|September 18, 2013, 02:19||
How to set AOA for an Airfoil in CFX?
Join Date: Sep 2013
Posts: 8Rep Power: 3
I am using CFX 13, and I want to do analysis of a half delta wing which is at an AOA of 5 deg. At inlet I am giving Total pressure values, and in the flow direction I am giving the unit vector components along X and Z directions. My question is are the settings correct and Does the direction components in flow direction tab take unit vector values or Actual velocity components. Or is der any other method for doing so.
Last edited by fender26; September 19, 2013 at 04:22.
|angle of attack, aoa, wing|
|Thread||Thread Starter||Forum||Replies||Last Post|
|What to set the turbulence specification of airfoil||shlgzz||FLUENT||13||August 29, 2014 06:04|
|tutorial or links in set up the boundary condition of fan||michelle||FLUENT||1||July 18, 2013 09:09|
|[Pointwise] cannot set "fan" boundary condition to 2D Ducted fan model||brksnn||Pointwise & Gridgen||1||January 11, 2013 10:05|
|Need help with CFX simulation for airfoil||Arti||CFX||53||July 14, 2009 13:30|
|Simulating flow past airfoil with different AOA||Quarkz||Main CFD Forum||2||January 6, 2006 11:56|