|November 8, 2013, 10:09||
Import airfoil SpaceClaim
Join Date: Nov 2013
Posts: 8Rep Power: 5
I started working on Workbench a few days ago and my goal is to analyze an airfoil.
So my first step is to load the airfoil coordinates in SpaceClaim (I do not have DesignModeler). But it does not work. I have read many explanations on how to do it on the internet and they are all very clear. However it does not work, even though I am using (I think!) the proper format.
So I started investigating and I tried with only a few points of my airfoil. Here is my file:
The result is in the attached picture. I read the coordinates of the points and I have the feeling that SpaceClaim separates the figures through the commas. For example, one of my points has the coordinates (7272; 7641) which really looks like the last line of code...
(btw I also tried adding a "1" at the beginning of everyline to say that it is the curve number 1, but in this case, SpaceClaim would not even read the file and find an error instead at line 1)
Are you familiar with this problem? Your help is much appreciated
|November 4, 2015, 07:42||
Join Date: Jan 2013
Posts: 260Rep Power: 9
just in case anyone needs it:
It shows how to prepare the point data file
|airfoil, coordinates, load, spaceclaim|
|Thread||Thread Starter||Forum||Replies||Last Post|
|Annoying issue of automatic "Rescale to Data Range " with paraFoam/paraview 3.12||keepfit||OpenFOAM Paraview & paraFoam||60||September 18, 2013 03:23|
|Problem with restart solution in shape_optimization.py||robyTKD||SU2 Shape Design||21||May 29, 2013 09:26|
|Creat or Import 2D airfoil profile.||Jackie||FLUENT||14||May 11, 2013 06:16|
|Import an airfoil to ANSYS workbench||NAJEM||FLUENT||0||November 3, 2009 15:12|
|Errors running allwmake in OpenFOAM141dev with WM_COMPILE_OPTION%3ddebug||unoder||OpenFOAM Installation||11||January 30, 2008 21:30|