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Old   August 10, 2023, 10:33
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Originally Posted by hunt_mat View Post
The position starts with u=0, the Neumann condition is a stress free condition basically, it's the temperature that drives the process. I'm not too sure for nu, as the boundary condition comes from the velocity.
Ho do you express nu as a function of u? That seems more a sort of Robin condition, not exactly Neumann.
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Old   August 10, 2023, 10:45
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In order to get an idea of the Reynolds number Vr*L/D, one needs to estimate Vr from the BCs:


du/dx=-k*nu -> du*/dx*=-k*nu*L/Vr




Thus, since this is the driving force, one prescribe


Vr=k*nu*L


and Re= k*nu*L^2/D


But that assumes nu=constant, but if you have nu(u) the issue is different.
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Old   August 10, 2023, 11:00
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Quote:
Originally Posted by FMDenaro View Post
In order to get an idea of the Reynolds number Vr*L/D, one needs to estimate Vr from the BCs:


du/dx=-k*nu -> du*/dx*=-k*nu*L/Vr




Thus, since this is the driving force, one prescribe


Vr=k*nu*L


and Re= k*nu*L^2/D


But that assumes nu=constant, but if you have nu(u) the issue is different.
Nu is separate to u, nu varies in space and time, it's the specific volume. Can you use the initial value of nu in the calculations?
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Old   August 10, 2023, 12:13
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Originally Posted by hunt_mat View Post
Nu is separate to u, nu varies in space and time, it's the specific volume. Can you use the initial value of nu in the calculations?
No, maybe the max value to get an idea of the max Re number
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Old   August 10, 2023, 12:43
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Originally Posted by hunt_mat View Post
Nu is separate to u, nu varies in space and time, it's the specific volume. Can you use the initial value of nu in the calculations?



Your M-files shows a solution not only oscillating but under instability, the values are aroud 10^73. Thus, a bug in the code or the numerical stability constraints are not satisfied.
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Old   August 10, 2023, 12:48
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A further big issue is that you have simply assigned


t=linspace(0,3,M);
x=linspace(0,1,N+1);
dt=t(2);
dx=x(2);



without any check about the CFDL and diffusive stability constraint
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Old   August 10, 2023, 13:31
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%Eulerian code for viscous Burgers equation with Neumann BC at x_max
clear;clc;
N=200; %This is the number of point in the x-variable, and also h.
M=1000; %This is the discretisation for the time variable;
t=linspace(0,0.0003,M);
x=linspace(0,1,N+1);
nu=0.1;
u=zeros(M,N+1); %This is the velocity;
dt=t(2);
dx=x(2);
D=0.01;
k=-0.1;
Re=1.0;

% initial condition for u
M=1
u0(1:N+1)=0.0 ;
%BC
u0(1)=0 ;
u0(N+1)=u0(N)-1 ;
u(M,1:N+1)=u0 ;

for k=1:1000,
% fluxes
for i=2:N+1,
conv=0.5*(u0(i)^2+u0(i-1)^2)/2.;
diff=(u0(i)-u0(i-1))/dx/Re;
f(i)=-conv+diff;
end

% Update
for i=2:N,
u1(i)=u0(i)+dt*(f(i+1)-f(i))/dx;
end
%BC
u1(1)=0;
u1(N+1)=u1(N)-1;


%Swap
u0(1:N+1)=u1(1:N+1);
u(k+1,1:N+1)=u1(1:N+1);

plot(u1)
end

pause

contour(u)
end
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Old   August 10, 2023, 13:32
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Se the few-lines code for solving the Burgers equation in FV formulation on a Eulerian grid.


Again, you have to compute the time step allowing the stability.
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Old   August 11, 2023, 07:08
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If I scale my variables according to the following:
h=M\hat{h}, t=\hat{t}/k, \nu=\nu_{0}\hat{\nu}, and u=Mk\nu_{0}\hat{u} leaves us with the following (cleaner) equations upon dropping the hats:
\frac{\partial\nu}{\partial t}=\frac{\partial u}{\partial h}
\frac{\partial}{\partial t}(\nu u)=\frac{\partial }{\partial h}\left(\frac{\alpha}{\nu}\frac{\partial u}{\partial h}+\frac{u^{2}}{2}\right)
The boundary conditions for u are
u(t,0)=0,\frac{\partial u}{\partial h}\Bigg|_{h=1}=\nu(t,1)The constant \alpha=\frac{D}{kM^{2}\nu_{0}^{2}}
To do the stability analysis, do I look at the linear case?
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Old   August 11, 2023, 07:23
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Quote:
Originally Posted by hunt_mat View Post
If I scale my variables according to the following:
h=M\hat{h}, t=\hat{t}/k, \nu=\nu_{0}\hat{\nu}, and u=Mk\nu_{0}\hat{u} leaves us with the following (cleaner) equations upon dropping the hats:
\frac{\partial\nu}{\partial t}=\frac{\partial u}{\partial h}
\frac{\partial}{\partial t}(\nu u)=\frac{\partial }{\partial h}\left(\frac{\alpha}{\nu}\frac{\partial u}{\partial h}\right)
The boundary conditions for u are
u(t,0)=0,\frac{\partial u}{\partial h}\Bigg|_{h=1}=\nu(t,1)The constant \alpha=\frac{D}{kM^{2}\nu_{0}^{2}}
To do the stability analysis, do I look at the linear case?
The stability von Neumann analysis is always based on the linear equation.
In my code I used a very small time step as you can see. Try running.
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Old   August 11, 2023, 08:52
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Quote:
Originally Posted by FMDenaro View Post
The stability von Neumann analysis is always based on the linear equation.
In my code I used a very small time step as you can see. Try running.
I like the fact you compute the fluxes as a separate function, I think that simplifies the code considerably, and it also allows the experimentation with different methods easily.

So I do a von Neumann stability analysis on the equations:
\frac{\partial \nu}{\partial t}=\frac{\partial u}{\partial h}
\frac{\partial u}{\partial t}=\alpha\frac{\partial^{2}u}{\partial h^{2}}
and find out the requirements for stability and try that?
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Old   August 11, 2023, 09:42
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Quote:
Originally Posted by hunt_mat View Post
I like the fact you compute the fluxes as a separate function, I think that simplifies the code considerably, and it also allows the experimentation with different methods easily.

So I do a von Neumann stability analysis on the equations:
\frac{\partial \nu}{\partial t}=\frac{\partial u}{\partial h}
\frac{\partial u}{\partial t}=\alpha\frac{\partial^{2}u}{\partial h^{2}}
and find out the requirements for stability and try that?
A FVM is always coded by computing the fluxes sepatately.
For the stability analysis you have to work on the numerical schemes not on the linear PDEs.
Choose a scheme and the do that.
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Old   August 11, 2023, 10:42
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Quote:
Originally Posted by FMDenaro View Post
A FVM is always coded by computing the fluxes sepatately.
For the stability analysis you have to work on the numerical schemes not on the linear PDEs.
Choose a scheme and the do that.
As I said, I'm relatively new to numerical stuff, and I only know selected bits, computing the fluxes separately has allowed my code to be easier to be read. I corrected my time step accordingly and it now converges beautifully.

Thank you for extending my knowledge of finite volume methods and also getting my code working.
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Old   August 11, 2023, 11:06
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So now I've got it working with the Euler method, are there any other methods I can use that will allow me to decrease the timestep?
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Old   August 11, 2023, 12:35
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So now I've got it working with the Euler method, are there any other methods I can use that will allow me to decrease the timestep?
You have a lot of issues to learn about numerical methods. I strongly suggest to learn the fundamental topics in a good textbook.
For example, here you can read a lot of topics about numerical solution of PDEs

http://www.math.science.cmu.ac.th/do...20of%20PDE.pdf
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Old   August 11, 2023, 17:42
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Originally Posted by FMDenaro View Post
You have a lot of issues to learn about numerical methods. I strongly suggest to learn the fundamental topics in a good textbook.
For example, here you can read a lot of topics about numerical solution of PDEs

http://www.math.science.cmu.ac.th/do...20of%20PDE.pdf
I now have the thorny issue of replacing the constant D with a function of the porosity, and I have to think about how I relate the porosity to the specific volume.
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Old   August 11, 2023, 17:55
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I now have the thorny issue of replacing the constant D with a function of the porosity, and I have to think about how I relate the porosity to the specific volume.

That is as same as happens in turbulence for eddy viscosity model. You have to compute D on any single face of the volumes by introducing the functional relation D=f(x,t).
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Old   August 14, 2023, 08:16
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A scaled version of the equations are:

\frac{\partial\nu}{\partial t}=\frac{\partial u}{\partial h}
\frac{\partial u}{\partial t}=\frac{\partial}{\partial h}\left(\frac{\alpha\zeta(\theta)}{\nu}\frac{\partial u}{\partial h}\right)
Where \theta=1-\nu_{0}/\nu is the porosity, and the function is defined as
\zeta(\theta)=\frac{2}{3\theta}(1-\theta)^{2}
The boundary conditions are given as:
u(t,0)=0,\quad\frac{\partial u}{\partial h}\Bigg|_{h=1}=-\nu(t,1)
The code is playing up, and I was thinking it was something to do with the speed at which the diffusion happens, the speed seems to be increasing negatively quicker than the density seems to be increasing which I find odd.

Another thing I was thinking about is using the Neuman BC for u, to give me a BC for u at h=1, by writing the derivative as a one-sided stencil to get a value for u(t,1). Thoughts? Do you think that will things better?
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Old   August 14, 2023, 11:06
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Quote:
Originally Posted by hunt_mat View Post
A scaled version of the equations are:

\frac{\partial\nu}{\partial t}=\frac{\partial u}{\partial h}
\frac{\partial u}{\partial t}=\frac{\partial}{\partial h}\left(\frac{\alpha\zeta(\theta)}{\nu}\frac{\partial u}{\partial h}\right)
Where \theta=1-\nu_{0}/\nu is the porosity, and the function is defined as
\zeta(\theta)=\frac{2}{3\theta}(1-\theta)^{2}
The boundary conditions are given as:
u(t,0)=0,\quad\frac{\partial u}{\partial h}\Bigg|_{h=1}=-\nu(t,1)
The code is playing up, and I was thinking it was something to do with the speed at which the diffusion happens, the speed seems to be increasing negatively quicker than the density seems to be increasing which I find odd.

Another thing I was thinking about is using the Neuman BC for u, to give me a BC for u at h=1, by writing the derivative as a one-sided stencil to get a value for u(t,1). Thoughts? Do you think that will things better?

The Neumann Bc at x=xmax is what I used in the code I posted.
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Old   August 14, 2023, 14:12
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Originally Posted by FMDenaro View Post
The Neumann Bc at x=xmax is what I used in the code I posted.
I've been looking at your code, and I'm not sure what you've done. I don't quite understand how you've applied the BC. You've solved the viscous burgers equation, I am looking at a system, my conservation of mass, in terms of the finite volume approach is
\int_{h_{j}-\frac{\delta h}{2}}^{h_{j}+\frac{\delta h}{2}}\frac{\partial \nu}{\partial t}dh=\left[ u\right]_{h_{j}-\frac{\delta h}{2}}^{h_{j}+\frac{\delta h}{2}}
So on the end, I need to find an expression for u_{h_{N}+\frac{\delta h}{2}}
I think that If you use a one-sided backward derivative, you can use it to obtain it to get u on the right boundary.
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