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Search: Posts Made By: michaelmoor.aero
Forum: Main CFD Forum July 16, 2012, 12:23
Replies: 23
Views: 4,540
Posted By michaelmoor.aero
I assume then that this is what you mean: %%...

I assume then that this is what you mean:

%% Apply Boundary Conditions
boundary_conditions();
%% Solve for u*
[ustar, diJ]=u_momentum();

%% Check continuity again
%...
Forum: Main CFD Forum July 14, 2012, 12:05
Replies: 23
Views: 4,540
Posted By michaelmoor.aero
Thanks again for the help! so you are saying that...

Thanks again for the help! so you are saying that after solving the momentum equations yielding u* and v*, that i should apply the outlet boundary condition to these guessed velocity fields u* and...
Forum: Main CFD Forum July 14, 2012, 11:48
Replies: 23
Views: 4,540
Posted By michaelmoor.aero
Thank-you so much for the reply! The pressure...

Thank-you so much for the reply! The pressure boundary condition here was indeed a mistake, however since my domain is I=2 to I=NI-1, and J=2 to NJ-1, those cells never actually came into the...
Forum: Main CFD Forum July 12, 2012, 05:49
Replies: 23
Views: 4,540
Posted By michaelmoor.aero
Hello everyone, thanks for the advice! I went...

Hello everyone, thanks for the advice! I went through it again and found a mistake, but things are still not right.. I am trying to solve for steady Poiseulle flow on a backward staggered grid using...
Forum: Main CFD Forum July 7, 2012, 12:53
Replies: 23
Views: 4,540
Posted By michaelmoor.aero
Hi everyone! I know that I am...

Hi everyone!
I know that I am being an absolute pest on this forum, but desperate times call for desperate measures! I am about 80% complete on my implementation of the SIMPLE...
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