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Search took 0.00 seconds. Search: Posts Made By: black&gold
Forum: Main CFD Forum June 26, 2011, 05:55
Replies: 11
Views: 7,530
Posted By black&gold
Thanks for the tips :-)...even though...

Thanks for the tips :-)...even though all-nighters seem inevitable at some point during this project. I realized the complexities of this type of coding (nonlinear panel generation, etc.) while...
Forum: Main CFD Forum June 25, 2011, 22:25
Replies: 11
Views: 7,530
Posted By black&gold
Also, I couldn't find any detailed references for...

Also, I couldn't find any detailed references for coding panel methods apart from the NASA reports; thats one of the reasons I am looking into VSAERO.

I have been using Katz & Plotkin, Bertin,...
Forum: Main CFD Forum June 25, 2011, 22:20
Replies: 11
Views: 7,530
Posted By black&gold
I am developing the code for use in a larger...

I am developing the code for use in a larger project. I will only be considering a specific wing (with airfoil, wingspan, etc. specified). I went through the VSAERO manual and it seems quite doable...
Forum: Main CFD Forum June 25, 2011, 16:23
Replies: 11
Views: 7,530
Posted By black&gold
Great...I thought I was doing something wrong....

Great...I thought I was doing something wrong. I'll go ahead and try to see if I can code this VSAERO; it seems like exactly what I've been looking for.

Thanks for the help.
Forum: Main CFD Forum June 24, 2011, 22:15
Replies: 11
Views: 7,530
Posted By black&gold
Martin, thanks for the reply. I get a better...

Martin, thanks for the reply. I get a better (closer to the actually values) when I use only the panels as you suggested. I have not been placing the vortex rings panels on the camber line, however....
Forum: Main CFD Forum June 24, 2011, 16:58
Replies: 11
Views: 7,530
Posted By black&gold
Question Vortex Lattice Method: Calculating lift using circulation from vortex ring elements

I am not an aerodynamics guy specifically but I need to do some aerodynamic modeling for my research and ran into some trouble:

I am calculating the lift on a wing using the vortex lattice method...
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