CFD Online Logo CFD Online URL
www.cfd-online.com
[Sponsors]
Home > Forums > Software User Forums > SU2

Automatic mesh for airfoil coordinates?

Register Blogs Community New Posts Updated Threads Search

Reply
 
LinkBack Thread Tools Search this Thread Display Modes
Old   May 27, 2015, 13:46
Default Automatic mesh for airfoil coordinates?
  #1
New Member
 
Ryan Barrett
Join Date: May 2015
Posts: 15
Rep Power: 11
Ry10 is on a distinguished road
Hi,

I'm attempting to use SU2 to do a free-form airfoil shape optimization for a wind turbine blade using Kulfan parameters. The problem that I am having is that I need a method to automatically generate the .su2 mesh file based on the airfoil coordinates that I obtain from the input of my Kulfan parameters. I know this is possible because this is what appears to be done in the educational version (SU2_EDU). I am currently using a third-party software called Construct2D to automatically generate the meshes in .p3d and then convert to .su2. The problem is that when I compute the adjoint gradients with this mesh it always gives me a gradient of 0 for all the design variables. Basically, is there a code that I could use to automatically generate the .su2 mesh with the input of an airfoil coordinate file? Thank you very much for your time.
Ry10 is offline   Reply With Quote

Old   June 3, 2015, 01:04
Default
  #2
Senior Member
 
Cean
Join Date: Feb 2010
Posts: 128
Rep Power: 16
shirazbj is on a distinguished road
maybe use gmsh
shirazbj is offline   Reply With Quote

Old   June 4, 2015, 13:09
Default
  #3
New Member
 
Philip Hewitt
Join Date: Oct 2013
Posts: 4
Rep Power: 13
PawHewitt is on a distinguished road
Could use gmsh seeing as there's a script to convert the mesh format to su2. It's in the Meshtools/Fortran folder on github. Haven't used it myself though.

Or you could try to use one of the ready made su2 aerofoil meshes and deform it to match your aerofoil using SU2_DEF/MDC. You have to supply the surface deformations which you could get from the kulfan parameterisation. Requires some tinkering of the code however
PawHewitt is offline   Reply With Quote

Reply

Tags
airfoil coordinate, mesh, su2


Posting Rules
You may not post new threads
You may not post replies
You may not post attachments
You may not edit your posts

BB code is On
Smilies are On
[IMG] code is On
HTML code is Off
Trackbacks are Off
Pingbacks are On
Refbacks are On


Similar Threads
Thread Thread Starter Forum Replies Last Post
[ICEM] Mirror Mesh | Delete duplicate mesh pythag0ra5 ANSYS Meshing & Geometry 6 November 19, 2013 08:35
Automatic Mesh Refinement in OpnFOAM-1.6-ext Daniel_Khazaei OpenFOAM Running, Solving & CFD 0 October 4, 2013 18:48
increasing mesh quality is leading to poor convergence tippo CFX 2 May 5, 2009 11:55
Icemcfd 11: Loss of mesh from surface mesh option? Joe CFX 2 March 26, 2007 19:10
How to control Minximum mesh space? hung FLUENT 7 April 18, 2005 10:38


All times are GMT -4. The time now is 17:22.