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

Search Results

Register Blogs Community New Posts Updated Threads Search

Showing results 1 to 1 of 1
Search took 0.00 seconds.
Search: Posts Made By: xTamx420
Forum: Main CFD Forum July 18, 2011, 08:52
Replies: 0
Views: 970
Posted By xTamx420
How do you think this will perform?

I have this sort of aerofoil shaped profile that I am currently testing with ANSYS Fluent to get a plot of lift versus angle attack. I got the results for the lift coefficient at 4 degrees this...
Showing results 1 to 1 of 1

 
Forum Jump

All times are GMT -4. The time now is 09:20.