CFD Online Logo CFD Online URL
www.cfd-online.com
[Sponsors]
Home > Forums

Search Results

Register Blogs Members List Search Today's Posts Mark Forums Read

Showing results 1 to 1 of 1
Search took 0.00 seconds.
Search: Posts Made By: inspiron
Forum: FLUENT November 19, 2013, 02:26
Replies: 1
Views: 2,176
Posted By inspiron
Unhappy Wrong Drag and Lift Coefficient when changing AoA

I'm trying to calculate Drag and Lift Coefficient of NACA 2415 airfoil. When flow with velocity of 10m/s passes over the airfoil with angle of attack (AOA) = 0, the CD and CL is as same as the data...
Showing results 1 to 1 of 1

 
Forum Jump

All times are GMT -4. The time now is 04:12.