cfx struttural test that

[ferossi]

Bye to all,

I have to find the equivalent stress and aerodynamic forces on a wing, Naca wing profile 0012. I thought I'd use cfx and make a one-way fluid structure interaction. What do you think? or are there any other methods that it is best to use? Please let me know.

for my purpose, is it better to use transient or static?

thanks to all and good day.