|December 2, 2013, 18:27||
Extracting a control volume around an airfoil.
Join Date: Nov 2012
Posts: 2Rep Power: 0
I have simulated a 2D airfoil and I want to determine the drag by the momentum of the fluid. So I want to create a rectangular control volume (CV) around the airfoil to integrate the flow variables over it. For the integration I want to use Matlab, therefore I need to extract the flow variables in the blue CV (s. attached screenshot), but is this possible?
To extract the points on a line I can use Data->Extract->Points from polyline, but how can I extract the points of this CV?
Your help would be appreciated!
|Thread||Thread Starter||Forum||Replies||Last Post|
|Curvature Correction For A Circulation Control Airfoil||Jorg||FLUENT||0||November 19, 2012 12:06|
|BlockMesh FOAM warning||gaottino||OpenFOAM Native Meshers: blockMesh||7||July 19, 2010 14:11|
|Size of control volume||nomad||OpenFOAM||1||September 2, 2009 01:28|
|Axisymmetrical mesh||Rasmus Gjesing (Gjesing)||OpenFOAM Native Meshers: blockMesh||10||April 2, 2007 14:00|
|Control Volume FEM||Charles||Main CFD Forum||0||February 26, 1999 05:19|