m trying to write the equation for an ideal gas. Can I use enthalpy and write the conservation of heat as:
$$ frac{partial}{partial t}left( rho T right)
+check{nabla}left( rho T , check{nu}^T right)=
frac{1}{c_P} check{tau}:check{nabla}^Tcheck{nu} tag{4}$$
Or should I use the internal energy:
$$ frac{partial}{partial t}left( rho T right)
+check{nabla}left( rho T , check{nu}^T right)=
frac{1}{c_{nu}} check{tau}:check{nabla}^Tcheck{nu} tag{5}$$
Which one of the equations 4 or 5 is the correct form? Or maybe they are both wrong?
Notation:
Ok, after extensive research I think I have found the right answer to this question. Unfortunately there are a lot of different notations and some sources, such as Transport Phenomena by Bird (ed2 2002) which was suggested in the comments, are entirely different.
Firstly, the definition I wrote for viscous stress tensor is wrong. In a perfect fluid:
$$check{tau}=check{sigma}+Pcheck{I} tag{6}$$
Where $check{sigma}$ is the cauchy stress tensor.
Secondly internal energy $e$ is heat and enthalpy $h=e+frac{P}{rho}$ is the total non-kinetic energy (if there is a such a term! or maybe potential energy?), the total energy is $h+frac{1}{2}check{nu}check{nu}^T$. The detailed proof can be found in [1,2] but in the end the result is:
$$ rho frac{D e}{D t}=check{sigma}:check{nabla}check{nu} tag{7}$$
Or in expanded form for an ideal fluid:
$$rholeft( frac{partial e}{partial t}+left( check{nu}check{nabla}^T right)e right)=-Pleft( check{nabla}check{nu}^T right)+ check{tau}:check{nabla}check{nu} tag{8}$$
Obviously for ideal gas $e=c_nu T$ and $P=rho mathring{R} T$. I have the feeling that 8 can be derived from Eqn. 4 in the OP. But I'm not sure.
References:
Answered by Foad on December 6, 2020
Get help from others!
Recent Answers
Recent Questions
© 2024 TransWikia.com. All rights reserved. Sites we Love: PCI Database, UKBizDB, Menu Kuliner, Sharing RPP