|October 12, 2011, 12:37||
Cl, Cd, Reference Values in 2D?
Join Date: Oct 2011
Posts: 2Rep Power: 0
I'm fairly new to fluent so bear with me.
Let me explain my situation:
I am doing a 2D simulation of airfoils (to be more specific NACA 4421 and NACA 23012) and I am confused with what the Cd and Cl are in terms of. Is the Cd and Cl displayed while the simulation is running in units of per meter?
Also, what should my reference area be? My chord length is 2, however, there are alot of opinions that say that the reference area should be the chord length, others that say that it should be the chord length squared.
If you could give any input, that would be great!
|October 20, 2011, 13:04||
Join Date: May 2011
Location: London, UK
Posts: 45Rep Power: 6
Use the chord length as the ref length.
Cl and Cd are non dimensional and it cannot not said to be per m. 2D flow simulation over an aerofoil is analogous to flow past a wing of infinite span.
Also make sure that you set the reference pressure correctly.
|October 20, 2011, 18:04||
Join Date: Feb 2010
Location: Shiraz, Iran
Posts: 108Rep Power: 7
in 2d simulations dept=1,length=chord,area=chord
and about cl,cd,cm reference pressure is not important but reference velocity and density should be checked.
|October 21, 2011, 10:47||
Join Date: May 2009
Posts: 22Rep Power: 8
in such a problem for a 2d prblem and for cd and cl refreance values for velocity,density,area and viscosity should be checked!
|Thread||Thread Starter||Forum||Replies||Last Post|
|It would be wonderful if a tool for FoamToTecplot is available||luckyluke||OpenFOAM Post-Processing||165||November 27, 2012 07:54|
|Building OF 1.6 - CentOS 4.x||Pytthon||OpenFOAM||1||February 2, 2010 12:05|
|Reference Values for Air-Foils with high Angle-of-Attack?||hornig||FLUENT||0||January 9, 2010 12:11|
|Simulation of a single bubble with a VOF-method||Suzzn||CFX||18||October 2, 2009 04:18|
|Fluent 2D Reference Values||Adam||FLUENT||1||January 16, 2009 03:58|