|May 17, 2013, 02:43||
how to calculate the turbulent input parameters for boundary conditions?
nguyen van trieu
Join Date: Jul 2009
Posts: 70Rep Power: 8
Hi every ones,
I am doing simulation for 3D NACA 0012 wing.
I use 3 different tubulent models:
The boundary conditions are:
My question is how to set the turbulent parameters for the input and output bcs such: k,e,I,L,...
I also want to calculate the lift and drag coefficient acting on the wing surface. But I am not sure about the reference values such: area, length. I set the reference area=chord*span and the reference length=chord. Is this right or wrong?
|Thread||Thread Starter||Forum||Replies||Last Post|
|How to calculate turbulent structure?||mohammad||ANSYS||0||December 12, 2012 00:55|
|Problem with divergence||TDK||FLUENT||10||September 8, 2012 01:11|
|giving spacially varying input conditions to Kiva||CHANDER SHEKHAR SHARMA||Main CFD Forum||0||October 6, 2005 09:33|
|Turbulent Mass Injection Boundary Conditions||B. Laubacher||Main CFD Forum||6||October 16, 1999 11:56|
|Initial Conditions in unsteady turbulent flow||Z. Zeng||Main CFD Forum||5||April 28, 1999 17:38|