CFD Online Discussion Forums

CFD Online Discussion Forums (http://www.cfd-online.com/Forums/)
-   CD-adapco (http://www.cfd-online.com/Forums/cd-adapco/)
-   -   Drag coefficient for an airfoil from 0-360 degrees (http://www.cfd-online.com/Forums/cd-adapco/89655-drag-coefficient-airfoil-0-360-degrees.html)

ramarya June 18, 2011 23:54

Drag coefficient for an airfoil from 0-360 degrees
 
hi i'm a electrical student but as a part of my project i need to do analysis in star ccm plus on a airfoil

Joukowski foil wit 16%c camber and 6%c thickness

1. i had a made a 3d file in UG iges file but where to generate mesh file caal i mesh it in star ccm plus if so how?

2.at an angle of attack of 90 degrees and above which method i had to follow in star ccm plus ......................i.e at more flow separation which method is better for better results?

3. for my air foil i need to analyse angle of attack from 0-360 degrees for that can i get better results in star ccm plus or else i need to try some other software?


All times are GMT -4. The time now is 15:25.