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Search: Posts Made By: pdp.aero
Forum: SU2 May 21, 2014, 03:31
Replies: 19
Views: 12,010
Posted By pdp.aero
Please, turn off the AMG solver. %...

Please, turn off the AMG solver.

% Multi-Grid Levels (0 = no multi-grid)
MGLEVEL= 0
%
% Multi-Grid Cycle (0 = V cycle, 1 = W Cycle)
MGCYCLE= 0

What is your SU2 version?
Forum: SU2 May 20, 2014, 18:57
Replies: 19
Views: 12,010
Posted By pdp.aero
The attachment is provided in the previous...

The attachment is provided in the previous message.
Forum: SU2 May 20, 2014, 16:46
Replies: 19
Views: 12,010
Posted By pdp.aero
Okay, thank you for providing extra information. ...

Okay, thank you for providing extra information.
The main point is, your Mach number is below the 0.3, so the flow is incompressible. However, you have created a compressible domain which includes...
Forum: SU2 May 20, 2014, 14:48
Replies: 19
Views: 12,010
Posted By pdp.aero
In what dimension the grid and geometry is...

In what dimension the grid and geometry is created? Inch or m?
Further, your geometry is a wing, right? what is the root and tip chord length?
Besides, what is the MAC (Mean Aerodynamic Chord)...
Forum: SU2 May 20, 2014, 14:08
Replies: 19
Views: 12,010
Posted By pdp.aero
Could you please provide more information on your...

Could you please provide more information on your test case, I mean the flow condition, solver setting and etc. It would be more helpful to see your .cfg file to figure out the issue. It will...
Forum: SU2 May 20, 2014, 09:49
Replies: 19
Views: 12,010
Posted By pdp.aero
CFDbeginner88, You need more evaluation for...

CFDbeginner88,

You need more evaluation for making a comparison between the Roe and JST schemes and their accuracy.

Considering the external compressible inviscid flow over an airfoil with AoA...
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