|April 9, 2010, 10:58||
Simple Question Regarding Symmetry Planes
Join Date: Jan 2010
Posts: 8Rep Power: 7
Simple question i hope...
I am looking at the flow around an airfoil and i used a symmetry plane down the centre of the wing in order to reduce computational time.
When it comes to working out the CL of the wing i obtain my z-force using CFX and using CL=L/0.5*rho*v^2*A calculate CL.
My question is what is the area is use? I know it has to be the planform area however as i used a symmetry plane is the area now HALF as the symmetry plane cuts the wing in half, or has the CFD taken this into account and the area is the full plan area.
|Thread||Thread Starter||Forum||Replies||Last Post|
|Question of Anil Date's SIMPLE method||universez||Main CFD Forum||0||November 18, 2009 21:12|
|3D Airplane 'symmetry' BC question (Gambit)||cestrin||ANSYS Meshing & Geometry||2||August 20, 2009 23:43|
|CFX-Pre 5.6 text font - A simple question||Pedro Lima||CFX||3||January 22, 2008 11:29|
|A simple question!||Raintung||FLUENT||3||February 27, 2003 11:11|
|A Simple Question||Thomas P. Abraham||Main CFD Forum||3||September 6, 1999 18:19|