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

Calculating tangential skin friction coefficient on an airfoil

Register Blogs Community New Posts Updated Threads Search

Reply
 
LinkBack Thread Tools Search this Thread Display Modes
Old   May 14, 2021, 06:02
Default Calculating tangential skin friction coefficient on an airfoil
  #1
New Member
 
Ioannis Mandralis
Join Date: May 2021
Posts: 7
Rep Power: 5
imandralis is on a distinguished road
Dear all,

I am trying to calculate the skin friction coefficient on the surface of an airfoil. The output of the SU2 solver gives me the skin friction coefficient in the x-direction, but this needs to be projected onto the tangent of the airfoil surface.

It seems that Su2 doesn't output surface normals that I would normally use for this calculation. How can this be done with the outputs given by SU2, or the functionality in Paraview (I tried generating surface normals but this only works well with polydata).

Thanks in advance.
imandralis is offline   Reply With Quote

Reply

Tags
airfoil, normal, projection, tangent


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
[OpenFOAM] Plotting and calculating Coefficient of lift/drag/moment for an airfoil in Paraview rosalie347 ParaView 0 November 12, 2020 10:43
Ffd_control_point_2d feiyi SU2 4 September 30, 2019 13:42
Skin friction coefficient over surface mich_K OpenFOAM Post-Processing 14 July 5, 2017 10:27
How to plot skin friction coefficient? adilio FLUENT 0 May 29, 2016 16:48
[OpenFOAM] Plot skin friction coefficient on a airfoil dinonettis ParaView 3 April 23, 2009 08:24


All times are GMT -4. The time now is 21:34.